CN205098484U - Aircraft launches system of fleing - Google Patents
Aircraft launches system of fleing Download PDFInfo
- Publication number
- CN205098484U CN205098484U CN201520858862.8U CN201520858862U CN205098484U CN 205098484 U CN205098484 U CN 205098484U CN 201520858862 U CN201520858862 U CN 201520858862U CN 205098484 U CN205098484 U CN 205098484U
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- escape compartment
- piston
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- escape
- passenger
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Abstract
The utility model provides an aircraft launches system of fleing, includes the escape compartment, the escape compartment is located the inclined to one side pro -moiety annular region of aircraft afterbody, is equipped with the several catapult between this escape compartment and the aircraft shell, and this catapult comprises piston and piston cylinder, and this piston is equipped with the piston rod inside locating the piston cylinder on this piston, and this piston rod is connected with the shell of escape compartment, the escape compartment comprises passenger's seat, mechanical core space and storage district, and the total several of passenger's seat, align to grid are in the inside of escape compartment, and the below of passenger's seat is equipped with mechanical core space, the both ends of escape compartment all are equipped with the storage district, this aircraft launches system of fleing can provide urgent protection to passenger in the passenger plane and service on buses or trains personnel when aircraft emergence accident to launch away the escape compartment, guarantee the descending of escape compartment safety under the buffering of parachute, the objective staff on board's of maximum guarantee life safety is worth wideling popularize when reducing economic loss.
Description
Technical field
The utility model relates to aviation safety field, especially a kind of airplane catapult escape system.
Background technology
Aircraft achieves the dream of mankind's flying apsaras, and drawn aircraft industry, greatly facilitate the way far away travelling of people, shorten the time of travel abroad, along with the raising of people's living standard, the development of aircraft and aircraft industry, aircraft is subject to pursuing of more and more people with its safety, traveling comfort, agility.But because increasing people selects aircraft as remote travel kit, the occurrence frequency of pernicious airplane crash is also increasing, as horse boat event.Aircraft trip is because of its particularity, and the impact being subject to environment is very large, and the fault of rugged environment and aircraft itself all may cause aircraft get out of hand, is easy to cause large area injures and deaths when running into emergency episode.Airplane crash not only, while causing tremendous economic to lose, also causes affectional dual injury to victim family members.
Utility model content
The utility model provides following technical scheme: a kind of airplane catapult escape system, comprise escape compartment, described escape compartment is positioned at airplane tail group part annular region to the front, several ejector is provided with between this escape compartment and airplane skin, this ejector is made up of piston and piston cylinder, this piston is located at piston cylinder inside, this piston is provided with piston rod, this piston rod is connected with the shell of escape compartment, piston cylinder is also provided with the chute coordinated with piston rod, sealing band is provided with in this chute, sealing bar is connected with the winding wheel in piston, the rear end of piston cylinder is provided with fuel chambers, rocket propulsion fuel is provided with in this fuel chambers, described escape compartment is made up of passenger seat, mechanical core space and warehouse district, and passenger seat has several, is evenly arranged in the inside of escape compartment, and the below of passenger seat is provided with mechanical core space, installs black box, GPS, level indicator in mechanical core space, the two ends of described escape compartment are equipped with warehouse district, are provided with parachute and oxygen canister in this warehouse district.
As further scheme of the present utility model: described escape compartment is positioned at the section position of aircraft.
As further scheme of the present utility model: the top of described passenger seat is provided with leg safety strap and upper body safety strap, and the bottom of passenger seat is provided with a storage bin, stores parachute pack and emergency medical articles for use in this storage bin.
Compared with prior art, the beneficial effects of the utility model are: this airplane catapult escape system can provide urgent protection at emergency chute to the passenger in passenger plane and crew member, and escape compartment is launched away, escape compartment safe falling is ensured under the buffering of parachute, while reducing economic loss, farthest ensure the life security of objective staff on board, be worth promoting.
Accompanying drawing explanation
Fig. 1 is rigging position schematic diagram one of the present utility model;
Fig. 2 is rigging position schematic diagram two of the present utility model;
Fig. 3 is structural representation of the present utility model;
Fig. 4 is the structural representation of ejector;
Fig. 5 is the cutaway view of ejector;
Fig. 6 is the front elevation of passenger seat;
Fig. 7 is passenger seat rear portion schematic diagram;
Fig. 8 is the utility model landing schematic diagram;
Fig. 9 is workflow diagram of the present utility model.
Detailed description of the invention
Below in conjunction with the accompanying drawing in the utility model embodiment, be clearly and completely described the technical scheme in the utility model embodiment, obviously, described embodiment is only the utility model part embodiment, instead of whole embodiments.Based on the embodiment in the utility model, those of ordinary skill in the art are not making the every other embodiment obtained under creative work prerequisite, all belong to the scope of the utility model protection.
Refer to Fig. 1-9, in the utility model embodiment, a kind of airplane catapult escape system, comprise escape compartment 1, described escape compartment 1 is positioned at aircraft 21 afterbody part annular region to the front, be in 48 section positions (a kind of segmented mode for aircaft configuration, for 737-300 type aircraft, be divided into four parts " 41 sections: head is to 360 erect-positions the chances are aeroplane nose; 43 sections: 360 erect-positions are to 540 erect-positions, and nosing is to the leading edge of a wing; 46 sections: 540 erect-positions are to 1016 erect-positions, and the leading edge of a wing is to afterbody pressure-bearing bulkhead; 48 sections: 1016 erect-positions to tail, after afterbody pressure-bearing bulkhead."), divide because conventional failure position is generally positioned at middle front part, and be generally head when aircraft 21 is out of control and rush at ground, therefore during et out of order, 48 section positions are relatively safe, several ejector 2 is provided with between described escape compartment 1 and airplane skin 22, this ejector 2 is made up of piston 201 and piston cylinder 202, it is inner that this piston 201 is located at piston cylinder 202, this piston 201 is provided with piston rod 203, this piston rod 203 is connected with the shell of escape compartment 1, piston 201 drives escape compartment 1 to depart from aircraft 21 by piston rod 203 in motion process, piston cylinder 202 is also provided with the chute 204 coordinated with piston rod 203, sealing band 205 is provided with in this chute 204, sealing bar 205 is connected with the winding wheel 206 in piston 201, in piston 201 motion process, sealing band 205 pulls out from winding wheel 206, the sealing of moment guarantee piston cylinder 202, the rear end of piston cylinder 202 is provided with fuel chambers 207, rocket propulsion fuel is provided with in this fuel chambers 207, produce pressure propelling piston 201 by rocket propulsion fuel combustion to move, rocket propulsion fuel is then responsible for whole system and provides ejection power, rocket propulsion fuel due to density large, combustion efficiency is high, pollute little, acceleration/accel is large, what can ensure escape compartment to the full extent launches efficiency.
Described escape compartment 1 is made up of passenger seat 3, mechanical core space 4 and warehouse district 5, passenger seat 3 has several, be evenly arranged in the inside of escape compartment 1, the below of passenger seat 3 is provided with mechanical core space 4, in machinery core space 4, the devices such as black box, GPS, level indicator are installed, can record flight data, and launch distress signal towards periphery, simultaneously for escape personnel carries out location, position etc.; The two ends of described escape compartment 1 are equipped with warehouse district 5, parachute and oxygen canister is provided with in this warehouse district 5, oxygen canister can ensure that passenger is at High aititude, can not produce at a high speed and suffocate, parachute then ensures that escape compartment 1 is at disengaging casing, when entering near-earth position, reduction of speed is carried out to escape compartment 1, make its stable landing.
The top of described passenger seat 3 is provided with leg safety strap 301 and upper body safety strap 302, the position such as chest, waist, leg that safety strap comprises human body is fixed, prevent under the effect of enormous impact power, related parts of human body sustains damage, the bottom of passenger seat 3 is provided with a storage bin 303, store parachute pack and emergency medical articles for use in this storage bin 303, prevent secondary injury, double protection is carried out to people.
Emergency flow process of the present utility model: one, when passenger plane et out of order, captain assigns and abandons machine order, emergency evacuation button on uncapping machine, and driving passenger enters in escape compartment 1 and awaits orders;
Two, passenger and flight attendant are sitting on escape seat subsequently, tie safety strap, the position such as chest, waist, leg that safety strap comprises human body is fixed, prevent under the effect of enormous impact power, related parts of human body sustains damage, and rear side below safety seat, stores parachute pack and emergency medical articles for use simultaneously, prevent secondary injury, double protection is carried out to people;
Three, captain checks escape compartment 1 subsequently, report to control tower, after end-of-job, captain opens escape button, and escape compartment 1 carries out startup countdown, and captain is seated in oneself position, countdown terminates, escape compartment 1 starts to launch, and rocket fuel is lighted, and piston 201 drives escape compartment 1 to accelerate fast by piston rod 203.
The utility model designs with reference to the escaping tool of fighter pilot, when generation airplane crash, can provide urgent protection, farthest ensure the life security of objective staff on board while reducing economic loss to the passenger in passenger plane and crew member.
To those skilled in the art, obvious the utility model is not limited to the details of above-mentioned one exemplary embodiment, and when not deviating from spirit of the present utility model or essential characteristic, can realize the utility model in other specific forms.Therefore, no matter from which point, all should embodiment be regarded as exemplary, and be nonrestrictive, scope of the present utility model is limited by claims instead of above-mentioned explanation, and all changes be therefore intended in the implication of the equivalency by dropping on claim and scope are included in the utility model.Any Reference numeral in claim should be considered as the claim involved by limiting.
In addition, be to be understood that, although this specification sheets is described according to embodiment, but not each embodiment only comprises an independently technical scheme, this narrating mode of specification sheets is only for clarity sake, those skilled in the art should by specification sheets integrally, and the technical scheme in each embodiment also through appropriately combined, can form other embodiments that it will be appreciated by those skilled in the art that.
Claims (3)
1. an airplane catapult escape system, comprise escape compartment (1), it is characterized in that, described escape compartment (1) is positioned at aircraft (21) afterbody part annular region to the front, several ejector (2) is provided with between this escape compartment (1) and airplane skin (22), this ejector (2) is made up of piston (201) and piston cylinder (202), it is inner that this piston (201) is located at piston cylinder (202), this piston (201) is provided with piston rod (203), this piston rod (203) is connected with the shell of escape compartment (1), piston cylinder (202) is also provided with the chute (204) coordinated with piston rod (203), sealing band (205) is provided with in this chute (204), sealing bar (205) is connected with the winding wheel (206) in piston (201), the rear end of piston cylinder (202) is provided with fuel chambers (207), this fuel chambers is provided with rocket propulsion fuel in (207), described escape compartment (1) is made up of passenger seat (3), mechanical core space (4) and warehouse district (5), passenger seat (3) is total several, be evenly arranged in the inside of escape compartment (1), the below of passenger seat (3) is provided with mechanical core space (4), installs black box, GPS, level indicator in mechanical core space (4), the two ends of described escape compartment (1) are equipped with warehouse district (5), and this warehouse district is provided with parachute and oxygen canister in (5).
2. airplane catapult escape system according to claim 1, is characterized in that, described escape compartment (1) is positioned at 48 section positions of aircraft (21).
3. airplane catapult escape system according to claim 1, it is characterized in that, the top of described passenger seat (3) is provided with leg safety strap (301) and upper body safety strap (302), the bottom of passenger seat (3) is provided with a storage bin (303), stores parachute pack and emergency medical articles for use in this storage bin (303).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520858862.8U CN205098484U (en) | 2015-10-26 | 2015-10-26 | Aircraft launches system of fleing |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520858862.8U CN205098484U (en) | 2015-10-26 | 2015-10-26 | Aircraft launches system of fleing |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205098484U true CN205098484U (en) | 2016-03-23 |
Family
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201520858862.8U Expired - Fee Related CN205098484U (en) | 2015-10-26 | 2015-10-26 | Aircraft launches system of fleing |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN205098484U (en) |
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105947223A (en) * | 2016-05-05 | 2016-09-21 | 莫国斌 | Split airplane |
| CN106081126A (en) * | 2016-06-13 | 2016-11-09 | 王晨 | Bionical cellular active safety escape compartment embeds application and the design of aviation aircraft |
| CN106781835A (en) * | 2017-01-11 | 2017-05-31 | 佛山市三水区希望火炬教育科技有限公司 | A kind of special interspace tourism vehicle model of Teenagers Popular Science Education |
| CN108216645A (en) * | 2018-01-02 | 2018-06-29 | 晨龙飞机（荆门）有限公司 | A kind of aircraft escape device |
| CN109927913A (en) * | 2019-04-26 | 2019-06-25 | 上海盛昌文化传播有限公司 | A kind of aircraft intelligent escape seat |
| CN110510126A (en) * | 2019-08-02 | 2019-11-29 | 西安飞机工业（集团）有限责任公司 | A kind of protective device and guard method of airplane catapult |
-
2015
- 2015-10-26 CN CN201520858862.8U patent/CN205098484U/en not_active Expired - Fee Related
Cited By (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105947223A (en) * | 2016-05-05 | 2016-09-21 | 莫国斌 | Split airplane |
| CN106081126A (en) * | 2016-06-13 | 2016-11-09 | 王晨 | Bionical cellular active safety escape compartment embeds application and the design of aviation aircraft |
| CN106781835A (en) * | 2017-01-11 | 2017-05-31 | 佛山市三水区希望火炬教育科技有限公司 | A kind of special interspace tourism vehicle model of Teenagers Popular Science Education |
| CN108216645A (en) * | 2018-01-02 | 2018-06-29 | 晨龙飞机（荆门）有限公司 | A kind of aircraft escape device |
| CN109927913A (en) * | 2019-04-26 | 2019-06-25 | 上海盛昌文化传播有限公司 | A kind of aircraft intelligent escape seat |
| CN109927913B (en) * | 2019-04-26 | 2023-03-24 | 上海盛昌文化传播有限公司 | Intelligent escape seat for airplane |
| CN110510126A (en) * | 2019-08-02 | 2019-11-29 | 西安飞机工业（集团）有限责任公司 | A kind of protective device and guard method of airplane catapult |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20160323 Termination date: 20171026 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |