CN109795709A - A kind of safety-type ejection capsule of helicopter - Google Patents
A kind of safety-type ejection capsule of helicopter Download PDFInfo
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- CN109795709A CN109795709A CN201910225108.3A CN201910225108A CN109795709A CN 109795709 A CN109795709 A CN 109795709A CN 201910225108 A CN201910225108 A CN 201910225108A CN 109795709 A CN109795709 A CN 109795709A
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- 239000002775 capsule Substances 0.000 title claims abstract description 20
- 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 claims abstract description 24
- 238000013016 damping Methods 0.000 claims description 20
- 238000007667 floating Methods 0.000 claims description 9
- 238000003491 array Methods 0.000 claims description 4
- 239000005341 toughened glass Substances 0.000 claims description 4
- 230000002146 bilateral effect Effects 0.000 claims description 2
- 238000009434 installation Methods 0.000 abstract 1
- 108010066114 cabin-2 Proteins 0.000 description 11
- 238000010586 diagram Methods 0.000 description 5
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 4
- 230000007423 decrease Effects 0.000 description 3
- 230000003313 weakening effect Effects 0.000 description 3
- 230000003321 amplification Effects 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 2
- 230000008901 benefit Effects 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- 238000003199 nucleic acid amplification method Methods 0.000 description 2
- 230000035939 shock Effects 0.000 description 2
- 230000005540 biological transmission Effects 0.000 description 1
- 238000004891 communication Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 238000004134 energy conservation Methods 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 239000007787 solid Substances 0.000 description 1
- 238000002834 transmittance Methods 0.000 description 1
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Abstract
The invention discloses a kind of safety-type ejection capsules of helicopter, including inflating pedestal, cabin, safety seat and internal layer cylinder, the top of the inflation pedestal is fixed with cabin, and cabin includes internal layer cylinder and outer layer barrel, it is connected between the internal layer cylinder and outer layer barrel uniformly through rubber short column, bottom end inside the internal layer cylinder is provided with cavity, the other end of the cavity inside is fixed with GPS locator, the output end of the GPS locator is electrically connected by the input terminal of conducting wire and single-chip microcontroller, and the output end of single-chip microcontroller is electrically connected by conducting wire and wireless signal transceiver module.The present invention passes through installation inflation pedestal and cabin, cabin includes outer layer barrel and internal layer cylinder, it is connected between outer layer barrel and internal layer cylinder uniformly through rubber short column, support spring is evenly arranged between rubber short column, convenient for improving the structural strength and compressive property of cabin, make it possible to guarantee to the greatest extent the safety of cabin.
Description
Technical field
The present invention relates to Helicopter Technology field, the safety-type ejection capsule of specially a kind of helicopter.
Background technique
Helicopter is difficult to the advantage accomplished or can not accomplished there are many other aircraft, is widely applied, in addition to logical
With helicopter, gradually developed transport helicopter, dustoff, armed helicopter, search and rescue helicopter, anti-submarine helicopter,
Communication helicopter, electronic warfare helicopter etc. specialized helicopter, it should be noted that because irresistible or human factor exists
The case where only a few, which first also will appear, goes straight up to consuming machine, and when going straight up to consuming machine, persons on board can use ejection capsule and escape
Raw, the devices such as cooperation parachute can greatly reduce casualties rate when going straight up to consuming machine, but existing ejection capsule is big
It is more that there are the following problems；
1, existing ejection capsule structural strength and compressive property are poor, not comprehensive enough to the protection of escape personnel, although and matching
Standby parachute, if but landing in water, still dangerous property；
2, the most structure of seat in such device is simple, escape personnel can not be fixed limit, mistake of the device in decline
It is easy to be generated by airflow influence in journey to jolt, keeps escape personnel injured；
3, such device does not have positioning function, and escape personnel, and this can not be recovered according to positioning by going straight up to consuming machine descendants
Class device needs to expend electric power resource when in use, is unfavorable for energy-saving and emission-reduction.
Summary of the invention
The purpose of the present invention is to provide a kind of safety-type ejection capsules of helicopter, to solve to propose in above-mentioned background technique
Existing ejection capsule structural strength and compressive property it is bad, safety is lower, seat escape personnel can not be fixed limit
Position does not have positioning function and the serious problem of power consumption.
To achieve the above object, it the invention provides the following technical scheme: a kind of safety-type ejection capsule of helicopter, including fills
The top of gas pedestal, cabin, safety seat and internal layer cylinder, the inflation pedestal is fixed with cabin, and cabin includes internal layer cylinder
Body and outer layer barrel connect between the internal layer cylinder and outer layer barrel uniformly through rubber short column, in the internal layer cylinder
The bottom end in portion is provided with cavity, and one end of cavity inside is fixed with single-chip microcontroller, and the other end of the cavity inside is fixed with GPS
Locator, and the central position of cavity inside is fixed with battery, is fixed between the battery and GPS locator wireless
Signal transmitting and receiving module, the top of the cavity is fixed with safety seat, and the bottom of safety seat is equipped with damping base, described
Bottom end inside damping base is provided with damping, and the side of the safety seat is fixed with motor, and the output end of motor
Roller is installed by shaft, fixed bandage is wound on the roller, baffle is hinged in front of the safety seat, it is described
The inside of the internal layer cylinder of safety seat two sides is respectively and fixedly provided with locker, and is wherein equipped with control panel on 1 locker, institute
The top for stating cabin is fixed with landing pack, and the top for the pack that lands is provided with umbrella opening, and the side of the cabin is equipped with door
The output end of body, the GPS locator is electrically connected by the input terminal of conducting wire and single-chip microcontroller, and the output end of single-chip microcontroller passes through
Conducting wire and wireless signal transceiver module are electrically connected.
Preferably, the two sides of the inflation pedestal are provided with floating ball, and floating ball is distributed about inflation pedestal bilateral symmetry.
Preferably, the both ends at the top of the cabin are mounted on solar panel, and the outside of solar panel is equal
It is provided with tempered glass.
Preferably, support spring is respectively and fixedly provided between the rubber short column, and support spring is in concentric with rubber short column
Circle best-fit.
Preferably, the fixed bandage is fixed with hook far from one end of motor, the safety seat far from motor one
End is provided with the link to match with hook.
Preferably, the central position inside the damping is provided with elastomeric pad, and the inside of elastomeric pad is equal
Even to be provided with through-hole, the two sides of the elastomeric pad are evenly distributed disc spring, and disc spring is in the connection arrangement of " W " type structure.
Compared with prior art, the beneficial effects of the present invention are:
(1) for the helicopter with safety-type ejection capsule by being equipped with inflation pedestal and cabin, cabin includes outer layer barrel and interior
Layer cylinder, connects between outer layer barrel and internal layer cylinder uniformly through rubber short column, is evenly arranged with support between rubber short column
Spring, rubber short column and support spring are in concentric arrays, convenient for improving the structural strength and compressive property of cabin, so that
It can guarantee the safety of cabin to the greatest extent, while device is provided with floating ball by the two sides in pedestal, so that even if dress
It sets to drop to and is also avoided that sinking in water, improve the reliability used.
(2) helicopter is provided with damping by being equipped with safety seat, the bottom end of safety seat with safety-type ejection capsule
Pedestal, the central position of the inside of damping base are arranged elastomeric pad, are equipped with through-hole in elastomeric pad, through-hole can increase bullet
Property gasket elasticity, the two sides of elastomeric pad are evenly arranged with disc spring, and disc spring is connected according to " W " shape, and disc spring is symmetrical, has
Conducive to the damping shock resistance for improving safety seat, has the function of weakening the impact force of high speed, avoid rushing due to powerful
Hitting power can cause to impact to escape personnel's body, can preferably guarantee the life security of escape personnel, while the one of safety seat
Side is provided with motor, roller, fixed bandage and hook, the other side of safety seat and is provided with the link to match with hook,
Convenient for carrying out escape personnel to tighten fixation by fixed bandage, avoid during declining since shaking of jolting makes escape personnel
It is injured.
(3) helicopter is with safety-type ejection capsule by being equipped with solar panel, battery, GPS locator, wireless
Signal transmitting and receiving module and single-chip microcontroller, solar panel are convenient for luminous energy being transformed into electric energy, by photovoltaic controller by electric current
It is transferred in battery, powers for device, be beneficial to energy conservation emission reduction, also avoiding the occurrence of power drain device can not normal use
The output end of dangerous situation, GPS locator is electrically connected by the input terminal of conducting wire and single-chip microcontroller, and the output end of single-chip microcontroller passes through
The input terminal of conducting wire and wireless signal transceiver module is electrically connected, convenient for sending the real time position of device in the prison of background terminal
Control center records the landing track of the escape compartment in real time, recovers convenient for rescue worker.
Detailed description of the invention
Fig. 1 faces the schematic diagram of the section structure for of the invention；
Fig. 2 is amplification profile structural schematic diagram at A in Fig. 1 of the invention；
Fig. 3 is amplification profile structural schematic diagram at B in Fig. 1 of the invention；
Fig. 4 is positive structure diagram of the invention；
Fig. 5 is system block diagram of the invention.
In figure: 1, inflating pedestal；2, cabin；3, rubber short column；4, locker；5, safety seat；6, link；7, it links up with；
8, internal layer cylinder；9, land pack；10, umbrella opening；11, outer layer barrel；12, baffle；13, control panel；14, damping base；15,
Support spring；16, floating ball；17, GPS locator；18, wireless signal transceiver module；19, cavity；20, battery；21, monolithic
Machine；22, fixed bandage；23, roller；24, motor；25, elastomeric pad；26, through-hole；27, disc spring；28, damping；29, door
Body；30, solar panel.
Specific embodiment
Following will be combined with the drawings in the embodiments of the present invention, and technical solution in the embodiment of the present invention carries out clear, complete
Site preparation description, it is clear that described embodiments are only a part of the embodiments of the present invention, instead of all the embodiments.It is based on
Embodiment in the present invention, it is obtained by those of ordinary skill in the art without making creative efforts every other
Embodiment shall fall within the protection scope of the present invention.
Fig. 1-5 is please referred to, a kind of embodiment provided by the invention: a kind of safety-type ejection capsule of helicopter, including inflation
The top of pedestal 1, cabin 2, safety seat 5 and internal layer cylinder 8, inflation pedestal 1 is fixed with cabin 2, and the two sides for inflating pedestal 1 are equal
It is provided with floating ball 16, and floating ball 16 is symmetrically distributed about inflation pedestal 1, so that being avoided that device drops in water
Sink, improves the reliability used, and cabin 2 includes internal layer cylinder 8 and outer layer barrel 11, internal layer cylinder 8 and outer layer cylinder
Connected between body 11 uniformly through rubber short column 3, be respectively and fixedly provided with support spring 15 between rubber short column 3, and support spring 15 with
Rubber short column 3 is in that concentric arrays make it possible to protect to the greatest extent convenient for improving the structural strength and compressive property of cabin 2
The safety of cabin 2 is demonstrate,proved, the bottom end inside internal layer cylinder 8 is provided with cavity 19, and one end inside cavity 19 is fixed with monolithic
The model of machine 21, single-chip microcontroller 21 can be AT89C51, and the other end inside cavity 19 is fixed with GPS locator 17, GPS locator
17 model can be GF07, and the central position inside cavity 19 is fixed with battery 20, battery 20 and GPS locator 17
Between be fixed with wireless signal transceiver module 18, the both ends at 2 top of cabin are mounted on solar panel 30, and solar-electricity
The outside of pond plate 30 is provided with tempered glass, and luminous energy is transformed into electric energy by solar panel 30, will by photovoltaic controller
Current transmission is powered into battery 20 for device, and energy-saving and emission-reduction are conducive to, and tempered glass is conducive to improve solar panel 30
Intensity, and do not influence light transmittance, the top of cavity 19 is fixed with safety seat 5, and the bottom of safety seat 5 is equipped with damping
Pedestal 14, the bottom end inside damping base 14 are provided with damping 28, and the central position inside damping 28 is provided with
Elastomeric pad 25, and the inside of elastomeric pad 25 is evenly arranged with through-hole 26, the two sides of elastomeric pad 25 are evenly distributed disc spring
27, and disc spring 27 is had the function of weakening the impact force of high speed, avoids being rushed due to powerful in the connection arrangement of " W " type structure
Hitting power can cause to impact to escape personnel's body, can preferably guarantee the life security of escape personnel, and the side of safety seat 5 is solid
Surely there is motor 24, the model of motor 24 can be Y90S-2, and the output end of motor 24 is equipped with roller 23, roller 23 by shaft
On be wound with fixed bandage 22, fixed bandage 22 is fixed with hook 7 far from one end of motor 24, and safety seat 5 is far from motor 24
One end be provided with and avoided with 7 links 6 that match of hook convenient for carrying out escape personnel to tighten fixation by fixation bandage
Since shaking of jolting keeps escape personnel injured during decline, the front of safety seat 5 is hinged with baffle 12, safety seat 5
The inside of the internal layer cylinder 8 of two sides is respectively and fixedly provided with locker 4, and is wherein equipped with control panel 13, cabin 2 on 1 locker 4
Top be fixed with landing pack 9, and land pack 9 top be provided with umbrella opening 10, the side of cabin 2 is equipped with door body 29,
The output end of GPS locator 17 is electrically connected by the input terminal of conducting wire and single-chip microcontroller 21, and the output end of single-chip microcontroller 21 passes through
Conducting wire and wireless signal transceiver module 18 are electrically connected.
Working principle: in use, luminous energy is transformed into electric energy by solar panel 30, it is by photovoltaic controller that electric current is defeated
It is sent in battery 20 and powers for device, be first turned on door body 29, escape personnel enters internal layer cylinder 8, and is sitting in safety seat 5
On, motor 24 drives roller 23 to rotate, and fixed bandage 22 is pulled out certain length, by the hook 7 and peace on fixed bandage 22
Link 6 on full seat 5 connects, and escape personnel is carried out to tighten fixation, while being hinged with baffle 12 before safety seat 5, is convenient for
The chest of escape personnel is limited, is avoided since shaking of jolting keeps escape personnel injured during declining, safety seat 5
Bottom end be provided with damping base 14, elastomeric pad 25, elastomeric pad 25 is arranged in the central position of the inside of damping base 14
Interior to be equipped with through-hole 26, through-hole 26 can increase the elasticity of elastomeric pad 25, and the two sides of elastomeric pad 25 are evenly arranged with disc spring 27,
Disc spring 27 is connected according to " W " shape, is conducive to the damping shock resistance for improving safety seat 5, has the impact for weakening high speed
The effect of power avoids to cause to impact to escape personnel's body due to powerful impact force, can preferably guarantee escape personnel's
Life security, after cabin 2 is ejected helicopter, the control of single-chip microcontroller 21 landing pack 9 goes out to open from umbrella opening 10, pacifies cabin 2
Full decline, connects between outer layer barrel 11 and internal layer cylinder 8 uniformly through rubber short column 3, is evenly arranged between rubber short column 3
Support spring 15, rubber short column 3 and support spring 15 are in concentric arrays, convenient for improving the structural strength of cabin 2 and resisting
Performance is pressed, makes it possible to guarantee to the greatest extent the safety of cabin 2, while device is floating by being provided in the two sides of pedestal 1
Ball 16 improves the reliability used, the output of GPS locator 17 so that being avoided that sinking device drops in water
End is electrically connected by the input terminal of conducting wire and single-chip microcontroller 21, and the output end of single-chip microcontroller 21 receives and dispatches mould by conducting wire and wireless signal
The input terminal of block 18 is electrically connected, and convenient for sending the real time position of device to the monitoring center of background terminal, record should in real time
The landing track of escape compartment, is recovered convenient for rescue worker.
It is obvious to a person skilled in the art that invention is not limited to the details of the above exemplary embodiments, Er Qie
In the case where without departing substantially from spirit or essential attributes of the invention, the present invention can be realized in other specific forms.Therefore, no matter
From the point of view of which point, the present embodiments are to be considered as illustrative and not restrictive, and the scope of the present invention is by appended power
Benefit requires rather than above description limits, it is intended that all by what is fallen within the meaning and scope of the equivalent elements of the claims
Variation is included within the present invention.Any reference signs in the claims should not be construed as limiting the involved claims.
Claims (6)
1. a kind of safety-type ejection capsule of helicopter, including inflation pedestal (1), cabin (2), safety seat (5) and internal layer cylinder
(8), it is characterised in that: the top of inflation pedestal (1) is fixed with cabin (2), and cabin (2) include internal layer cylinder (8) with
And outer layer barrel (11), it is connected between the internal layer cylinder (8) and outer layer barrel (11) uniformly through rubber short column (3), it is described
The internal bottom end of internal layer cylinder (8) is provided with cavity (19), and one end of cavity (19) inside is fixed with single-chip microcontroller (21), described
The internal other end of cavity (19) is fixed with GPS locator (17), and the central position of cavity (19) inside is fixed with electric power storage
Pond (20) is fixed with wireless signal transceiver module (18), the cavity between the battery (20) and GPS locator (17)
(19) top is fixed with safety seat (5), and the bottom of safety seat (5) is equipped with damping base (14), the damping bottom
The internal bottom end of seat (14) is provided with damping (28), and the side of the safety seat (5) is fixed with motor (24), and motor
(24) output end is equipped with roller (23) by shaft, is wound with fixed bandage (22), the safety on the roller (23)
It is hinged in front of seat (5) baffle (12), the inside of the internal layer cylinder (8) of safety seat (5) two sides is respectively and fixedly provided with storage
Object cabinet (4), and be wherein equipped with control panel (13) on 1 locker (4), the top of the cabin (2) is fixed with parachute
It wraps (9), and the top of landing pack (9) is provided with umbrella opening (10), the side of the cabin (2) is equipped with door body (29), described
The output end of GPS locator (17) is electrically connected by conducting wire and the input terminal of single-chip microcontroller (21), and the output of single-chip microcontroller (21)
End is electrically connected by conducting wire and wireless signal transceiver module (18).
2. a kind of safety-type ejection capsule of helicopter according to claim 1, it is characterised in that: the inflation pedestal (1)
Two sides be provided with floating ball (16), and floating ball (16) about inflation pedestal (1) bilateral symmetry be distributed.
3. a kind of safety-type ejection capsule of helicopter according to claim 1, it is characterised in that: at the top of the cabin (2)
Both ends be mounted on solar panel (30), and be provided with tempered glass on the outside of solar panel (30).
4. a kind of safety-type ejection capsule of helicopter according to claim 1, it is characterised in that: the rubber short column (3)
Between be respectively and fixedly provided with support spring (15), and support spring (15) and rubber short column (3) are in concentric arrays.
5. a kind of safety-type ejection capsule of helicopter according to claim 1, it is characterised in that: the fixed bandage (22)
One end far from motor (24) is fixed with hook (7), and the safety seat (5) is provided with and links up with far from the one end of motor (24)
(7) link (6) to match.
6. a kind of safety-type ejection capsule of helicopter according to claim 1, it is characterised in that: the damping (28)
Internal central position is provided with elastomeric pad (25), and the inside of elastomeric pad (25) is evenly arranged with through-hole (26), institute
State elastomeric pad (25) two sides it is evenly distributed have disc spring (27), and disc spring (27) in " W " type structure connection arrangement.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910225108.3A CN109795709B (en) | 2019-03-25 | 2019-03-25 | Safety type ejection cabin for helicopter |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910225108.3A CN109795709B (en) | 2019-03-25 | 2019-03-25 | Safety type ejection cabin for helicopter |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN109795709A true CN109795709A (en) | 2019-05-24 |
| CN109795709B CN109795709B (en) | 2024-08-02 |
Family
ID=66563075
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201910225108.3A Active CN109795709B (en) | 2019-03-25 | 2019-03-25 | Safety type ejection cabin for helicopter |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN109795709B (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112185048A (en) * | 2020-09-23 | 2021-01-05 | 袁文莹 | Forest fire monitoring rod |
| CN113997896A (en) * | 2021-10-09 | 2022-02-01 | 易显智能科技有限责任公司 | Automobile for guaranteeing safety of passengers |
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|---|---|---|---|---|
| US20080128555A1 (en) * | 2006-05-15 | 2008-06-05 | Airbus France | Ejection device, ejectable hatch and aircraft having at least one ejectable hatch |
| WO2015199567A1 (en) * | 2014-06-27 | 2015-12-30 | Rînea Tiberiu Emil Ilie | Method and apparatus for deploying a parachute from falling helicopters, aircraft and land vehicles and for aerial braking |
| CN107487450A (en) * | 2016-06-13 | 2017-12-19 | 金进 | Aircraft bottom electromagnetic launch supervising device |
| CN107487454A (en) * | 2017-07-03 | 2017-12-19 | 丁兆源 | A kind of preposition synchronous steam-operating automatically controls single-stage vapor ejector |
| CN208119441U (en) * | 2018-04-09 | 2018-11-20 | 秦睿桢 | A kind of unmanned plane falls descending lifeline |
| CN209600834U (en) * | 2019-03-25 | 2019-11-08 | 张天祥 | A kind of safety-type ejection capsule of helicopter |
-
2019
- 2019-03-25 CN CN201910225108.3A patent/CN109795709B/en active Active
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20080128555A1 (en) * | 2006-05-15 | 2008-06-05 | Airbus France | Ejection device, ejectable hatch and aircraft having at least one ejectable hatch |
| WO2015199567A1 (en) * | 2014-06-27 | 2015-12-30 | Rînea Tiberiu Emil Ilie | Method and apparatus for deploying a parachute from falling helicopters, aircraft and land vehicles and for aerial braking |
| CN107487450A (en) * | 2016-06-13 | 2017-12-19 | 金进 | Aircraft bottom electromagnetic launch supervising device |
| CN107487454A (en) * | 2017-07-03 | 2017-12-19 | 丁兆源 | A kind of preposition synchronous steam-operating automatically controls single-stage vapor ejector |
| CN208119441U (en) * | 2018-04-09 | 2018-11-20 | 秦睿桢 | A kind of unmanned plane falls descending lifeline |
| CN209600834U (en) * | 2019-03-25 | 2019-11-08 | 张天祥 | A kind of safety-type ejection capsule of helicopter |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112185048A (en) * | 2020-09-23 | 2021-01-05 | 袁文莹 | Forest fire monitoring rod |
| CN113997896A (en) * | 2021-10-09 | 2022-02-01 | 易显智能科技有限责任公司 | Automobile for guaranteeing safety of passengers |
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| Publication number | Publication date |
|---|---|
| CN109795709B (en) | 2024-08-02 |
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Effective date of registration: 20240403 Address after: No. 148, Hefeng West Road, Hefeng Town, Lishui District, Nanjing City, Jiangsu Province, 211200 Applicant after: Nanjing Xiangyuan Aviation Technology Co.,Ltd. Country or region after: China Address before: 272100 No. 502, Row 5, No. 59, Xichenghuangmiao Street, Yanzhou District, Jining City, Shandong Province Applicant before: Zhang Tianxiang Country or region before: China |
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