CN207545656U - Escape flying suit - Google Patents
Escape flying suit Download PDFInfo
- Publication number
- CN207545656U CN207545656U CN201721565599.9U CN201721565599U CN207545656U CN 207545656 U CN207545656 U CN 207545656U CN 201721565599 U CN201721565599 U CN 201721565599U CN 207545656 U CN207545656 U CN 207545656U
- Authority
- CN
- China
- Prior art keywords
- interlayer
- ontology
- width
- wingspread
- front side
- 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.)
- Expired - Fee Related
Links
- 239000011229 interlayer Substances 0.000 claims abstract description 50
- 239000000112 cooling gas Substances 0.000 claims abstract description 13
- 210000002414 leg Anatomy 0.000 claims abstract description 9
- 210000001217 buttock Anatomy 0.000 claims abstract description 7
- 239000007789 gas Substances 0.000 claims description 12
- 241000270666 Testudines Species 0.000 claims description 5
- 230000000694 effects Effects 0.000 abstract description 4
- 206010013647 Drowning Diseases 0.000 abstract description 2
- 208000027418 Wounds and injury Diseases 0.000 abstract description 2
- 230000006378 damage Effects 0.000 abstract description 2
- 208000014674 injury Diseases 0.000 abstract description 2
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 abstract description 2
- 238000010586 diagram Methods 0.000 description 5
- 238000009434 installation Methods 0.000 description 3
- 230000009191 jumping Effects 0.000 description 2
- 239000010410 layer Substances 0.000 description 2
- 238000000926 separation method Methods 0.000 description 2
- 235000001674 Agaricus brunnescens Nutrition 0.000 description 1
- 229920000742 Cotton Polymers 0.000 description 1
- 230000003139 buffering effect Effects 0.000 description 1
- 239000002775 capsule Substances 0.000 description 1
- 230000007423 decrease Effects 0.000 description 1
- 238000011161 development Methods 0.000 description 1
- 238000007599 discharging Methods 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 238000002474 experimental method Methods 0.000 description 1
- 239000004744 fabric Substances 0.000 description 1
- 230000003993 interaction Effects 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000000465 moulding Methods 0.000 description 1
- 230000004083 survival effect Effects 0.000 description 1
- 238000012549 training Methods 0.000 description 1
Landscapes
- Professional, Industrial, Or Sporting Protective Garments (AREA)
Abstract
The utility model provides a kind of escape flying suit, including garment body, wingspread is set between the both arms and buttocks of the ontology and between both legs, whole back panel is set on rear side of ontology and on rear side of wingspread, the first interlayer is formed between wingspread and back panel on rear side of the ontology, multiple air holes are offered on wingspread, it is characterised in that：Width before being provided on front side of the ontology forms the second interlayer of the closing being located on front side of body between preceding width and ontology, and the cooling gas check valve that can only be circulated from the first interlayer to the second interlayer is equipped between second interlayer and the first interlayer.So as to form air bag on front side of human body, increase the skyborne buoyancy of human body, significantly reduce sinking speed；Cushioning effect is played in landing, reduces the injury to human body, and if fallen on the water, can also avoid drowning；It impacted so as to provide a kind of reduction landing, be more suitable for the escape flying suit that ordinary people uses, be particularly suitable for high building or aircraft high altitude escape.
Description
Technical field
The utility model is related to a kind of escape flying suit, in particular, being mainly used for high building or high altitude escape.
Background technology
At present, traditional flying suit mainly includes the garment body that is adapted with human body, ontology both arms and buttocks it
Between and both legs between be respectively mounted double-deck flying wing cloth, respectively front wing and rear wing.Air hole, front wing are provided on the forward and backward wing
Air hole be opened at armpit, and the air hole of rear wing is then opened in below buttocks.The effect of air hole is that the front and rear wing is made to fly
When gassy, such flying wing just can fully unfold, and gas, when discharging flying wing, direction is converted into downwards, in this way
With regard to lift during flight can be increased.Also there is flying suit to use and the wing is set between the both arms and buttocks of ontology and between both legs
Width sets whole back panel on rear side of the ontology and on rear side of wingspread, air holes is opened up on wingspread, and during decline, air is from air holes
In interlayer on rear side of into wingspread, ontology between back panel, so as to the lift to human body bigger.
Although these existing flying suits can reduce the speed of personal fall, in landing, impact is still very big, needs
Parachute is coordinated to be landed, and ordinary people does not carry out the study and training that parachute uses, therefore these flying suits
Use limit to very much, be not suitable for ordinary people escape.Application No. is 201420530299.7 utility application texts
A kind of wind-tunnel aerofoil profile clothes are disclosed in part, proposes to carry out landing and buffering in joint setting cotton pad, but is suitable only for wind-tunnel
Experiment.With the development of society, city high rise building is more and more, aircraft trip is also more and more common.But high building and aircraft high-altitude
Escape problem still have it is to be solved.
Utility model content
The technical problem to be solved by the utility model is to provide a kind of escape flying suits, are impacted for reducing landing,
It is more suitable for ordinary people's use.
The technical solution of the utility model is as follows：A kind of escape flying suit, including garment body, in the both arms of the ontology
Wingspread between buttocks and between both legs is set, whole back panel is set on rear side of ontology and on rear side of wingspread, in the ontology
The first interlayer is formed between rear side and wingspread and back panel, multiple air holes are offered on wingspread, is provided on front side of the ontology
Preceding width forms the second interlayer of the closing being located on front side of body between preceding width and ontology, is pressed from both sides in second interlayer and first
The cooling gas check valve that can only be circulated from the first interlayer to the second interlayer is equipped between layer.
The edge that the preceding width is connected with ontology extends into the first interlayer, forms at least one be located in the first interlayer
A bilayer mounting portion, each double-deck mounting portion includes front side width and rear side width, between the front side width and rear side width
Space is penetrated through with the second interlayer, and at least one air admission hole, the cooling gas check valve installation are provided on each front side width
In each air inlet position.
There are three the bilayer mounting portions, respectively the top below both arms between both legs.
It is equipped with and the one-to-one air holes of each air admission hole on the wing bat.
When the second interlayer gassy, the air bag of turtle shell shape is formed in front of body.The air bag of turtle shell shape in this way can be with
Further reduce landing impact, and body is protected.
Gas tube is installed on the preceding width, also be provided on gas tube can only air inlet cooling gas check valve, the inflation
Pipe is located at preceding width neckline.
Multiple parachutes are installed on width in the rear.
Advantageous effect：The utility model forms the second folder by width before being set on front side of ontology between preceding width and ontology
Layer installs the cooling gas check valve that can only be circulated from the first interlayer to the second interlayer between the second interlayer and the first interlayer；In reality
Border is in use, the air in the first interlayer is filled with the second interlayer under gas pressure, so as to form air bag on front side of human body, the gas
Capsule can not only further increase the skyborne buoyancy of human body, significantly reduce sinking speed；And it can be played in landing
Cushioning effect reduces the injury to human body, and if fallen on the water, can also play the role of loop for seeking survival, avoids drowning；From
And provide a kind of reduce and land impact, be more suitable for the escape flying suit that ordinary people uses, it is particularly suitable for high building or aircraft
High altitude escape.Also, this flying suit is worn in bungee jumping, when aerostatic buoyancy and human bady gravitational balance, human body can be suspended in
In the air, it can be creeped in the air and wait multi-motions, so as to increase the style playing method of bungee jumping campaign, be improved recreational.Further,
Cooling gas check valve is installed by stretching into the double-deck mounting portion in the first interlayer, be may advantageously facilitate air and is promptly and efficiently entered into second
Interlayer.The gas tube that setting is located at neckline on preceding width can be blown using artificial to second in the case of ample time
Interlayer is inflated, make the utility model even if in low latitude in use, buffer air bag can be formed in front of human body.Pacify on back panel
The parachute of dress, when landing, can be unfolded to form the parachute of multiple similar small mushrooms, be conducive to further reduce sinking speed.
Description of the drawings
It, below will be right in order to illustrate more clearly of specific embodiment of the present invention or technical solution of the prior art
Specific embodiment or attached drawing needed to be used in the description of the prior art are briefly described.In all the appended drawings, it is similar
Element or part are generally identified by similar reference numeral.In attached drawing, each element or part might not be according to practical ratios
It draws.
Fig. 1 is the structure diagram of the utility model.
The A-A section views rotation figure that Fig. 2 is Fig. 1.
Fig. 3 is the structure diagram of ontology.
Fig. 4 is the structure diagram of preceding width.
Fig. 5 is the structure diagram of back panel.
The unfolded state schematic diagram of parachute when Fig. 6 is landing.
Reference numeral：Preceding 1, gas tube 2, wing bat 3, air holes 4, ontology 5, back panel 6, front side 7, rear side 8, air admission hole
9th, parachute 10, the first interlayer 11, the second interlayer 12.
Specific embodiment
The embodiment of technical solutions of the utility model is described in detail below in conjunction with attached drawing.Following embodiment is only
For clearly illustrating the technical solution of the utility model, therefore example is only used as, and cannot this practicality be limited with this
Novel protection domain.
In the description of the present application, it is to be understood that the orientation or position of the instructions such as term "front", "rear", " interior ", " outer "
Relationship is put as orientation or position relationship based on the user for putting on flying suit, is for only for ease of description the utility model and letter
Change description, therefore it is not intended that limitation to the utility model.
In addition, term " first ", " second " etc. are only used for description purpose, and it is not intended that indicating or implying relatively important
Property or the implicit quantity for indicating indicated technical characteristic." multiple " are meant that two in the description of the present invention,
More than, unless otherwise specifically defined.
In this application unless specifically defined or limited otherwise, term " installation ", " connected ", " connection ", " fixation " etc.
Term should be interpreted broadly, for example, it may be being fixedly connected or being detachably connected or integral；Can be that machinery connects
It connects or is electrically connected；It can be directly connected, can also be indirectly connected by intermediary, can be in two elements
The connection in portion or the interaction relationship of two elements.It for the ordinary skill in the art, can be according to specific feelings
Condition understands concrete meaning of the above-mentioned term in the utility model.
As shown in Figure 1, Figure 2, shown in Fig. 3, Fig. 4 and Fig. 5, the utility model includes the garment body 5 being adapted with human body, in institute
It states between the both arms and buttocks of ontology 5 and wingspread is set between both legs, after setting is whole on rear side of 5 rear side of ontology and wingspread
6, form the first interlayer 11 between 5 rear side of ontology and wingspread and back panel 6.Multiple perforations first are offered on wingspread
The air holes 4 of interlayer 11.1 before being provided in 5 front side of the ontology, moulding and the human body front side shape of the preceding width are adapted,
In the second interlayer 12 that described preceding 1 forms the closing being located on front side of body between ontology 5.In second interlayer 12 and
The cooling gas check valve that can only be circulated from the first interlayer 11 to the second interlayer 12 is equipped between one interlayer 11 (attached drawing is not shown).When
During two 12 gassies of interlayer, the air bag of turtle shell shape is formed in front of body.Gas tube 2 on described preceding 1 is installed, is inflated
Also is provided on pipe 2 can only air inlet cooling gas check valve, the gas tube 2 is located at preceding 1 neckline.The knot of the cooling gas check valve
Structure is using the air inlet mouth structure on existing inflatable toys.
As shown in Figure 1, Figure 2, it shown in Fig. 3, Fig. 4 and Fig. 5, is rapidly entered in the second interlayer 12 for the ease of air, described preceding 1
Extend with the edge that ontology 5 is connected into the first interlayer 11, form at least one double-deck installation being located in the first interlayer 11
Portion.Each double-deck mounting portion includes front side 7 and rear side 8, the space between the front side 7 and rear side 8 with
Second interlayer 12 penetrates through, and is provided at least one air admission hole 9 on each front side 7, the cooling gas check valve is mounted on
At each air admission hole 9.There are three the bilayer mounting portions, respectively the top below both arms between both legs.In the wing
Bat 3 is equipped with and each 9 one-to-one air holes 4 of air admission hole.
Multiple small-sized parachutes 10 are installed on 6 in the rear.
For the ease of the dress of flying suit entirety, 5 front of ontology is equipped with vertical slide fastener along center line, before described
1 top can also be correspondingly provided with vertical separation, but preceding 1 lower part be still perforation namely body on front side of second
Interlayer is always an entirety, and even if the forepart of preceding 1 is equipped with vertical separation, is still presented in front of body after inflation
Left and right merges the turtle shell shape formed.Under the premise of 1 slide fastener of ontology has airtight setting, described preceding 1 can also be still using not
Entirety with cut-off rule.
Finally it should be noted that：The above various embodiments is only to illustrate the technical solution of the utility model rather than it is limited
System；Although the utility model is described in detail with reference to foregoing embodiments, those of ordinary skill in the art should
Understand：It can still modify to the technical solution recorded in foregoing embodiments either to which part or whole
Technical characteristic carries out equivalent replacement；And these modifications or replacement, this practicality that it does not separate the essence of the corresponding technical solution are new
The range of each embodiment technical solution of type, should all cover in the claim of the utility model and the range of specification.
Claims (7)
1. a kind of escape flying suit including garment body, is set between the both arms and buttocks of the ontology and between both legs
Wingspread sets whole back panel on rear side of the ontology and on rear side of wingspread, and the is formed between wingspread and back panel on rear side of the ontology
One interlayer offers multiple air holes on wingspread, it is characterised in that：Width before being provided on front side of the ontology, in preceding width and this
The second interlayer of the closing being located on front side of body is formed between body, being equipped between second interlayer and the first interlayer can only be from
The cooling gas check valve that first interlayer circulates to the second interlayer.
2. escape flying suit according to claim 1, it is characterised in that：The edge that the preceding width is connected with ontology is to
Extend in one interlayer, form at least one double-deck mounting portion being located in the first interlayer, each double-deck mounting portion includes
Front side width and rear side width, the space between the front side width and rear side width is penetrated through with the second interlayer, on each front side width
At least one air admission hole is provided with, the cooling gas check valve is mounted on each air inlet position.
3. escape flying suit according to claim 2, it is characterised in that：There are three the bilayer mounting portions, is located at respectively
Top below both arms between both legs.
4. escape flying suit according to claim 3, it is characterised in that：It is equipped with and each air admission hole one on the wingspread
One corresponding air holes.
5. escape flying suit according to claim 4, it is characterised in that：When the second interlayer gassy, before body
The rectangular air bag into turtle shell shape.
6. according to the escape flying suit described in claims 1 or 2 or 3 or 4 or 5, it is characterised in that：It is equipped on the preceding width
Gas tube, also be provided on gas tube can only air inlet cooling gas check valve, the gas tube is located at preceding width neckline.
7. escape flying suit according to claim 6, it is characterised in that：Multiple parachutes are installed on width in the rear.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721565599.9U CN207545656U (en) | 2017-11-21 | 2017-11-21 | Escape flying suit |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721565599.9U CN207545656U (en) | 2017-11-21 | 2017-11-21 | Escape flying suit |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN207545656U true CN207545656U (en) | 2018-06-29 |
Family
ID=62679693
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201721565599.9U Expired - Fee Related CN207545656U (en) | 2017-11-21 | 2017-11-21 | Escape flying suit |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN207545656U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2022177788A1 (en) * | 2021-02-19 | 2022-08-25 | Mcmullin Eric William | Sail shirt |
| CN117401163A (en) * | 2023-12-14 | 2024-01-16 | 中国人民解放军空军特色医学中心 | Wearable protective equipment for parachuting training |
-
2017
- 2017-11-21 CN CN201721565599.9U patent/CN207545656U/en not_active Expired - Fee Related
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2022177788A1 (en) * | 2021-02-19 | 2022-08-25 | Mcmullin Eric William | Sail shirt |
| US11766073B2 (en) | 2021-02-19 | 2023-09-26 | Eric William McMullin | Sail shirt |
| US11849780B2 (en) | 2021-02-19 | 2023-12-26 | Eric William McMullin | Sail shirt |
| CN117401163A (en) * | 2023-12-14 | 2024-01-16 | 中国人民解放军空军特色医学中心 | Wearable protective equipment for parachuting training |
| CN117401163B (en) * | 2023-12-14 | 2024-02-09 | 中国人民解放军空军特色医学中心 | Wearable protective equipment for parachuting training |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20180629 Termination date: 20191121 |