CN107054661A - A kind of substitute bladder type aircraft seat - Google Patents
A kind of substitute bladder type aircraft seat Download PDFInfo
- Publication number
- CN107054661A CN107054661A CN201710019592.5A CN201710019592A CN107054661A CN 107054661 A CN107054661 A CN 107054661A CN 201710019592 A CN201710019592 A CN 201710019592A CN 107054661 A CN107054661 A CN 107054661A
- Authority
- CN
- China
- Prior art keywords
- seat
- air bag
- protector
- buffer unit
- bladder type
- 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
- 230000001012 protector Effects 0.000 claims abstract description 22
- 230000015572 biosynthetic process Effects 0.000 claims abstract description 4
- 238000005452 bending Methods 0.000 claims description 3
- 230000003139 buffering effect Effects 0.000 claims description 2
- 238000009423 ventilation Methods 0.000 claims description 2
- 208000027418 Wounds and injury Diseases 0.000 abstract description 6
- 230000006378 damage Effects 0.000 abstract description 5
- 208000014674 injury Diseases 0.000 abstract description 5
- 238000010586 diagram Methods 0.000 description 2
- 230000001681 protective effect Effects 0.000 description 2
- 206010052428 Wound Diseases 0.000 description 1
- 238000007599 discharging Methods 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D11/00—Passenger or crew accommodation; Flight-deck installations not otherwise provided for
- B64D11/06—Arrangements of seats, or adaptations or details specially adapted for aircraft seats
- B64D11/0619—Arrangements of seats, or adaptations or details specially adapted for aircraft seats with energy absorbing means specially adapted for mitigating impact loads for passenger seats, e.g. at a crash
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D11/00—Passenger or crew accommodation; Flight-deck installations not otherwise provided for
- B64D11/06—Arrangements of seats, or adaptations or details specially adapted for aircraft seats
- B64D11/062—Belts or other passenger restraint means for passenger seats
- B64D11/06205—Arrangements of airbags
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D11/00—Passenger or crew accommodation; Flight-deck installations not otherwise provided for
- B64D11/06—Arrangements of seats, or adaptations or details specially adapted for aircraft seats
- B64D11/062—Belts or other passenger restraint means for passenger seats
- B64D11/06205—Arrangements of airbags
- B64D11/0621—Airbag initiation or activation means
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Seats For Vehicles (AREA)
Abstract
A kind of substitute bladder type aircraft seat, including seat, protector, buffer unit and control device；The chair back one closing space of formation of protector and seat, the seating area of seat is located in closing space, and protector is provided with the enabling area for being passed through closing space；Buffer unit is installed in closing space, and positioned at the front end of seat；Control device is connected with buffer unit, in aircraft severe jolt, and control device control buffer unit is expanded in seat front end.Due to that in aircraft severe jolt, duplicate protection can be carried out to the passenger of seat region by protector and buffer unit, so as to reduce passenger's unexpected injury, the security of passenger is added.
Description
Technical field
The present invention relates to aircraft seat technical field, and in particular to a kind of substitute bladder type aircraft seat.
Background technology
Aircraft, due to the particularity of its own, requires higher for its security performance, flown compared with other vehicles
Support chair is one of very important equipment in civil aircraft, and the security and comfortableness of seat have direct shadow to passenger
Ring.
Such as, when severe jolt occurs for aircraft, it is also possible to passenger is damaged because of the structure of seat, or even extremely
Die, therefore, design of the countries in the world to seat is all paid much attention to.
The content of the invention
For how design safety aircraft seat the problem of, the application provides a kind of substitute bladder type aircraft seat,
Including seat, in addition to protector, buffer unit and control device；
The chair back one closing space of formation of protector and seat, the seating area of seat is located in closing space, protection dress
Install the enabling area for being passed through closing space；
Buffer unit is installed in closing space, and positioned at the front end of seat；
Control device is connected with buffer unit, in aircraft severe jolt, and control device control buffer unit is expanded in seat
Chair front end.
In a kind of embodiment, protector is provided with the air-vent for being used for ventilating to closing space.
In a kind of embodiment, protector includes：Left plate, right plate, epipleural, lower side panel and front side board；
Left plate is fixedly connected on the left side of seat, and right plate is fixedly connected on the right side of seat, and epipleural is fixedly connected
In the upside of the chair back of seat, lower side panel is fixedly connected on the bottom side of seat, and front side board is fixedly connected on epipleural and lower side panel
Between；
Left plate is provided with enabling area.
In a kind of embodiment, lower side panel is L-shape, and the bending part of lower side panel is circular arc.
In a kind of embodiment, buffer unit includes air bag disk and air bag；
Air bag disk is installed on the lower section of front side board, whole space of the air bag through seat front end；
Air bag disk is connected with control device, and the passage of air bag disk is communicated in air bag.
In a kind of embodiment, control device includes vibrating sensor and control panel；
Vibrating sensor and control panel are respectively arranged on protector, the output end of vibrating sensor and control panel it is defeated
Enter end connection, the output end of control panel is connected with the input of air bag disk.
According to the substitute bladder type aircraft seat of above-described embodiment, due in aircraft severe jolt, protection can be passed through
Device and buffer unit carry out duplicate protection to the passenger of seat region, so as to reduce passenger's unexpected injury, add the peace of passenger
Quan Xing.
Brief description of the drawings
Fig. 1 is substitute bladder type aircraft seat structural representation；
Fig. 2 is armchair structure schematic diagram；
Fig. 3 is a kind of structural representation of state of buffer unit；
Fig. 4 is the structural representation of another state of buffer unit；
Fig. 5 is buffer unit use state structural representation.
Embodiment
The present invention is described in further detail below by embodiment combination accompanying drawing.
It is inevitable to jolt, vibrate in aircraft flight, rocking etc., if the design of seat is unreasonable,
It is easy to cause unexpected injury to passenger in aircraft flight, how ingehious design aircraft seat avoids occurring these accidental wounds
Evil, for the problem, this example provides a kind of substitute bladder type aircraft seat.
As shown in figure 1, the substitute bladder type aircraft seat of this example includes seat 1, protector 2, buffer unit 3 and control
Device, wherein, the chair back one closing space of formation of protector 2 and seat 1, the seating area of seat is located in the closing space,
Protector 2 is provided with the enabling area for being passed through closing space, and buffer unit 3 is installed in closing space, and before seat 1
End, control device is connected with buffer unit 3, in aircraft severe jolt, and control device control buffer unit 3 is expanded in seat 1
Front end, certain protective effect is produced to passenger, so as to reduce unexpected injury.The structure chart of seat 1 is as shown in Figure 2.
In order that passenger can experience the comfortableness of extraneous natural air simultaneously in seating area, the protector 2 of this example is set
There is the air-vent for being ventilated to the closing space, further, protector 2 includes left plate 21, right plate 22, epipleural
23rd, lower side panel 24 and front side board 25, wherein, left plate 21 is fixedly connected on the left side of seat 1, and right plate 22 is fixedly connected on seat
The right side of chair 1, epipleural 23 is fixedly connected on the upside of the chair back of seat 1, and lower side panel 24 is fixedly connected on the bottom side of seat 1,
Front side board 25 is fixedly connected between epipleural 23 and lower side panel 24, and left plate 21 is provided with enabling area, and passenger passes through left plate
Enabling area on 21 opens or closes the closing space.
Specifically, lower side panel 24 is L-shape, and its bending part is circular arc, and the one end and front side board 25 for facilitating lower side panel 24 connect
Connect, the other end is connected with the bottom side of seat 1.
The buffer unit 3 of this example includes air bag disk 31 and air bag 32, as shown in figure 3, air bag disk 31 is installed on front side board 25
Lower section, air bag 32 is through the whole space of the front end of seat 1, and air bag disk 31 is connected with control device, and the ventilation of air bag disk
Hole 33 is communicated in air bag 32, as shown in figure 4, passage 33 is located at the centre position of air bag disk 31.
Further, control device includes vibrating sensor and control panel, and vibrating sensor and control panel are respectively arranged in anti-
On protection unit 2, the input of the output end of vibrating sensor and control panel is connected, and the output end of control panel is defeated with air bag disk 31
Enter end connection.
The operation principle of the substitute bladder type aircraft seat of this example is：Passenger is entered in closing space by enabling area, seat
Enter on seat 1, and close enabling area, because protector 2 is provided with air-vent so that passenger still can enjoy in closing space
To extraneous natural air；In aircraft flight, in the event of severe jolt, vibrating sensor is by the vibration signal detected
Send to control panel, then, control panel controls air bag disk 31 by passage 33 to discharging suitable air pressure inside air bag 32 again,
Air bag 32 is set to expand in the front end of seat 1, the use state schematic diagram of buffer unit 3 as shown in figure 5, the air bag 32 expanded is to human body
The certain protective effect produced, so as to reduce the unexpected injury of severe jolt generation, because passenger periphery is wrapped by protector 2
Enclose so that air bag 32 is only capable of expanding in the space of the front end of seat 1, further, improves the buffering effect of air bag 32.
Security and comfortableness in passenger flight can be effectively improved by the substitute bladder type aircraft seat of this example, this
The substitute bladder type aircraft seat of example has certain actual application value, meanwhile, possess the function such as safe, automatic.
Use above specific case is illustrated to the present invention, is only intended to help and is understood the present invention, not to limit
The system present invention.For those skilled in the art, according to the thought of the present invention, it can also make some simple
Deduce, deform or replace.
Claims (6)
1. a kind of substitute bladder type aircraft seat, including seat, it is characterised in that also include：Protector, buffer unit and control
Device processed；
The chair back one closing space of formation of the protector and the seat, the seating area of the seat is located at the closing sky
In, the protector is provided with the enabling area for being passed through the closing space；
The buffer unit is installed in the closing space, and positioned at the front end of the seat；
The control device is connected with the buffer unit, in aircraft severe jolt, and the control device controls the buffering
Device is expanded in the seat front end.
2. substitute bladder type aircraft seat as claimed in claim 1, it is characterised in that the protector, which is provided with, to be used for institute
State the air-vent of closing space ventilation.
3. substitute bladder type aircraft seat as claimed in claim 1, it is characterised in that the protector includes：Left plate,
Right plate, epipleural, lower side panel and front side board；
The left plate is fixedly connected on the left side of the seat, and the right plate is fixedly connected on the right side of the seat, institute
The upside that epipleural is fixedly connected on the chair back of the seat is stated, the lower side panel is fixedly connected on the bottom side of the seat, institute
Front side board is stated to be fixedly connected between the epipleural and lower side panel；
The left plate is provided with the enabling area.
4. substitute bladder type aircraft seat as claimed in claim 3, it is characterised in that the lower side panel is L-shape, and it is described under
The bending part of side plate is circular arc.
5. substitute bladder type aircraft seat as claimed in claim 4, it is characterised in that the buffer unit include air bag disk and
Air bag；
The air bag disk is installed on the lower section of the front side board, whole space of the air bag through the seat front end；
The air bag disk is connected with the control device, and the passage of the air bag disk is communicated in the air bag.
6. substitute bladder type aircraft seat as claimed in claim 5, it is characterised in that the control device includes vibrating sensing
Device and control panel；
The vibrating sensor and control panel are respectively arranged on the protector, the output end of the vibrating sensor and institute
The input connection of control panel is stated, the output end of the control panel is connected with the input of the air bag disk.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710019592.5A CN107054661A (en) | 2017-01-11 | 2017-01-11 | A kind of substitute bladder type aircraft seat |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710019592.5A CN107054661A (en) | 2017-01-11 | 2017-01-11 | A kind of substitute bladder type aircraft seat |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN107054661A true CN107054661A (en) | 2017-08-18 |
Family
ID=59598855
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201710019592.5A Pending CN107054661A (en) | 2017-01-11 | 2017-01-11 | A kind of substitute bladder type aircraft seat |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN107054661A (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110097800A (en) * | 2019-04-30 | 2019-08-06 | 中北大学 | A kind of Aerospace vehicle test system and test method for simulated flight environment |
| CN110182370A (en) * | 2019-07-11 | 2019-08-30 | 苏州标图高级座椅有限公司 | A kind of aircarrier aircraft Special safety seat |
Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN2556127Y (en) * | 2002-08-20 | 2003-06-18 | 官留柱 | Safety seat with egg-type storehouse for plane |
| CN101631697A (en) * | 2007-02-07 | 2010-01-20 | 爱诺华技术发展有限公司 | Air bag system, the method for releasing that has the automotive seat of air bag system and be used for air bag system |
| WO2011110875A1 (en) * | 2010-03-11 | 2011-09-15 | GUBÁS, Gabi | Safety seat |
| WO2016041783A1 (en) * | 2014-09-15 | 2016-03-24 | Recaro Aircraft Seating Gmbh & Co. Kg | Aircraft seat device having an air bag element |
| CN105774738A (en) * | 2014-10-07 | 2016-07-20 | 现代自动车株式会社 | Rear Seat Airbag Apparatus For Vehicle And Controlling Method Of The Same |
-
2017
- 2017-01-11 CN CN201710019592.5A patent/CN107054661A/en active Pending
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN2556127Y (en) * | 2002-08-20 | 2003-06-18 | 官留柱 | Safety seat with egg-type storehouse for plane |
| CN101631697A (en) * | 2007-02-07 | 2010-01-20 | 爱诺华技术发展有限公司 | Air bag system, the method for releasing that has the automotive seat of air bag system and be used for air bag system |
| WO2011110875A1 (en) * | 2010-03-11 | 2011-09-15 | GUBÁS, Gabi | Safety seat |
| WO2016041783A1 (en) * | 2014-09-15 | 2016-03-24 | Recaro Aircraft Seating Gmbh & Co. Kg | Aircraft seat device having an air bag element |
| CN105774738A (en) * | 2014-10-07 | 2016-07-20 | 现代自动车株式会社 | Rear Seat Airbag Apparatus For Vehicle And Controlling Method Of The Same |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110097800A (en) * | 2019-04-30 | 2019-08-06 | 中北大学 | A kind of Aerospace vehicle test system and test method for simulated flight environment |
| CN110182370A (en) * | 2019-07-11 | 2019-08-30 | 苏州标图高级座椅有限公司 | A kind of aircarrier aircraft Special safety seat |
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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: 20170818 |