CN107466990A - Fluid reinforcement structure, check valve, intelligent mosquito eradication equipment, hair dryer, fan, aircraft or rocket or the propeller of ship or submarine - Google Patents
Fluid reinforcement structure, check valve, intelligent mosquito eradication equipment, hair dryer, fan, aircraft or rocket or the propeller of ship or submarine Download PDFInfo
- Publication number
- CN107466990A CN107466990A CN201710960603.XA CN201710960603A CN107466990A CN 107466990 A CN107466990 A CN 107466990A CN 201710960603 A CN201710960603 A CN 201710960603A CN 107466990 A CN107466990 A CN 107466990A
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- fluid
- check valve
- conical cavity
- reinforcement structure
- valve element
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- 239000012530 fluid Substances 0.000 title claims abstract description 156
- 230000002787 reinforcement Effects 0.000 title claims abstract description 98
- 241000255925 Diptera Species 0.000 title claims abstract description 23
- 230000008029 eradication Effects 0.000 title description 14
- 238000013473 artificial intelligence Methods 0.000 claims abstract description 5
- 241000256626 Pterygota <winged insects> Species 0.000 claims description 17
- 230000035945 sensitivity Effects 0.000 claims description 4
- 239000007787 solid Substances 0.000 claims description 2
- 238000005516 engineering process Methods 0.000 description 39
- 238000010586 diagram Methods 0.000 description 24
- 238000009826 distribution Methods 0.000 description 7
- 238000004519 manufacturing process Methods 0.000 description 6
- 238000006243 chemical reaction Methods 0.000 description 5
- 239000000463 material Substances 0.000 description 5
- 239000004033 plastic Substances 0.000 description 4
- 229920003023 plastic Polymers 0.000 description 4
- 239000005416 organic matter Substances 0.000 description 3
- CURLTUGMZLYLDI-UHFFFAOYSA-N Carbon dioxide Chemical compound O=C=O CURLTUGMZLYLDI-UHFFFAOYSA-N 0.000 description 2
- 230000000694 effects Effects 0.000 description 2
- 230000005484 gravity Effects 0.000 description 2
- 230000001788 irregular Effects 0.000 description 2
- 239000011553 magnetic fluid Substances 0.000 description 2
- 210000003934 vacuole Anatomy 0.000 description 2
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 2
- 235000017166 Bambusa arundinacea Nutrition 0.000 description 1
- 235000017491 Bambusa tulda Nutrition 0.000 description 1
- 241001330002 Bambuseae Species 0.000 description 1
- 229920000049 Carbon (fiber) Polymers 0.000 description 1
- 235000015334 Phyllostachys viridis Nutrition 0.000 description 1
- 230000006978 adaptation Effects 0.000 description 1
- 239000000956 alloy Substances 0.000 description 1
- 229910045601 alloy Inorganic materials 0.000 description 1
- 239000011425 bamboo Substances 0.000 description 1
- 229910002092 carbon dioxide Inorganic materials 0.000 description 1
- 239000001569 carbon dioxide Substances 0.000 description 1
- 239000004917 carbon fiber Substances 0.000 description 1
- 239000011111 cardboard Substances 0.000 description 1
- 239000000919 ceramic Substances 0.000 description 1
- 229910010293 ceramic material Inorganic materials 0.000 description 1
- 239000002131 composite material Substances 0.000 description 1
- 238000005260 corrosion Methods 0.000 description 1
- 230000007797 corrosion Effects 0.000 description 1
- 238000001514 detection method Methods 0.000 description 1
- 238000002474 experimental method Methods 0.000 description 1
- 239000004744 fabric Substances 0.000 description 1
- ZZUFCTLCJUWOSV-UHFFFAOYSA-N furosemide Chemical group C1=C(Cl)C(S(=O)(=O)N)=CC(C(O)=O)=C1NCC1=CC=CO1 ZZUFCTLCJUWOSV-UHFFFAOYSA-N 0.000 description 1
- 239000011521 glass Substances 0.000 description 1
- -1 inorganic matter Substances 0.000 description 1
- 231100000518 lethal Toxicity 0.000 description 1
- 230000001665 lethal effect Effects 0.000 description 1
- 239000007788 liquid Substances 0.000 description 1
- 239000002184 metal Substances 0.000 description 1
- 229910052751 metal Inorganic materials 0.000 description 1
- VNWKTOKETHGBQD-UHFFFAOYSA-N methane Chemical compound C VNWKTOKETHGBQD-UHFFFAOYSA-N 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 239000000203 mixture Substances 0.000 description 1
- 238000012544 monitoring process Methods 0.000 description 1
- 239000003870 refractory metal Substances 0.000 description 1
- 239000011435 rock Substances 0.000 description 1
- 239000005060 rubber Substances 0.000 description 1
- 239000002689 soil Substances 0.000 description 1
- 230000000007 visual effect Effects 0.000 description 1
- 239000002023 wood Substances 0.000 description 1
Classifications
-
- A—HUMAN NECESSITIES
- A01—AGRICULTURE; FORESTRY; ANIMAL HUSBANDRY; HUNTING; TRAPPING; FISHING
- A01M—CATCHING, TRAPPING OR SCARING OF ANIMALS; APPARATUS FOR THE DESTRUCTION OF NOXIOUS ANIMALS OR NOXIOUS PLANTS
- A01M1/00—Stationary means for catching or killing insects
- A01M1/08—Attracting and catching insects by using combined illumination or colours and suction effects
-
- A—HUMAN NECESSITIES
- A01—AGRICULTURE; FORESTRY; ANIMAL HUSBANDRY; HUNTING; TRAPPING; FISHING
- A01M—CATCHING, TRAPPING OR SCARING OF ANIMALS; APPARATUS FOR THE DESTRUCTION OF NOXIOUS ANIMALS OR NOXIOUS PLANTS
- A01M1/00—Stationary means for catching or killing insects
- A01M1/02—Stationary means for catching or killing insects with devices or substances, e.g. food, pheronones attracting the insects
- A01M1/026—Stationary means for catching or killing insects with devices or substances, e.g. food, pheronones attracting the insects combined with devices for monitoring insect presence, e.g. termites
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16K—VALVES; TAPS; COCKS; ACTUATING-FLOATS; DEVICES FOR VENTING OR AERATING
- F16K15/00—Check valves
- F16K15/02—Check valves with guided rigid valve members
-
- G—PHYSICS
- G05—CONTROLLING; REGULATING
- G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
- G05D13/00—Control of linear speed; Control of angular speed; Control of acceleration or deceleration, e.g. of a prime mover
- G05D13/62—Control of linear speed; Control of angular speed; Control of acceleration or deceleration, e.g. of a prime mover characterised by the use of electric means, e.g. use of a tachometric dynamo, use of a transducer converting an electric value into a displacement
-
- H—ELECTRICITY
- H04—ELECTRIC COMMUNICATION TECHNIQUE
- H04L—TRANSMISSION OF DIGITAL INFORMATION, e.g. TELEGRAPHIC COMMUNICATION
- H04L67/00—Network arrangements or protocols for supporting network services or applications
- H04L67/01—Protocols
- H04L67/10—Protocols in which an application is distributed across nodes in the network
-
- H—ELECTRICITY
- H04—ELECTRIC COMMUNICATION TECHNIQUE
- H04L—TRANSMISSION OF DIGITAL INFORMATION, e.g. TELEGRAPHIC COMMUNICATION
- H04L67/00—Network arrangements or protocols for supporting network services or applications
- H04L67/01—Protocols
- H04L67/12—Protocols specially adapted for proprietary or special-purpose networking environments, e.g. medical networks, sensor networks, networks in vehicles or remote metering networks
-
- H—ELECTRICITY
- H04—ELECTRIC COMMUNICATION TECHNIQUE
- H04N—PICTORIAL COMMUNICATION, e.g. TELEVISION
- H04N7/00—Television systems
- H04N7/18—Closed-circuit television [CCTV] systems, i.e. systems in which the video signal is not broadcast
- H04N7/183—Closed-circuit television [CCTV] systems, i.e. systems in which the video signal is not broadcast for receiving images from a single remote source
-
- A—HUMAN NECESSITIES
- A01—AGRICULTURE; FORESTRY; ANIMAL HUSBANDRY; HUNTING; TRAPPING; FISHING
- A01M—CATCHING, TRAPPING OR SCARING OF ANIMALS; APPARATUS FOR THE DESTRUCTION OF NOXIOUS ANIMALS OR NOXIOUS PLANTS
- A01M2200/00—Kind of animal
- A01M2200/01—Insects
- A01M2200/012—Flying insects
Landscapes
- Engineering & Computer Science (AREA)
- Life Sciences & Earth Sciences (AREA)
- Pest Control & Pesticides (AREA)
- Signal Processing (AREA)
- Zoology (AREA)
- Computer Networks & Wireless Communication (AREA)
- General Engineering & Computer Science (AREA)
- Environmental Sciences (AREA)
- Insects & Arthropods (AREA)
- Wood Science & Technology (AREA)
- Mechanical Engineering (AREA)
- Physics & Mathematics (AREA)
- Automation & Control Theory (AREA)
- General Physics & Mathematics (AREA)
- Multimedia (AREA)
- Health & Medical Sciences (AREA)
- Computing Systems (AREA)
- General Health & Medical Sciences (AREA)
- Medical Informatics (AREA)
- Check Valves (AREA)
Abstract
A kind of check valve fluid reinforcement structure, including collector, there is conical cavity on collector, the big big end of conical cavity opening is used to input fluid, the small small end of conical cavity opening is used to export fluid to valve element, and it using taper cavity axis is the consistent spiral stream guidance structure of clockwise that circles round of the equally distributed structure of circumference array unanimously to have at least two on the inwall of conical cavity;The convolution degree of spiral stream guidance structure is less than or equal to 135 degree;The attachment on access path between spiral stream guidance structure and spiral stream guidance structure is not passed through the axis of conical cavity on space path, that is to say, that the path on the axis of conical cavity be for fluid it is straight-through be not hinder.Check valve has a kind of foregoing check valve fluid reinforcement structure.Mosquito killer lamp or Intelligent mosquito killing lamp or artificial intelligence Mosquito killer lamp have foregoing check valve fluid reinforcement structure or check valve.The structure of the present invention is simple, long lifespan, and cost is cheap.
Description
Technical field
The present invention relates to fluidic structures, have fluid reinforcement structure, check valve, intelligent mosquito eradication equipment, blower fan, fluid dynamic
Aircraft or rocket or the propeller of ship or submarine.
Technical background
Winged insect equipment of going out is such as go out moth lamp, Mosquito killer lamp, electric mosquito flap etc. for killing the instrument of winged insect.
It is go out a kind of important way of winged insect equipment, such as mosquito eradication equipment to hold winged insect using wind-force, carbon dioxide bait
Inhale mosquito equipment.
Our company kills equipment in research winged insect, when devise a kind of winged insect trapping equipment(Referring to our company
2017108372608th, No. 2017211880165 patent applications), its mode is to use detection device(Such as camera)Monitoring is set
Standby surrounding whether there is winged insect, then starts blower fan if there is winged insect and blows check valve open, is sucked winged insect using the suction of blower fan
Winged insect cage, reach the lethal purpose of imprison winged insect.
The existing blower fan for inhaling winged insect typically has an axle at center, and the presence of this axle causes the wind that blower fan is blown out
There is area at a slow speed in central area, the small surrounding in wind-force center is big, and our company finds, it is difficult to blow the valve element of check valve open, causes list
It is difficult to open to valve.
Although there is the shaftless blower fan in center in prior art, but cost has the blower fan of axle much larger than center, consider commodity
Cost, have that the blower fan of axle is cheaper using center, more there is competitiveness in civil area.
The pressure in the ejection section of traditional fluid nozzle is generally uniformly continuous change, once the fluid driving of propeller
The Fluid pressure that section failure flows to spout is irregular, and the easy disequilibrium of fluid of ejection, especially rocket nozzles are released
Fluid pressure distribution it is unbalance, easily cause rocket offset track or even tumble and cause disaster.The appearance of existing electric fan, hair dryer
Easily being scattered because of the resistance of air, it is not far to blow.
The content of the invention
To solve above technical problem, the present invention proposes fluid reinforcement structure, check valve, mosquito eradication equipment, intelligent mosquito eradication
Equipment, artificial intelligence mosquito eradication equipment.The engineer of our company chance on flow spiral is advanced can to strengthen blower fan blowout logical
There is the blower fan blowout channel end pressure of entity axle at the blast of road end, the center of solving the problems, such as.
1st, fluid reinforcement structure, it is characterised in that:Including collector, there is conical cavity on collector, conical cavity opening is big
Big end be used to input fluid, the small small end of conical cavity opening is used to export fluid, have on the inwall of conical cavity at least two with
Taper cavity axis are the consistent spiral stream guidance structure of the consistent convolution clockwise of the equally distributed structure of circumference array;Spiral is led
The convolution degree of flow structure is less than or equal to 135 degree;The company on access path between spiral stream guidance structure and spiral stream guidance structure
Connect the axis that thing is not passed through conical cavity on space path, that is to say, that the path on the axis of conical cavity is for fluid
Straight-through is that the unencumbered solid for being advantageous to be mingled with fluid passes through conical cavity;What the valve element for increasing check valve was subject to
Pressure increases the sensitivity of check valve(For the fluid of input, the stream at the big end of conical cavity opening corresponding to valve element is opened
Body force pressure more sluggishness is bigger).(Convolution degree refers to contact line and the taper of the inwall of spiral stream guidance structure and conical cavity
Total number of degrees that line rotates when big end of the line along conical cavity to small extreme direction between the axis of chamber develops, with reference to spring, return
Rotation can be more than the 360 degree i.e. number of turns of spiral and be more than 1, and convolution degree is less than 180 degree that is the spiral number of turns of spiral stream guidance structure
Less than half-turn.)When convolution degree is more than 135, flow-guiding structure edge is largely vortexed generation, and the boosting function of structure becomes very weak.
2nd, the fluid reinforcement structure as described in technology contents 1, it is characterised in that:Spiral stream guidance structure is to be attached to conical cavity
Spiral plate or plate face on the inwall straight panel neither parallel also misaligned with taper cavity axis or bent plate.
3rd, the fluid reinforcement structure as described in technology contents 2, it is characterised in that:The spiral in the longitudinal section figure of conical cavity
Line segment that the one end on the surface of plate is connected with taper cavity wall is straight line or is curve or for perpendicular to the axis of conical cavity
Straight line.
4th, the fluid reinforcement structure as described in technology contents 2, it is characterised in that:Spiral plate or straight panel by conical cavity big end
Thickness to the small end plate of conical cavity gradually changes.
5th, the fluid reinforcement structure as described in technology contents 2, it is characterised in that:The height conversion of spiral plate is coordinate curve
It is presented as the line of camber line, bend in one direction.(The height of spiral plate refers to the surface of spiral plate in the longitudinal section figure of conical cavity
The length of straight line).
6th, the fluid reinforcement structure as described in technology contents 2, it is characterised in that:In the central side and spiral plate of spiral plate
The sectional area of the without hindrance passage formed between heart side is more than or equal to the fluid effluent face product of the small small end of conical cavity opening.
(The central side of spiral plate refers to the side of the hithermost conical cavity of spiral plate).
7th, the fluid reinforcement structure as described in technology contents 2, it is characterised in that:In the central side and spiral plate of spiral plate
The heart is reinforced between side using ring, increases the life-span.
8th, the fluid reinforcement structure as described in technology contents 1, it is characterised in that:Spiral stream guidance structure is taper cavity wall
On helicla flute.
9th, the fluid reinforcement structure as described in technology contents 8, it is characterised in that:The groove width of helicla flute by conical cavity big end
Small end to conical cavity tapers into.
10th, the fluid reinforcement structure as described in technology contents 8, it is characterised in that:The sectional view of helicla flute is V-arrangement or ladder
Shape or U-shaped, the opening of conical cavity is on the inwall of conical cavity.
11st, the fluid reinforcement structure as described in technology contents 8, it is characterised in that:Each helicla flute with adjacent spiral
Groove connects so that in the dentation that peak valley is adjacent on the inside of the annular image of the cross section of conical cavity.
12nd, the fluid reinforcement structure as described in technology contents 1, it is characterised in that:The quantity of spiral stream guidance structure be 3,4,
5th, 6,7,8,9,10,11,12,13,14,15,16,17,18,19, (ellipsis represents ellipsis both ends number to 20......99999
Integer sequence between value).
13rd, the fluid reinforcement structure as described in technology contents 1, it is characterised in that:Spiral stream guidance structure in conical cavity by
Big end to the convolution degree of small end is the arbitrary value between 2 degree to 90 degree.
14th, the fluid reinforcement structure as described in technology contents 1, it is characterised in that:Spiral stream guidance structure in conical cavity by
Big end to the convolution degree of small end is the arbitrary value between 2 degree to 75 degree.
15th, the fluid reinforcement structure as described in technology contents 1, it is characterised in that:Spiral stream guidance structure in conical cavity by
Big end to the convolution degree of small end is the arbitrary value between 2 degree to 60 degree.
16th, the fluid reinforcement structure as described in technology contents 1, it is characterised in that:Spiral stream guidance structure in conical cavity by
Big end to the convolution degree of small end is the arbitrary value between 2 degree to 45 degree.
17th, the fluid reinforcement structure as described in technology contents 1, it is characterised in that:Spiral stream guidance structure in conical cavity by
Big end to the convolution degree of small end is the arbitrary value between 2 degree to 30 degree.
18th, the fluid reinforcement structure as described in technology contents 1, it is characterised in that:Spiral stream guidance structure in conical cavity by
Big end to the convolution degree of small end is the arbitrary value between 2 degree to 15 degree.
19th, the fluid reinforcement structure as described in technology contents 1, it is characterised in that:Spiral stream guidance structure in conical cavity by
Big end to the convolution degree of small end is the arbitrary value between 2 degree to 5 degree.
20th, the fluid reinforcement structure as described in technology contents 1, it is characterised in that:One end of spiral stream guidance structure and taper
The aperture position at the big big end of chamber opening is connected.
21st, the fluid reinforcement structure as described in technology contents 1, it is characterised in that:One end of spiral stream guidance structure and taper
The aperture position of the small small end of chamber opening is connected.
22nd, the fluid reinforcement structure as described in technology contents 1, it is characterised in that:One end of spiral stream guidance structure and taper
The aperture position at the big big end of chamber opening is connected, the other end of spiral stream guidance structure and the opening of the big small end of conical cavity opening
Position is connected.
23rd, the fluid reinforcement structure as described in technology contents 1, it is characterised in that:Spiral stream guidance structure neither with conical cavity
The aperture position at the big big end of opening is connected, and the aperture position of the small end big with conical cavity opening is not connected yet, that is to say, that spiral
Flow-guiding structure is located between big end and the small end of conical cavity.
24th, the fluid reinforcement structure as described in technology contents 1, it is characterised in that:The quantity of spiral stream guidance structure is odd number.
25th, the fluid reinforcement structure as described in technology contents 1, it is characterised in that:The quantity of spiral stream guidance structure is even number.
26th, the fluid reinforcement structure as described in technology contents 1, it is characterised in that:For as the wind for having axle using center
A part of the machine as the automatic fluid valve of the winged insect equipment of going out of getter device, improve the sensitivity of the automatic opening of check valve.
27th, a kind of check valve, it is characterised in that:Including the fluid reinforcement described in any technology contents in technology contents 1-26
Structure, valve element, valve element are located at outside the small small end of conical cavity opening of check valve fluid reinforcement structure, check valve fluid reinforcement structure
For increasing to the thrust of valve element, when the big big end of the conical cavity opening of check valve fluid reinforcement structure inputs without fluid, valve element
Obstruction or the partly small small end of obstruction conical cavity opening.
28th, a kind of check valve as described in technology contents 27, it is characterised in that:Described valve element is spherical shape.
29th, a kind of check valve as described in technology contents 27, it is characterised in that:Described valve element be sheet or it is discoid or
It is cylindric.
30th, a kind of check valve as described in technology contents 27, it is characterised in that:Described valve element or the knot coordinated with valve element
There is space, or valve element and the cooperation between the structure of valve element cooperation have space, are flowed when fluid strength very little on structure
Body is from the space on valve element by the way that when fluid strength is big, valve element is pushed open by fluid, open larger fluid passage.(Space
Actual internal area is less than the actual internal area for the fluid passage phase that valve element is controlled).
31st, mosquito eradication equipment or intelligent mosquito eradication equipment or artificial intelligence mosquito eradication equipment, it is characterised in that:With such as technology contents
Fluid reinforcement structure in 1-26 described in any technology contents.
32nd, mosquito eradication equipment or intelligent mosquito eradication equipment or artificial intelligence mosquito eradication equipment, it is characterised in that:With such as technology contents
A kind of check valve in 27-30 described in any technology contents.
33rd, hair dryer or fan, it is characterised in that:With the fluid as described in any technology contents in technology contents 1-26
Reinforcement structure.
34th, aircraft or the propeller of rocket or ship or submarine, it is characterised in that:With any in such as technology contents 1-26
Fluid reinforcement structure described in technology contents.
Although the original intent of the present invention is researched and developed for the winged insect lamp that goes out, but the reinforcement structure of the present invention can be used for other and set
It is standby, for example sewer anti-backflow, muddy water anti-backflow, the puff prot for aircraft jet engine can increase stability, be used for
The motive fluid spout of magnetohydrodynamic propeller can increase stability, the flame jet for rocket engine can increase
Stability, the motive fluid spout for the submarine of magnetic fluid driving can increase stability and reduce the generation of fluid vacuole,
Other operations repeat no more, and reinforcement Structure adaptation of the invention is in various fluids, and the compressibility of fluid is better, and reinforcement effect is got over
Substantially, structure of the invention is simple, long lifespan, and cost is cheap.The manufacture material of the reinforcement structure of the present invention includes but is not limited to
Artificial plastics, rubber, ceramics, glass, metal, alloy, carbon fiber, bamboo wood, timber, cortex, cardboard, cloth, rock, soil,
Abiotic organic matter, inorganic matter, organic matter, biological organic matter, the manufacture material of fluid reinforcement structure of the invention can be single
Matter can also be mixture, and the specifically chosen engineer of the manufacture material of reinforcement structure of the invention can be according to specifically using ring
Border is selected, for example selects plastic material to manufacture fluid reinforcement structure with cost-effective in mosquito eradication equipment, in aircraft, rocket
Utilization on select refractory metal or ceramic material manufacture fluid reinforcement structure, magnetic fluid driving submarine motive fluid
The homogenous material or composite manufacture fluid reinforcement structure that resistance to vacuole impact is lost with upper selection corrosion resistant chemistry of spout.Fluid
The pressure distribution in the ejection section of fluid nozzle of the fluid after the conical cavity outflow of the collector of the present invention by the present invention
Distribution is different from the pressure distribution in the ejection section of traditional fluid nozzle, and pressure distribution area is uneven, and higher-pressure region is with circle
All array distributions are better than traditional spout under stability, anti-risk, selfreparing.(The ejection section of traditional fluid nozzle
Pressure is generally uniformly continuous change, once fluid drive apparatus breaks down, air-out is irregular, can not restoration fluids spout automatically
The fluid pressure distribution that the easy disequilibrium of fluid of ejection, especially rocket nozzles are released is unbalance, easily causes rocket to deviate
Track, which even tumbles, causes disaster), fluid reinforcement structure of the invention is desirably integrated into existing aircraft, rocket, ship, magnetic current
Body is promoted on the liquid propeller of submarine, and qualified engineer knows specifically how to use, and repeats no more, the present invention is the army and the people two
Technology, the present invention are the inventions of structure class, it is easy to are understood, secrecy is unnecessary, it is difficult to maintain secrecy, should not be used as and protect
Close patent, the international patent application of the present invention please not be hindered using the present invention as secret patent.
Brief description of the drawings
Fig. 1 is the schematic diagram of embodiment 1, and wherein a is outline plan figure, and b is a midship sections A-A schematic diagram, and c is bottom
Portion's line of vision schematic diagram, d are stereo-picture schematic diagram;S1 be body, the S10 of check valve fluid reinforcement structure be conical cavity, S11 be
Spiral stream guidance structure, S12 are the small end of conical cavity i.e. the fluid issuing of check valve fluid reinforcement structure, and S13 is conical cavity
Big end i.e. check valve fluid reinforcement structure fluid intake;Spiral stream guidance structure is spiral plate, and the quantity of spiral plate is
5, the height conversion of spiral plate is presented as the line of camber line, bend in one direction for coordinate curve.
Fig. 2 is the schematic diagram of embodiment 2, and wherein a is top line of vision figure, and b is a midship sections A-A schematic diagram, and c is bottom
Portion's line of vision schematic diagram, d are stereo-picture schematic diagram;S1 be body, the S10 of check valve fluid reinforcement structure be conical cavity, S11 be
Spiral stream guidance structure, S12 are the small end of conical cavity i.e. the fluid issuing of check valve fluid reinforcement structure, and S23 is conical cavity
Big end i.e. check valve fluid reinforcement structure fluid intake;Spiral stream guidance structure is spiral plate, and the quantity of spiral plate is
5, the height conversion of spiral plate is presented as straight line for coordinate curve, that is to say, that the height of the spiral plate of this embodiment is constant
's.
Fig. 3 is the schematic diagram of embodiment 3, and wherein a is outline plan figure, and b is a midship sections A-A schematic diagram, and c is bottom
Portion's line of vision schematic diagram, d are stereo-picture schematic diagram;S3 be body, the S30 of check valve fluid reinforcement structure be conical cavity, S31 be
Spiral stream guidance structure, S32 are the small end of conical cavity i.e. the fluid issuing of check valve fluid reinforcement structure, and S33 is conical cavity
Big end i.e. check valve fluid reinforcement structure fluid intake;Spiral stream guidance structure is helicla flute, and the quantity of spiral plate is
12, helicla flute position V-shaped groove.
Fig. 4 is the schematic diagram of embodiment 4, and wherein a is top line of vision figure, and b is a midship sections B-B schematic diagram;S4 is single
Body, S41 to valve fluid reinforcement structure are spiral stream guidance structure, each helicla flute of small end of S4 conical cavity with it is adjacent
Helicla flute connects annular image of the inner side to be formed in the adjacent dentation of peak valley(Referring to position pointed by S49).
Fig. 5 is the schematic diagram of embodiment 5, and wherein a is outline plan figure, and b is a midship sections A-A schematic diagram, and c is bottom
Portion's line of vision schematic diagram, d are stereo-picture schematic diagram;S5 be body, the S50 of check valve fluid reinforcement structure be conical cavity, S51 be
Spiral stream guidance structure, S59 be valve element its be ball, S57 that foamed plastics is made be valve element containing body, S58 be valve element accommodating chamber, valve
Core accommodating chamber is conical cavity, spiral stream guidance structure S51 is tabular;The conical cavity of the body of check valve fluid reinforcement structure it is small
End is connected with the valve element accommodating chamber of valve element containing body by cylindrical pipe S56;Valve element is placed in valve element accommodating chamber.Use
When by the big big end of the opening of the conical cavity of the body of check valve fluid reinforcement structure down, valve element accommodating chamber is opened for conical cavity
Mouthful big end upward, by the big big end of the opening of the conical cavity of the body of check valve fluid reinforcement structure and blower fan phase during use
Even, valve element is blown afloat into floating after the wind of blower fan blowout is pressurized via check valve fluid reinforcement structure, when blower fan is not dried
Valve element is because gravity fall is blocked or half obstruction cylindrical pipe S56, the embodiment can be used as
2017108372608th, the check valve of winged insect lamp is inhaled in No. 2017211880165 patent applications.
Fig. 6 is the schematic diagram of embodiment 6, and wherein a is bottom line of vision figure, and b is a midship sections A-A schematic diagram, and c is side
Portion's schematic diagram, d are stereo-picture schematic diagram;S6 is the body of check valve fluid reinforcement structure, and S61 is as fluid flow guiding knot
The helicla flute of structure, the aperture position at the lower end of the helicla flute big end big with conical cavity opening are connected, the upper end of helicla flute not with
The aperture position of the small small end of conical cavity opening is connected.
The schematic diagram of technical problem overcome is needed when Fig. 7 is original research of the present invention, wherein P3 is blower fan, and Z1 is wind
The axle at machine center, P3 motor are ensconced inside axle Z1(Referring to the CPU or power supply heat sinking fan of computer), W1 is that blower fan end is hindered
Area of leaking out after plug, P4 are the conical cavity for not possessing the spiral stream guidance structure of the present invention, although can also collect the presence of wind efficiency
Room for improvement, although the collection wind effect of conical cavity can be increased by elongating conical cavity P4 length, meeting if elongating
The volume of product is caused to increase, Fig. 7 is to reader's interpretation technique problem, strengthen the understanding of reader, Fig. 7 is from this
Among the product schematic diagram of 2017108372608, No. 2017211880165 patent applications of company;With the reinforcement knot of the present invention
The taper cavity segment that structure is replaced in Fig. 7 can increase the thrust that light ball is subject to, and improve the sensitivity of the unlatching fluid passage of light ball,
Increase product efficiency, reduce product cost, increase product competitiveness.Be worth reiterating when, original research mesh of the invention
Be not to the present invention application limit the reasons why, reinforcement structure of the invention can be used for other equipment,
Such as check valve, the check valve of muddy water anti-backflow of sewer anti-backflow, the check valve of the water channel anti-backflow containing debris.
Specific embodiment
The implementation example of the present invention is illustrated below in conjunction with the accompanying drawings.
Embodiment 1, as shown in figure 1, fluid reinforcement structure, S1 is that body, the S10 of check valve fluid reinforcement structure are cone
Shape chamber, S11 are spiral stream guidance structure, and S12 is the small end of conical cavity i.e. the fluid issuing of check valve fluid reinforcement structure,
S13 is big end i.e. the fluid intake of check valve fluid reinforcement structure of conical cavity;Spiral stream guidance structure is spiral plate, spiral
The quantity of plate is 5, and the height conversion of spiral plate is presented as the line of camber line, bend in one direction for coordinate curve.
Embodiment 2, as shown in Fig. 2 fluid reinforcement structure, S1 is that body, the S10 of check valve fluid reinforcement structure are cone
Shape chamber, S11 are spiral stream guidance structure, and S12 is the small end of conical cavity i.e. the fluid issuing of check valve fluid reinforcement structure,
S23 is big end i.e. the fluid intake of check valve fluid reinforcement structure of conical cavity;Spiral stream guidance structure is spiral plate, spiral
The quantity of plate is 5, and the height conversion of spiral plate is presented as straight line for coordinate curve, that is to say, that the spiral plate of this embodiment
Height is constant.
Embodiment 3, as shown in figure 3, fluid reinforcement structure, S3 is that body, the S30 of check valve fluid reinforcement structure are cone
Shape chamber, S31 are spiral stream guidance structure, and S32 is the small end of conical cavity i.e. the fluid issuing of check valve fluid reinforcement structure,
S33 is big end i.e. the fluid intake of check valve fluid reinforcement structure of conical cavity;Spiral stream guidance structure is helicla flute, spiral
The quantity of plate is 12, helicla flute position V-shaped groove.
Embodiment 4, as shown in figure 4, fluid reinforcement structure,;S4 is that body, the S41 of check valve fluid reinforcement structure are
Spiral stream guidance structure, each helicla flute of small end of the S4 conical cavity inner side to be formed that connects with adjacent helicla flute is in peak valley phase
The annular image of adjacent dentation(Referring to position pointed by S49).
Embodiment 5, as shown in figure 5, body, S50 that S5 is check valve fluid reinforcement structure are conical cavity, S51 is spiral shell
Rotation flow-guiding structure, S59 be valve element its be ball, S57 that foamed plastics is made be valve element containing body, S58 be valve element accommodating chamber, valve element
Accommodating chamber is conical cavity, spiral stream guidance structure S51 is tabular;The small end of the conical cavity of the body of check valve fluid reinforcement structure
It is connected with the valve element accommodating chamber of valve element containing body by cylindrical pipe S56;Valve element is placed in valve element accommodating chamber.During use
By the big big end of the opening of the conical cavity of the body of check valve fluid reinforcement structure down, valve element accommodating chamber is the opening of conical cavity
The big big end of the opening of the conical cavity of the body of check valve fluid reinforcement structure upward, is connected during use by big end with blower fan,
Valve element is blown afloat floating by the wind of blower fan blowout via after the supercharging of check valve fluid reinforcement structure, valve element when blower fan is not dried
Because gravity fall obstruction or half obstruction cylindrical pipe S56, this embodiment can be used as 2017108372608,
The check valve of winged insect lamp is inhaled in No. 2017211880165 patent applications.
Embodiment 6, as shown in fig. 6, S6 is the body of check valve fluid reinforcement structure, S61 is as fluid flow guiding
The helicla flute of structure, the aperture position at the lower end of the helicla flute big end big with conical cavity opening are connected, and the upper end of helicla flute is not
The aperture position of the small end small with conical cavity opening is connected.
Other explanations, part is not repeated as prior art either common knowledge or those skilled in the art this visual human
It can settle a dispute by the parties concerned themselves, our company did substantial amounts of real experiment and also made substantial amounts of computer computer and imitates for the structure of the present invention
Very, some the emulation annex of data by patent application(Referring to other documentary evidences)Submit to Patent Office, the application text
The reader of part needs that if these these emulation data Patent Office can be seeked advice from, and can also contact our company's acquisition.
Claims (10)
- A kind of 1. check valve fluid reinforcement structure, it is characterised in that:Including collector, there is conical cavity, conical cavity on collector The big big end of opening is used to inputting fluid, and the small small end of conical cavity opening is used to exporting fluid to valve element, on the inwall of conical cavity Led with least two using the taper cavity axis convolution clockwise consistent spiral consistent as the equally distributed structure of circumference array Flow structure;The convolution degree of spiral stream guidance structure is less than or equal to 135 degree;Company between spiral stream guidance structure and spiral stream guidance structure Connect the axis that the attachment on path is not passed through conical cavity on space path, that is to say, that the path pair on the axis of conical cavity For fluid be it is straight-through be that the unencumbered solid for being advantageous to be mingled with fluid passes through conical cavity;For increasing check valve Valve element be subject to pressure increase check valve sensitivity(For the fluid of input, conical cavity corresponding to unlatching valve element is opened The Fluid pressure pressure more sluggishness at the big end of mouth is bigger).
- A kind of 2. check valve fluid reinforcement structure as claimed in claim 1, it is characterised in that:Spiral stream guidance structure is to be attached to Spiral plate on taper cavity wall.
- A kind of 3. check valve fluid reinforcement structure as claimed in claim 1, it is characterised in that:Spiral stream guidance structure is conical cavity Helicla flute on inwall.
- A kind of 4. check valve fluid reinforcement structure as claimed in claim 1, it is characterised in that:The quantity of spiral stream guidance structure is 3rd, 4,5,6,7,8,9,10,11,12,13,14,15,16,17,18,19, (ellipsis represents ellipsis two to 20......99999 Hold the integer sequence between numerical value).
- A kind of 5. check valve fluid reinforcement structure as claimed in claim 1, it is characterised in that:Spiral stream guidance structure is in conical cavity It is interior by hold greatly to small end convolution degree be 2 degree to 90 degree arbitrary value.
- A kind of 6. check valve fluid reinforcement structure as claimed in claim 1, it is characterised in that:For having axle as using center A part of the blower fan as the automatic fluid valve of the winged insect equipment of going out of getter device, improve check valve automatic opening it is sensitive Degree.
- A kind of 7. check valve, it is characterised in that:Including a kind of check valve stream described in any claim in claim 1-26 Body reinforcement structure, valve element, valve element are located at outside the small small end of conical cavity opening of check valve fluid reinforcement structure, and check valve fluid increases Power structure is used to increase the thrust to valve element, and the big end that the conical cavity opening of check valve fluid reinforcement structure is big inputs without fluid When, valve element obstruction or the partly small small end of obstruction conical cavity opening.
- A kind of 8. check valve as claimed in claim 27, it is characterised in that:Described valve element is spherical shape.
- A kind of 9. check valve as claimed in claim 27, it is characterised in that:On described valve element or the structure coordinated with valve element With space, or there is space in cooperation between valve element and the structure that coordinates valve element, when fluid strength very little fluid from Space on valve element is by the way that when fluid strength is big, valve element is pushed open by fluid, open larger fluid passage.
- 10. Mosquito killer lamp or Intelligent mosquito killing lamp or artificial intelligence Mosquito killer lamp, it is characterised in that:With any in such as claim 1-7 Check valve fluid reinforcement structure or check valve described in claim.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
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CN201710960603.XA CN107466990A (en) | 2017-10-16 | 2017-10-16 | Fluid reinforcement structure, check valve, intelligent mosquito eradication equipment, hair dryer, fan, aircraft or rocket or the propeller of ship or submarine |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
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CN201710960603.XA CN107466990A (en) | 2017-10-16 | 2017-10-16 | Fluid reinforcement structure, check valve, intelligent mosquito eradication equipment, hair dryer, fan, aircraft or rocket or the propeller of ship or submarine |
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CN201710960603.XA Withdrawn CN107466990A (en) | 2017-10-16 | 2017-10-16 | Fluid reinforcement structure, check valve, intelligent mosquito eradication equipment, hair dryer, fan, aircraft or rocket or the propeller of ship or submarine |
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Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN110631059A (en) * | 2019-10-08 | 2019-12-31 | 深圳市三利来智能厨业股份有限公司 | Damp-proof insulating radiationless device of induction cooker |
CN111306328A (en) * | 2020-03-27 | 2020-06-19 | 四川华气动力有限责任公司 | High-power gas engine precombustion chamber air inlet one-way valve |
CN112696624A (en) * | 2020-12-23 | 2021-04-23 | 梁飞燕 | Park deinsectization street lamp that city brightening engineering used |
CN117249426A (en) * | 2023-10-23 | 2023-12-19 | 湖北工程学院 | Landscape lighting lamp |
Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN201037434Y (en) * | 2007-04-04 | 2008-03-19 | 林灿煌 | Carbon deposit removing auxiliary device for vehicle exhaust pipe |
CN102401160A (en) * | 2011-08-09 | 2012-04-04 | 汪砚秋 | Conical core pressure difference one-way valve |
CN104006042A (en) * | 2014-06-10 | 2014-08-27 | 东南大学 | Flow guiding pipeline guiding fluid to spirally go forwards |
CN204510453U (en) * | 2014-12-08 | 2015-07-29 | 石景润 | A kind of prefabricated pumping plant without blocking self-cleaning function integral type |
CN204602449U (en) * | 2015-05-13 | 2015-09-02 | 濮阳市鸿宇压力容器有限公司 | A kind of air bubble spiral nozzle |
-
2017
- 2017-10-16 CN CN201710960603.XA patent/CN107466990A/en not_active Withdrawn
Patent Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN201037434Y (en) * | 2007-04-04 | 2008-03-19 | 林灿煌 | Carbon deposit removing auxiliary device for vehicle exhaust pipe |
CN102401160A (en) * | 2011-08-09 | 2012-04-04 | 汪砚秋 | Conical core pressure difference one-way valve |
CN104006042A (en) * | 2014-06-10 | 2014-08-27 | 东南大学 | Flow guiding pipeline guiding fluid to spirally go forwards |
CN204510453U (en) * | 2014-12-08 | 2015-07-29 | 石景润 | A kind of prefabricated pumping plant without blocking self-cleaning function integral type |
CN204602449U (en) * | 2015-05-13 | 2015-09-02 | 濮阳市鸿宇压力容器有限公司 | A kind of air bubble spiral nozzle |
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN110631059A (en) * | 2019-10-08 | 2019-12-31 | 深圳市三利来智能厨业股份有限公司 | Damp-proof insulating radiationless device of induction cooker |
CN111306328A (en) * | 2020-03-27 | 2020-06-19 | 四川华气动力有限责任公司 | High-power gas engine precombustion chamber air inlet one-way valve |
CN112696624A (en) * | 2020-12-23 | 2021-04-23 | 梁飞燕 | Park deinsectization street lamp that city brightening engineering used |
CN112696624B (en) * | 2020-12-23 | 2023-01-17 | 威海亚光灯具有限公司 | Park deinsectization street lamp that city brightening engineering used |
CN117249426A (en) * | 2023-10-23 | 2023-12-19 | 湖北工程学院 | Landscape lighting lamp |
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Application publication date: 20171215 |