CN107499521A - A kind of pilot's safety guard - Google Patents
A kind of pilot's safety guard Download PDFInfo
- Publication number
- CN107499521A CN107499521A CN201710729945.0A CN201710729945A CN107499521A CN 107499521 A CN107499521 A CN 107499521A CN 201710729945 A CN201710729945 A CN 201710729945A CN 107499521 A CN107499521 A CN 107499521A
- Authority
- CN
- China
- Prior art keywords
- safety
- pilot
- cushion
- backrest
- buffer layer
- 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.)
- Pending
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D25/00—Emergency apparatus or devices, not otherwise provided for
- B64D25/08—Ejecting or escaping means
- B64D25/10—Ejector seats
Abstract
The invention discloses a kind of pilot's safety guard, including launching cradle, safety belt and transmitting set, the launching cradle is arranged on the lower section side of buffer layer, opposite side is provided with supporting leg below the buffer layer, cushion is provided with above the buffer layer, the cushion interior side is provided with the transmitting set, safety rail is provided with above the cushion, the cushion opposite side is provided with safety backrest, the safety backrest side is provided with the safety belt and headrest, the safety backrest opposite side is provided with oxygen conveying bottle, basic living allowance case is provided with below the oxygen conveying bottle, landing pack is provided with above the safety backrest.The present invention solves pilot and pilot ejection can in case of emergency gone out by launching cradle, pilot is balanced landing by parachute, gives pilot to provide living guarantee by oxygen conveying bottle, basic living allowance case, simple in construction, practical.
Description
Technical field
The present invention relates to aerospace safety apparatus field, and in particular to a kind of pilot's safety guard.
Background technology
In Aero-Space fly detection and pilot's space training, the safety of pilot is the thing of a most important thing
Feelings, with the development of society and the progress of science and technology, increasing new technology and equipment are used in protection pilot's safety
In, such as resistance to compression safety clothes, crash helmet etc., all additional safety to pilot provide necessary guarantee, in bullet
It is also pilot's essential link safely to penetrate seat this part, and traditional ejector seat can substantially meet pilot
The purpose that emergency is escaped danger is run into, but target is positioned, prolonged to pilot's offer basic living allowance during follow-up search and rescue
It is not in place that long search and rescue time etc., which is made,.
The content of the invention
The purpose of the present invention is that to solve the above problems and provides a kind of pilot's safety guard.
The present invention is achieved through the following technical solutions above-mentioned purpose：
A kind of pilot's safety guard, including launching cradle, safety belt and transmitting set, the ejection are set up
Put the opposite side below the lower section side of buffer layer, the buffer layer and be provided with supporting leg, seat is provided with above the buffer layer
Pad, the cushion interior side are provided with the transmitting set, safety rail, the cushion are provided with above the cushion
Opposite side is provided with safety backrest, and the safety backrest side is provided with the safety belt and headrest, and the safety backrest is another
Side is provided with oxygen conveying bottle, is provided with basic living allowance case below the oxygen conveying bottle, is set above the safety backrest
It is equipped with landing pack.
Preferably, the buffer layer is linked together by bolt and the supporting leg, the buffer layer by buckle with
The launching cradle is connected.
Preferably, the buffer layer is connected by screw and the cushion, and the radio emitter passes through screw
The side being fixed on inside the cushion, the safety rail are fixed by screws in above the cushion.
Preferably, the safety backrest is fixed with cushion rotation connection, and the safety belt is bolted on institute
Safety backrest side is stated, the headrest is fixed on above the safety backrest by bonding way.
Preferably, the landing pack is fastened by bolts above the safety backrest, the oxygen conveying bottle and institute
Basic living allowance case is stated to be fixed by screws on the safety backrest.
Preferably, the launching cradle controlling switch is bolted on the cushion side, and the launching cradle control is opened
Close interrelated with the launching cradle.
The beneficial effects of the present invention are：Pilot can in case of emergency gone out pilot ejection by launching cradle
Go, pilot is balanced landing by parachute, bottle is conveyed by oxygen, basic living allowance case provides life to pilot and protected
Barrier, it is simple in construction, it is practical.
Brief description of the drawings
Fig. 1 is a kind of front view of pilot's safety guard of the present invention；
Fig. 2 is a kind of top view of the front view of pilot's safety guard of the present invention；
Fig. 3 is a kind of left view of the front view of pilot's safety guard of the present invention；
Description of reference numerals is as follows：
1st, launching cradle；2nd, buffer layer；3rd, supporting leg；4th, launching cradle controlling switch；5th, cushion；6th, safety rail；7th, safety
Band；8th, rest the head on；9th, land pack；10th, safety backrest；11st, oxygen conveying bottle；12nd, basic living allowance case；13rd, radio is sent out
Emitter.
Embodiment
The invention will be further described below in conjunction with the accompanying drawings：
As shown in Figure 1, Figure 2 and Figure 3, a kind of pilot's safety guard, including launching cradle 1, safety belt 7 and wireless
Electric transmitter 13, launching cradle 1 are arranged on the lower section side of buffer layer 2, and the lower section opposite side of buffer layer 2 is provided with supporting leg 3, ejection
Frame 1 in emergency circumstances can go out ejection of the safety seat together with one piece of pilot running into, and buffer layer 2 plays the work of damping
With the top of buffer layer 2 is provided with cushion 5, and the interior side of cushion 5 is provided with transmitting set 13, and transmitting set 13 can
To send mayby, search and rescue team member can be made to lock search and rescue region as soon as possible, the top of cushion 5 is provided with safety rail
6, the opposite side of cushion 5 is provided with safety backrest 10, and the side of safety backrest 10 is provided with safety belt 7 and headrest 8, and safety belt 7 is to winged
Office staff provides safety guarantee, and the opposite side of safety backrest 10 is provided with oxygen conveying bottle 11, and the lower section of oxygen conveying bottle 11 is provided with base
This living guarantee case 12, oxygen conveying bottle 11 and basic living allowance case 12, which can effectively extend, searches and rescues the time, ensures flight
The safety of member, the top of safety backrest 10 are provided with landing pack 9, and landing pack 9 can land pilot's safety and steady.
In said structure, after pilot is sitting on safety seat, 7 are first fastened one's safety belt, when in case of emergency, passing through
Control launching cradle controlling switch 4 starts launching cradle 1 and worked, and pilot is launched away for one piece together with seat, and landing pack 9 opens
It is dynamic, pilot is steadily landed, transmitting set 13 sends mayby, and search and rescue team member can be allowed to find as soon as possible
Position, oxygen conveying bottle 11 can in emergency circumstances use running into, and basic living allowance case 12 can be supplied to pilot's base
Needed for this life, it can effectively extend and search and rescue the time, so as to provide necessary guarantee to the safety of pilot.
In order to further improve the use function of pilot's safety guard, buffer layer 2 passes through bolt and supporting leg 3
Link together, buffer layer 2 is connected by buckle and launching cradle 1, and buffer layer 2 is connected by screw and cushion 5, nothing
Line electricity emitter 13 is fixed by screws in the side inside cushion 5, and safety rail 6 is fixed by screws in the top of cushion 5, peace
Full backrest 10 is fixed with the rotation connection of cushion 2, and safety belt 7 is bolted on the side of safety backrest 10, and headrest 8 passes through bonding
Mode is fixed on the top of safety backrest 10, and landing pack 9 is fastened by bolts safety backrest 10 above, oxygen conveying bottle 11 and
Basic living allowance case 12 is fixed by screws on safety backrest 10, and launching cradle controlling switch 4 is bolted on cushion 5
Side, launching cradle controlling switch 4 and launching cradle 1 are interrelated.
The basic principles, principal features and advantages of the present 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, the original for simply illustrating the present invention described in above-described embodiment and specification
Reason, without departing from the spirit and scope of the present invention, various changes and modifications of the present invention are possible, these changes and improvements
It all fall within the protetion scope of the claimed invention.The claimed scope of the invention is by appended claims and its Xiao Wu circle
It is fixed.
Claims (6)
- A kind of 1. pilot's safety guard, it is characterised in that：Including launching cradle, safety belt and transmitting set, institute State the lower section side that launching cradle is arranged on buffer layer, opposite side is provided with supporting leg below the buffer layer, on the buffer layer Side is provided with cushion, and the cushion interior side is provided with the transmitting set, and safety is provided with above the cushion and is helped Hand, the cushion opposite side are provided with safety backrest, and the safety backrest side is provided with the safety belt and headrest, the peace Full backrest opposite side is provided with oxygen conveying bottle, and basic living allowance case, the safety are provided with below the oxygen conveying bottle Landing pack is provided with above backrest.
- A kind of 2. pilot's safety guard according to claim 1, it is characterised in that：The buffer layer passes through spiral shell Bolt is linked together with the supporting leg, and the buffer layer is connected by buckle and the launching cradle.
- A kind of 3. pilot's safety guard according to claim 1, it is characterised in that：The buffer layer passes through spiral shell Nail is connected with the cushion, and the radio emitter is fixed by screws in the side inside the cushion, the peace Full handrail is fixed by screws in above the cushion.
- A kind of 4. pilot's safety guard according to claim 1, it is characterised in that：The safety backrest and institute State cushion rotation connection to fix, the safety belt is bolted on the safety backrest side, and the headrest passes through bonding Mode is fixed on above the safety backrest.
- A kind of 5. pilot's safety guard according to claim 1, it is characterised in that：The landing pack passes through Bolt is fastened on above the safety backrest, and the oxygen conveying bottle is fixed by screws in institute with the basic living allowance case State on safety backrest.
- A kind of 6. pilot's safety guard according to claim 1, it is characterised in that：The launching cradle control is opened Pass is bolted on the cushion side, and the launching cradle controlling switch and the launching cradle are interrelated.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710729945.0A CN107499521A (en) | 2017-08-23 | 2017-08-23 | A kind of pilot's safety guard |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710729945.0A CN107499521A (en) | 2017-08-23 | 2017-08-23 | A kind of pilot's safety guard |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN107499521A true CN107499521A (en) | 2017-12-22 |
Family
ID=60692562
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201710729945.0A Pending CN107499521A (en) | 2017-08-23 | 2017-08-23 | A kind of pilot's safety guard |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN107499521A (en) |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108216645A (en) * | 2018-01-02 | 2018-06-29 | 晨龙飞机（荆门）有限公司 | A kind of aircraft escape device |
| CN110077584A (en) * | 2019-05-16 | 2019-08-02 | 贵州大学 | A kind of DCB Specimen high-rise life saving aircraft |
| CN110758745A (en) * | 2019-12-09 | 2020-02-07 | 上海工程技术大学 | Safety seat for aviation aircraft |
| CN113602505A (en) * | 2021-08-30 | 2021-11-05 | 航宇救生装备有限公司 | Ejection seat headrest assembly resisting high-speed airflow blowing |
Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB2244962B (en) * | 1990-05-03 | 1993-12-08 | Grumman Aerospace Corp | Parachute deployment system. |
| CN201729274U (en) * | 2010-05-28 | 2011-02-02 | 沈阳航空航天大学 | Shock-absorption ejection seat |
| CN102126557A (en) * | 2011-01-05 | 2011-07-20 | 张培霞 | Aerial emergency life saving system for passenger plane |
| CN104071341A (en) * | 2014-05-21 | 2014-10-01 | 苏州标图高级座椅有限公司 | Intelligent control system for aircraft seat |
| CN106956779A (en) * | 2017-05-04 | 2017-07-18 | 中国航空工业集团公司西安飞机设计研究所 | A kind of Multifunctional navigation passenger seat backrest |
-
2017
- 2017-08-23 CN CN201710729945.0A patent/CN107499521A/en active Pending
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB2244962B (en) * | 1990-05-03 | 1993-12-08 | Grumman Aerospace Corp | Parachute deployment system. |
| CN201729274U (en) * | 2010-05-28 | 2011-02-02 | 沈阳航空航天大学 | Shock-absorption ejection seat |
| CN102126557A (en) * | 2011-01-05 | 2011-07-20 | 张培霞 | Aerial emergency life saving system for passenger plane |
| CN104071341A (en) * | 2014-05-21 | 2014-10-01 | 苏州标图高级座椅有限公司 | Intelligent control system for aircraft seat |
| CN106956779A (en) * | 2017-05-04 | 2017-07-18 | 中国航空工业集团公司西安飞机设计研究所 | A kind of Multifunctional navigation passenger seat backrest |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108216645A (en) * | 2018-01-02 | 2018-06-29 | 晨龙飞机（荆门）有限公司 | A kind of aircraft escape device |
| CN110077584A (en) * | 2019-05-16 | 2019-08-02 | 贵州大学 | A kind of DCB Specimen high-rise life saving aircraft |
| CN110758745A (en) * | 2019-12-09 | 2020-02-07 | 上海工程技术大学 | Safety seat for aviation aircraft |
| CN113602505A (en) * | 2021-08-30 | 2021-11-05 | 航宇救生装备有限公司 | Ejection seat headrest assembly resisting high-speed airflow blowing |
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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 | ||
| RJ01 | Rejection of invention patent application after publication | ||
| RJ01 | Rejection of invention patent application after publication |
Application publication date: 20171222 |