CN107933897A - A kind of unmanned plane based on infrared ray sensor - Google Patents
A kind of unmanned plane based on infrared ray sensor Download PDFInfo
- Publication number
- CN107933897A CN107933897A CN201711199054.5A CN201711199054A CN107933897A CN 107933897 A CN107933897 A CN 107933897A CN 201711199054 A CN201711199054 A CN 201711199054A CN 107933897 A CN107933897 A CN 107933897A
- Authority
- CN
- China
- Prior art keywords
- rack
- undercarriage
- unmanned plane
- landing
- present
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Granted
Links
- 238000013016 damping Methods 0.000 claims abstract description 33
- 239000000463 material Substances 0.000 claims description 10
- 230000000630 rising effect Effects 0.000 claims description 3
- 238000000034 method Methods 0.000 claims 2
- 230000000694 effects Effects 0.000 abstract description 8
- 230000033001 locomotion Effects 0.000 description 13
- 238000012544 monitoring process Methods 0.000 description 8
- 238000010586 diagram Methods 0.000 description 6
- 230000007613 environmental effect Effects 0.000 description 4
- 238000009434 installation Methods 0.000 description 4
- 230000001681 protective effect Effects 0.000 description 4
- NJPPVKZQTLUDBO-UHFFFAOYSA-N novaluron Chemical compound C1=C(Cl)C(OC(F)(F)C(OC(F)(F)F)F)=CC=C1NC(=O)NC(=O)C1=C(F)C=CC=C1F NJPPVKZQTLUDBO-UHFFFAOYSA-N 0.000 description 2
- 206010044565 Tremor Diseases 0.000 description 1
- 241000607479 Yersinia pestis Species 0.000 description 1
- 230000015572 biosynthetic process Effects 0.000 description 1
- 230000007123 defense Effects 0.000 description 1
- 230000007812 deficiency Effects 0.000 description 1
- 201000010099 disease Diseases 0.000 description 1
- 208000037265 diseases, disorders, signs and symptoms Diseases 0.000 description 1
- 239000003814 drug Substances 0.000 description 1
- 229940079593 drug Drugs 0.000 description 1
- 230000005611 electricity Effects 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 229910052500 inorganic mineral Inorganic materials 0.000 description 1
- 238000007689 inspection Methods 0.000 description 1
- 238000013507 mapping Methods 0.000 description 1
- 239000011707 mineral Substances 0.000 description 1
- 230000000116 mitigating effect Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000005070 sampling Methods 0.000 description 1
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C25/00—Alighting gear
- B64C25/02—Undercarriages
- B64C25/04—Arrangement or disposition on aircraft
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C25/00—Alighting gear
- B64C25/02—Undercarriages
- B64C25/08—Undercarriages non-fixed, e.g. jettisonable
- B64C25/10—Undercarriages non-fixed, e.g. jettisonable retractable, foldable, or the like
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C25/00—Alighting gear
- B64C25/02—Undercarriages
- B64C25/08—Undercarriages non-fixed, e.g. jettisonable
- B64C25/10—Undercarriages non-fixed, e.g. jettisonable retractable, foldable, or the like
- B64C25/12—Undercarriages non-fixed, e.g. jettisonable retractable, foldable, or the like sideways
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C25/00—Alighting gear
- B64C25/02—Undercarriages
- B64C25/08—Undercarriages non-fixed, e.g. jettisonable
- B64C25/10—Undercarriages non-fixed, e.g. jettisonable retractable, foldable, or the like
- B64C25/18—Operating mechanisms
- B64C25/24—Operating mechanisms electric
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C25/00—Alighting gear
- B64C25/32—Alighting gear characterised by elements which contact the ground or similar surface
- B64C25/58—Arrangements or adaptations of shock-absorbers or springs
- B64C25/62—Spring shock-absorbers; Springs
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/04—Helicopters
- B64C27/08—Helicopters with two or more rotors
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U10/00—Type of UAV
- B64U10/10—Rotorcrafts
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U70/00—Launching, take-off or landing arrangements
- B64U70/60—Take-off or landing of UAVs from a runway using their own power
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C25/00—Alighting gear
- B64C25/32—Alighting gear characterised by elements which contact the ground or similar surface
- B64C2025/325—Alighting gear characterised by elements which contact the ground or similar surface specially adapted for helicopters
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Remote Sensing (AREA)
- Operating, Guiding And Securing Of Roll- Type Closing Members (AREA)
- Power-Operated Mechanisms For Wings (AREA)
Abstract
The invention discloses a kind of unmanned plane based on infrared ray sensor.Gas bag including rack, undercarriage, motor, propeller and damping base；The undercarriage is located at center position immediately below rack, and undercarriage is connected with rack, and motor bottom is fixed on above stent, and propeller is installed on electric machine main shaft, and damping base is fixed on below stent.The present invention can be suitable for the takeoff and landing in the case of mountain area or ground relief and level land, strong applicability and good damping effect at the same time；And the difference in height that compensate for bringing because place is uneven by using support device, the present invention is allowd to carry out stable landing on rough place, avoiding unmanned plane, either the rough place in place causes unmanned plane to be broken or damaged phenomenon because of forced landing to mountain area.
Description
Technical field
The present invention relates to unmanned plane field, a kind of specifically new unmanned plane.
Background technology
Aircraft is to be manufactured by the mankind, can fly away from ground, controlled in space flight and by people in endoatmosphere or big
The apparatus flying object of the gas-bearing formation external space (space) flight, aircraft are divided into aircraft, spacecraft, rocket, guided missile and guided weapon；
Unmanned plane is also one kind of aircraft, and unmanned plane is manipulated not using radio robot and the presetting apparatus provided for oneself
Manned aircraft, from technical standpoint definition can be divided into unmanned helicopter, unmanned fixed-wing aircraft, unmanned multi-rotor aerocraft, nobody
Dirigible and unmanned parasol etc.；It can be divided into by application field military with civilian, military aspect unmanned plane is divided into reconnaissance plane and target drone；
At present, unmanned plane can be widely applied to national ecological environmental protection, aeroplane photography, mapping, mineral resources exploration, the condition of a disaster monitoring,
Traffic patrolling, power-line patrolling, security monitoring, emergent mitigation, emergency command, rain making, national defense safety, land resources exploration,
Town planning, seismic survey, environmental monitoring, forest fire protection, Crop Estimation, the monitoring of protection zone wild animal, air sampling, sea
Thing scouting, border tour, prohibition of drug scouting, fire inspection, ecological environmental protection, marine environmental monitoring, land use survey, water money
It is source exploitation, crop growth monitoring and the yield by estimation, agricultural operation, Natural calamity monitoring and assessment, urban planning and municipal administration, gloomy
The field such as the protection of woods pest and disease damage and monitoring, digital city.
Multi-rotor unmanned aerial vehicle belongs to one kind in unmanned plane, and multi-rotor unmanned aerial vehicle has that compact-sized, build is less than normal, popular
Change relatively strong, movement flexibly and the advantages that flight stability by extensively in civil and military, and quite it is popular；But at present
Multi-rotor unmanned aerial vehicle, so as to carry out battery altering, is supplemented since cruising time short flight is after a certain period of time with regard to needing to land
The energy, also in that this reason causes unmanned plane to be restricted in very many applications, such as unmanned plane in mountain area or
The rough place in place can not carry out takeoff and landing, and unmanned plane also often occurs because of forced landing to mountain area or field
The rough place in ground causes unmanned plane to be broken or damaged phenomenon.In consideration of it, the present invention provides it is a kind of it is new nobody
Machine.
The content of the invention
In order to make up for the deficiencies of the prior art, the present invention provides a kind of new unmanned plane.
The present invention to be solved its technical problem and be realized using following technical scheme.
A kind of new unmanned plane, including rack, undercarriage, motor, propeller and damping base；The undercarriage is located at
Center position immediately below rack, and undercarriage is connected with rack, central rack structure in the form of annular discs, and central rack is along machine
The central axis of frame is uniformly provided with fan-shaped material reducing mouth, and the central axis of shell outside along rack has been symmetrically arranged six branch
Frame, offers bar shaped material reducing mouth on stent, by setting fan-shaped material reducing mouth and bar shaped material reducing mouth to alleviate the weight of rack；It is described
Motor, the quantity of propeller and damping base be six, motor bottom is fixed on above stent, and propeller is installed on motor master
On axis, damping base is fixed on below stent.
Further, the undercarriage includes rise and fall plate, storage box, support device and closing device；The plate that rises and falls
Be square structure, and deck is respectively symmetrically arranged with plate left and right sides of rising and falling, and the cross section of deck is in " Ω " type structure,
Deck is used for the fixation between undercarriage and rack, and uses the deck of " Ω " type structure to be easy to the installation and removal of undercarriage；
The storage box, which is fixed on, to rise and fall on plate bottom face, and storage box is made of outline border and inside casing, and outline border surrounds what is connected with inside casing
" returning " font stores groove, and inside casing space is used for the installation of battery；The support device quantity is four, and support device head and the tail are successively
Outline border is arranged in surround with inside casing in " returning " font storage groove connected；The closing device quantity is two, closing device pair
Title is arranged in storage box lower end.
Further, the damping base includes cushion socket and damping spring；The trapezoidal structure of the cushion socket, damping
Seat upper end is provided with lead, and cushion socket lower end is provided with round bar, is provided with crosspiece in the middle part of cushion socket, is provided with down on crosspiece
Lead, and upper lead and lower lead are located on the same line, damping spring both ends rotating around be sleeved on upper lead and
On lower lead, when the present invention is when level land is taken off or is landed, undercarriage, which can be shunk, not to be had to, and damping base directly serves as
The effect of undercarriage, and damping base reduces the present invention in vibrations when landing of landing, and is effectively protected drop of the present invention
Fall safety and stability when landing.
Further, the support device includes electric rotating machine, motor cabinet, shaft, bearing, electric pushrod, supporting rod, branch
Spike seat, shock-proof spring and sensor；The electric rotating machine is installed in storage box by motor cabinet, shaft one end and rotation
Electric machine main shaft is attached, and the shaft other end is installed on storage box madial wall by bearing, in electric pushrod upper end and shaft
Portion is attached, and electric pushrod lower end is attached with supporting rod one end, and the supporting rod other end is connected with supporting seat, shock-absorbing bullet
Around being sleeved on supporting rod, sensor is installed on supporting seat lateral wall spring, and turning for shaft is driven by the rotation of electric rotating machine
It is dynamic, and be fixedly connected between shaft and electric pushrod, so as to drive electric pushrod to be rotated by pivot of shaft, work as electricity
When dynamic push rod turns to vertical with storage box, the rotation for the motor that stops rotating, starts the stretching motion of electric pushrod, due to support
Sensor is installed on pedestal, and sensor uses infrared ray sensor, when electric pushrod touches ground, electric pushrod stops
Only stretching motion, in the present invention, support device quantity are four, when the present invention mountain area or the place of ground relief into
It is different by the extended length of electric pushrod when row landing is landed, so as to compensate for the height brought because place is uneven
Difference so that the present invention can carry out stable landing on rough place, and reduce the present invention by shock-proof spring and exist
Jitter during landing.
Further, the closing device includes cover board, sliding block, motorized rails and limited block；Two before and after the cover board
Side is respectively symmetrically provided with sliding block, and motorized rails are separately fixed on the front and rear lateral wall of storage box, and motorized rails or so two
End is respectively fixed with limited block, and sliding block is installed on motorized rails, by motorized rails moving left and right with movable slider, so that band
The movement of dynamic cover board, realizes the folding effect of cover board, and closing device plays protective effect to support device.
Further, the supporting seat upper end is provided with sleeve, and sleeve inner is provided with internal thread, and supporting rod lower end is set
External screw thread is equipped with, to be threadedly coupled between supporting rod and the sleeve of supporting seat, supporting seat lower end is provided with support feet, and props up
Spike is evenly arranged along the circumferential direction of supporting seat, and support feet is wedge structure.
When unmanned plane in-flight needs landing to land in the area in mountain area or ground relief, start first electronic
Guide rail, by the left and right two lateral movement of the motorized rails with movable slider, so as to drive cover board, both sides are moved to the left and right, are realized out
Attach together the opening put；Then start electric rotating machine, the rotation of shaft is driven by the rotation of electric rotating machine, and shaft is pushed away with electronic
It is fixedly connected between bar, so as to drive electric pushrod to be rotated by pivot of shaft, when electric pushrod turns to and stores up
Put box it is vertical when, the rotation for the motor that stops rotating, starts the stretching motion of electric pushrod, due to being provided with sensing on supporting seat
Device, and sensor uses infrared ray sensor, when electric pushrod touches ground, electric pushrod stops stretching motion, at this
In invention, support device quantity is four, when the present invention carries out landing in mountain area or the place of ground relief to land, is led to
Cross that the extended length of electric pushrod is different, so as to compensate for the difference in height brought because place is uneven so that the present invention can
To carry out stable landing on rough place, and jitter of the present invention in landing is reduced by shock-proof spring,
Avoiding unmanned plane, either the rough place in place causes unmanned plane to break or damaged show because of forced landing to mountain area
As；When unmanned plane landing, which has supplemented power source, takes off, support device is packed up, closes closing device, closing device is to support
Device plays protective effect, and when unmanned plane is landed on level land, undercarriage, which can be shunk, not to be had to, and damping base directly fills
When the effect of undercarriage, and damping base reduces vibrations of the present invention when landing landing, is effectively protected the present invention
Safety and stability when landing is landed.
Compared with prior art, the present invention has the following advantages：
(1) present invention can be suitable for the takeoff and landing in the case of mountain area or ground relief and level land at the same time, be applicable in
Property strong and good damping effect.
(2) difference in height that the present invention compensate for bringing because place is uneven by using support device so that the present invention
Stable landing can be carried out on rough place, avoids unmanned plane because of forced landing to mountain area or place bumps not
Flat place causes unmanned plane to be broken or damaged phenomenon.
Brief description of the drawings
The present invention is further described with reference to the accompanying drawings and examples.
Fig. 1 is the dimensional structure diagram of the present invention；
Fig. 2 is dimensional structure diagram when rack, motor, propeller and damping base of the present invention coordinate；
Fig. 3 is the dimensional structure diagram of undercarriage of the present invention；
Fig. 4 is the dimensional structure diagram of undercarriage of the present invention (not including closing device)；
Fig. 5 is the bottom view of undercarriage of the present invention (not including closing device)；
Fig. 6 is the dimensional structure diagram of support device of the present invention；
Fig. 7 is the dimensional structure diagram of damping pedestal of the present invention.
Embodiment
In order to make the technical means, the creative features, the aims and the efficiencies achieved by the present invention easy to understand, tie below
Conjunction is specifically illustrating, and the present invention is further explained.
As shown in Figure 1, a kind of new unmanned plane, including rack 1, undercarriage 2, motor 3, propeller 4 and damping base 5；
The undercarriage 2 is located at 1 underface center position of rack, and undercarriage 2 is connected with rack 1, and the middle part of rack 1 is in disk
Shape structure, and the middle part of rack 1 is uniformly provided with fan-shaped material reducing mouth along the central axis of rack 1, the outside of rack 1 is along rack 1
Mandrel line has been symmetrically arranged six stents, and bar shaped material reducing mouth is offered on stent, by setting fan-shaped material reducing mouth and bar shaped
Material reducing mouth alleviates the weight of rack 1；The quantity of the motor 3, propeller 4 and damping base 5 is six, 3 bottom of motor
It is fixed on above stent, propeller 4 is installed on 3 main shaft of motor, and damping base 5 is fixed on below stent.
As shown in Fig. 3 to Fig. 7, the undercarriage 2 includes rise and fall plate 21, storage box 22, support device 23 and folding dress
Put 24；The plate 21 that rises and falls is square structure, and deck, and deck are respectively symmetrically arranged with 21 left and right sides of plate of rising and falling
Cross section be in " Ω " type structure, deck is used for the fixation between undercarriage 2 and rack 1, and using the deck of " Ω " type structure
Easy to the installation and removal of undercarriage 21；The storage box 22, which is fixed on, to rise and fall on 21 bottom face of plate, and storage box 22 is by outline border
Formed with inside casing, outline border surrounds " returning " font storage groove connected with inside casing, and inside casing space is used for the installation of battery；The branch
23 quantity of support arrangement is four, and 23 head and the tail of support device are sequentially arranged in outline border and " returning " font storage groove connected is surrounded with inside casing
It is interior；24 quantity of closing device is two, and closing device 24 is arranged symmetrically in 22 lower end of storage box.
As shown in Fig. 2, the damping base 5 includes cushion socket 51 and damping spring 52；The cushion socket 51 is in ladder
Shape structure, 51 upper end of cushion socket are provided with lead, and 51 lower end of cushion socket is provided with round bar, and the middle part of cushion socket 51 is provided with horizontal stroke
Grade, lower lead is provided with crosspiece, and upper lead and lower lead are located on the same line, 52 both ends of damping spring point
Not around being sleeved on upper lead and lower lead, when the present invention is when level land is taken off or is landed, undercarriage 2 can be shunk not
With damping base 5 has directly served as the effect of undercarriage 2, and damping base 5 reduces the present invention in shake when landing of landing
It is dynamic, it is effectively protected safety and stability when present invention landing is landed.
As shown in Fig. 3 to Fig. 7, the support device 23 includes electric rotating machine 231, motor cabinet 232, shaft 233, axis
Hold 234, electric pushrod 235, supporting rod 236, supporting seat 237, shock-proof spring 238 and sensor 239；The electric rotating machine
231 are installed in storage box 22 by motor cabinet 232, and 233 one end of shaft is attached with 231 main shaft of electric rotating machine, shaft 233
The other end is installed on 22 madial wall of storage box by bearing 234, and 235 upper end of electric pushrod is attached with the middle part of shaft 233,
235 lower end of electric pushrod is attached with 236 one end of supporting rod, and 236 other end of supporting rod is connected with supporting seat 237, shock-absorbing
Around being sleeved on supporting rod 236, sensor 239 is installed on 237 lateral wall of supporting seat spring 238, passes through electric rotating machine 231
The rotation for driving shaft 233 is rotated, and is fixedly connected between shaft 233 and electric pushrod 235, so as to drive electric pushrod 235
Rotated with shaft 233 for pivot, when electric pushrod 235 is turned to it is vertical with storage box 22 when, stop rotating motor
231 rotation, starts the stretching motion of electric pushrod 235, due to being provided with sensor 239, and sensor on supporting seat 237
239 use infrared ray sensor, and when electric pushrod 235 touches ground, electric pushrod 235 stops stretching motion, in this hair
In bright, 23 quantity of support device is four, when the present invention carries out landing in mountain area or the place of ground relief to land, is led to
Cross that the extended length of electric pushrod 235 is different, so as to compensate for the difference in height brought because place is uneven so that the present invention
Stable landing can be carried out on rough place, and the present invention trembling in landing is reduced by shock-proof spring 238
Dynamic property.
As shown in figure 3, the closing device 24 includes cover board 241, sliding block 242, motorized rails 243 and limited block 244；
Both sides are respectively symmetrically provided with sliding block 242 after 241 before the cover board, before motorized rails 243 are separately fixed at storage box 22
Afterwards on lateral wall, and 241 left and right ends of motorized rails are respectively fixed with limited block 244, and sliding block 242 is installed on motorized rails 243
On, by the moving left and right with movable slider 242 of motorized rails 243, so as to drive the movement of cover board 241, realize cover board 241
Folding effect, closing device 24 play protective effect to support device 23.
As shown in Figure 6 and Figure 7,237 upper end of supporting seat is provided with sleeve, and sleeve inner is provided with internal thread,
Supporting rod lower end is provided with external screw thread, to be threadedly coupled between supporting rod and the sleeve of supporting seat 237, under supporting seat 237
End is provided with support feet, and support feet is evenly arranged along the circumferential direction of supporting seat 237, and support feet is wedge structure.
When unmanned plane in-flight needs landing to land in the area in mountain area or ground relief, start first electronic
Guide rail 243, by the left and right two lateral movement of the motorized rails 243 with movable slider 242, so as to drive the both sides to the left and right of cover board 241
It is mobile, realize the opening of closing device 24；Then start electric rotating machine 231, shaft is driven by the rotation of electric rotating machine 231
233 rotation, and be fixedly connected between shaft 233 and electric pushrod 235, so as to drive electric pushrod 235 with shaft 233 for rotation
Turn center to be rotated, when electric pushrod 235 is turned to it is vertical with storage box 22 when, the rotation for the motor 231 that stops rotating, start
The stretching motion of electric pushrod 235, due to being provided with sensor 239 on supporting seat 237, and sensor 239 uses infrared ray
Sensor, when electric pushrod 235 touches ground, electric pushrod 235 stops stretching motion, in the present invention, support device
23 quantity are four, when the present invention carries out landing in mountain area or the place of ground relief to land, pass through electric pushrod 235
Extended length it is different, so as to compensate for the difference in height brought because place is uneven so that the present invention can it is concavo-convex not
Stable landing is carried out on flat place, and jitter of the present invention in landing is reduced by shock-proof spring 238；Work as unmanned plane
When landing has supplemented power source and takes off, support device 23 is packed up, closes closing device 24, closing device 24 is to support device 23
Protective effect is played, when unmanned plane is landed on level land, undercarriage 2, which can be shunk, not to be had to, and damping base 5 directly serves as
The effect of undercarriage 2, and damping base 5 reduces the present invention in vibrations when landing of landing, and is effectively protected the present invention
Safety and stability when landing is landed.
The basic principles, main features and advantages of the invention have been shown and described above.The technical staff of the industry should
Understand, the present invention is not limited to the above embodiments, and the description in above embodiments and description simply illustrates the present invention
Principle, without departing from the spirit and scope of the present invention, various changes and modifications of the present invention are possible, these change and change
Into all fall within the protetion scope of the claimed invention.The claimed scope of the invention is by appended claims and its equivalent
Define.
Claims (2)
- A kind of 1. method of work of unmanned plane, it is characterised in that：Including rack, undercarriage, motor, propeller and damping base； The undercarriage is located at center position immediately below rack, and undercarriage is connected with rack, central rack knot in the form of annular discs Structure, and the central axis of central rack along rack is uniformly provided with fan-shaped material reducing mouth, central axis point of the shell outside along rack Six stents are not symmetrically arranged with, and bar shaped material reducing mouth is offered on stent；The quantity of the motor, propeller and damping base It is six, motor bottom is fixed on above stent, and propeller is installed on electric machine main shaft, and damping base is fixed on below stent； Wherein：The undercarriage includes rise and fall plate, storage box, support device and closing device；The plate that rises and falls is square structure, Deck is respectively symmetrically arranged with plate left and right sides of rising and falling, and the cross section of deck is in " Ω " type structure；The storage Box, which is fixed on, to rise and fall on plate bottom face, and storage box is made of outline border and inside casing, and outline border surrounds " returning " font storage connected with inside casing Put groove；The support device quantity is four, and support device head and the tail are sequentially arranged in outline border and " returning " word connected is surrounded with inside casing In type storage groove；The closing device quantity is two, and closing device is arranged symmetrically in storage box lower end；The damping base includes cushion socket and damping spring；The trapezoidal structure of the cushion socket, cushion socket upper end are set There is upper lead, cushion socket lower end is provided with round bar, is provided with crosspiece in the middle part of cushion socket, lower lead is provided with crosspiece, and Upper lead and lower lead are located on the same line, and damping spring both ends are rotating around being sleeved on upper lead and lower lead On；When unmanned plane landing, which has supplemented power source, takes off, support device is packed up, closes closing device.
- 2. method of work according to claim 1, it is characterised in that：The closing device includes cover board, sliding block, electronic Guide rail and limited block；The cover board front and rear sides are respectively symmetrically provided with sliding block, and motorized rails are separately fixed at storage box On front and rear lateral wall, and motorized rails left and right ends are respectively fixed with limited block, and sliding block is installed on motorized rails.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201711199054.5A CN107933897B (en) | 2016-05-19 | 2016-05-19 | Unmanned aerial vehicle based on infrared ray sensor |
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610339028.7A CN105966602B (en) | 2016-05-19 | 2016-05-19 | A kind of unmanned plane |
| CN201711199054.5A CN107933897B (en) | 2016-05-19 | 2016-05-19 | Unmanned aerial vehicle based on infrared ray sensor |
Related Parent Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201610339028.7A Division CN105966602B (en) | 2016-05-19 | 2016-05-19 | A kind of unmanned plane |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN107933897A true CN107933897A (en) | 2018-04-20 |
| CN107933897B CN107933897B (en) | 2020-12-04 |
Family
ID=56956069
Family Applications (4)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201810082446.1A Active CN108216588B (en) | 2016-05-19 | 2016-05-19 | Unmanned aerial vehicle |
| CN201711199045.6A Withdrawn CN107985559A (en) | 2016-05-19 | 2016-05-19 | Using the unmanned plane and its method of work of infrared ray sensor |
| CN201711199054.5A Active CN107933897B (en) | 2016-05-19 | 2016-05-19 | Unmanned aerial vehicle based on infrared ray sensor |
| CN201610339028.7A Expired - Fee Related CN105966602B (en) | 2016-05-19 | 2016-05-19 | A kind of unmanned plane |
Family Applications Before (2)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201810082446.1A Active CN108216588B (en) | 2016-05-19 | 2016-05-19 | Unmanned aerial vehicle |
| CN201711199045.6A Withdrawn CN107985559A (en) | 2016-05-19 | 2016-05-19 | Using the unmanned plane and its method of work of infrared ray sensor |
Family Applications After (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201610339028.7A Expired - Fee Related CN105966602B (en) | 2016-05-19 | 2016-05-19 | A kind of unmanned plane |
Country Status (1)
| Country | Link |
|---|---|
| CN (4) | CN108216588B (en) |
Families Citing this family (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110654533A (en) * | 2018-06-29 | 2020-01-07 | 海鹰航空通用装备有限责任公司 | Unmanned aerial vehicle undercarriage |
| CN109353493A (en) * | 2018-09-28 | 2019-02-19 | 许剑聪 | A kind of self-rescue device of drowning unmanned plane equipped with gas generation buoyancy |
| CN112046735B (en) * | 2020-09-17 | 2024-05-28 | 辽宁工程技术大学 | Multifunctional unmanned aerial vehicle landing gear |
| CN112173115B (en) * | 2020-11-12 | 2022-05-13 | 观典防务技术股份有限公司 | Use method of high-altitude rescue unmanned aerial vehicle with damping device |
| CN113525664B (en) * | 2021-09-16 | 2022-01-07 | 速晟电子(深圳)有限公司 | Modularized sensor and unmanned aerial vehicle adaptive to same |
| CN114408199A (en) * | 2022-01-28 | 2022-04-29 | 广东皓耘科技有限公司 | Unmanned aerial vehicle positioning and correcting mechanism and undercarriage positioning auxiliary device |
| CN116142515B (en) * | 2023-04-18 | 2023-06-27 | 浙江亿钛数控机械有限公司 | Stably supported unmanned aerial vehicle undercarriage |
Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CA2815885A1 (en) * | 2013-05-15 | 2014-11-15 | Draganfly Innovations Inc. | Compact unmanned rotary aircraft |
| US8973861B2 (en) * | 2012-10-29 | 2015-03-10 | Shenzhen Hubsan Technology Co., Ltd. | Tetra-propeller aircraft |
| CN104787309A (en) * | 2015-05-12 | 2015-07-22 | 厦门大学 | Rotary wing drone landing gear |
| CN104787319A (en) * | 2015-04-23 | 2015-07-22 | 张�杰 | Four-rotor aircraft provided with telescopic and foldable undercarriages |
| CN205098463U (en) * | 2015-10-22 | 2016-03-23 | 郑州大学 | Full topography helicopter undercarriage |
Family Cites Families (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US6715714B2 (en) * | 2001-09-24 | 2004-04-06 | Larry Dan Temple | Landing gear for model airplane |
| CN101746500B (en) * | 2009-12-03 | 2012-10-03 | 李子赫 | Device for compensating the difference of height by which a helicopter lands on a non-horizontal ground and the method thereof |
| CN204161620U (en) * | 2014-10-16 | 2015-02-18 | 云南电网公司红河供电局 | The full landform retractable landing gear of depopulated helicopter |
| CN204916163U (en) * | 2015-06-19 | 2015-12-30 | 深圳一电科技有限公司 | Foot rest and unmanned aerial vehicle |
| CN204956904U (en) * | 2015-09-14 | 2016-01-13 | 南京工程学院 | Many rotor crafts intelligence alighting carriage and control system thereof |
| CN205055438U (en) * | 2015-09-21 | 2016-03-02 | 重庆燕蓝科技有限公司 | A buffering undercarriage for model aeroplane and model ship aircraft |
| CN205113694U (en) * | 2015-11-21 | 2016-03-30 | 长沙学院 | Buffering foot rest of rotor craft |
-
2016
- 2016-05-19 CN CN201810082446.1A patent/CN108216588B/en active Active
- 2016-05-19 CN CN201711199045.6A patent/CN107985559A/en not_active Withdrawn
- 2016-05-19 CN CN201711199054.5A patent/CN107933897B/en active Active
- 2016-05-19 CN CN201610339028.7A patent/CN105966602B/en not_active Expired - Fee Related
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US8973861B2 (en) * | 2012-10-29 | 2015-03-10 | Shenzhen Hubsan Technology Co., Ltd. | Tetra-propeller aircraft |
| CA2815885A1 (en) * | 2013-05-15 | 2014-11-15 | Draganfly Innovations Inc. | Compact unmanned rotary aircraft |
| CN104787319A (en) * | 2015-04-23 | 2015-07-22 | 张�杰 | Four-rotor aircraft provided with telescopic and foldable undercarriages |
| CN104787309A (en) * | 2015-05-12 | 2015-07-22 | 厦门大学 | Rotary wing drone landing gear |
| CN205098463U (en) * | 2015-10-22 | 2016-03-23 | 郑州大学 | Full topography helicopter undercarriage |
Also Published As
| Publication number | Publication date |
|---|---|
| CN105966602A (en) | 2016-09-28 |
| CN107985559A (en) | 2018-05-04 |
| CN108216588A (en) | 2018-06-29 |
| CN108216588B (en) | 2021-05-25 |
| CN105966602B (en) | 2018-01-19 |
| CN107933897B (en) | 2020-12-04 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN105966602B (en) | A kind of unmanned plane | |
| CN105952842B (en) | A kind of power-line patrolling unmanned plane charging base station damping device | |
| CN105966599B (en) | A kind of aircraft | |
| CN105644774B (en) | A kind of multi-rotor aerocraft undercarriage based on Stewart six-degree-of-freedom parallel connection mechanisms | |
| CN105730686B (en) | A kind of multi-rotor aerocraft based on Stewart six-degree-of-freedom parallel connection mechanisms | |
| CN105966605B (en) | A kind of six rotorcraft based on delta parallel institutions | |
| CN107140226A (en) | A kind of magnetic-type four rotor flying robots charging landing platform | |
| CN106122361A (en) | A kind of multi-rotor aerocraft intelligent docking equipment | |
| CN107813925A (en) | The high aircraft landing gear of landing stability of taking off | |
| CN106184795B (en) | A kind of plant protection unmanned plane charging station | |
| CN106184796A (en) | A kind of on-air radio network detecting unmanned plane charging station damped platform | |
| CN105914844B (en) | A kind of multidimensional damping type unmanned plane charging station | |
| CN105857585B (en) | A kind of unmanned plane undercarriage suitable for mountain area flight | |
| CN106081144B (en) | A kind of power-line patrolling unmanned plane charging base station | |
| CN105882944B (en) | A kind of unmanned plane undercarriage with dual shock absorption function | |
| CN106051034B (en) | A kind of electric power reconnoitres flying robot and stops charging equipment vibration-damped table | |
| CN106005464B (en) | A kind of energy-saving unmanned plane energy ancillary equipment | |
| CN105978458B (en) | A kind of adjustable supporting | |
| CN206939103U (en) | A kind of magnetic-type four rotor flying robots charging landing platform | |
| CN105909926A (en) | Vibration reducing device for unmanned aerial vehicle charging base station based on Stewart parallel mechanism | |
| CN106184797A (en) | A kind of novel UAV Intelligent stops equipment | |
| CN105966607B (en) | A kind of unmanned plane vibration-damped table based on delta parallel institutions | |
| CN105966606B (en) | A kind of telescopic type aircraft damping |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| TA01 | Transfer of patent application right | ||
| TA01 | Transfer of patent application right |
Effective date of registration: 20201117 Address after: 225400 Jiangsu city of Taizhou province Taixing City Grain Mill Road Economic Development Zone No. 28 Applicant after: JIANGSU JINCHENG AVIATION TECHNOLOGY Co.,Ltd. Address before: 213000 Jinling North Road, Xinbei District, Changzhou City, Jiangsu Province, No. 139 Applicant before: Cai Liufeng |
|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| TR01 | Transfer of patent right | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20230324 Address after: 311600 Building 108, No.1 Wenhua Road, Hangkong Town, Shouchang Town, Jiande City, Hangzhou City, Zhejiang Province Patentee after: Zhejiang Xianglong Aviation Technology Co.,Ltd. Address before: 225400 No. 28 Nianfang Road, Taixing Economic Development Zone, Taizhou City, Jiangsu Province Patentee before: JIANGSU JINCHENG AVIATION TECHNOLOGY Co.,Ltd. |