CN107097960A - It is a kind of to reply seat certainly for aviation - Google Patents
It is a kind of to reply seat certainly for aviation Download PDFInfo
- Publication number
- CN107097960A CN107097960A CN201710214499.XA CN201710214499A CN107097960A CN 107097960 A CN107097960 A CN 107097960A CN 201710214499 A CN201710214499 A CN 201710214499A CN 107097960 A CN107097960 A CN 107097960A
- Authority
- CN
- China
- Prior art keywords
- seat
- seat support
- aviation
- rotary shaft
- support
- 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
- 239000000463 material Substances 0.000 claims abstract description 14
- 230000003115 biocidal effect Effects 0.000 claims abstract description 6
- 230000005484 gravity Effects 0.000 claims description 5
- 230000001133 acceleration Effects 0.000 claims description 3
- 238000009825 accumulation Methods 0.000 claims description 2
- 230000000694 effects Effects 0.000 abstract description 7
- 230000009286 beneficial effect Effects 0.000 abstract description 3
- 210000003414 extremity Anatomy 0.000 description 6
- 238000010586 diagram Methods 0.000 description 4
- 206010016256 fatigue Diseases 0.000 description 3
- 238000004079 fireproofing Methods 0.000 description 3
- 238000012423 maintenance Methods 0.000 description 3
- 230000000844 anti-bacterial effect Effects 0.000 description 2
- 239000003242 anti bacterial agent Substances 0.000 description 1
- 229940088710 antibiotic agent Drugs 0.000 description 1
- 238000005452 bending Methods 0.000 description 1
- 244000309466 calf Species 0.000 description 1
- 239000000969 carrier Substances 0.000 description 1
- 230000007812 deficiency Effects 0.000 description 1
- 230000003111 delayed effect Effects 0.000 description 1
- 238000013461 design Methods 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 230000005802 health problem Effects 0.000 description 1
- 238000011835 investigation Methods 0.000 description 1
- 210000003141 lower extremity Anatomy 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 230000008520 organization Effects 0.000 description 1
- 230000002035 prolonged effect Effects 0.000 description 1
- 238000011160 research 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
- B64D11/0627—Seats combined with storage means
- B64D11/0629—Seats combined with storage means the storage means being specially adapted for emergency equipment
-
- 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
- B64D11/0639—Arrangements of seats, or adaptations or details specially adapted for aircraft seats with features for adjustment or converting of seats
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Special Chairs (AREA)
Abstract
The present invention relates to aviation interior trim field there is provided it is a kind of for aviation from replying seat, including the chair back, seat support, handrail, rotary shaft, for by seat support be returned to vertical position from response agency, support bar, base, life-saving enclosing；Seat support is fixed on the rotary shaft, and seat support can rotate, rotary shaft is fastenedly connected close to seat-back position, rotary shaft with base under response agency control around rotary shaft between horizontal level and vertical position；Support bar is arranged under seat support, is fixedly connected with base；Life-saving enclosing is arranged under seat support, is movably connected with the base.Beneficial effects of the present invention are：Seat support can be automatically replied, and automatically replying mechanism can take various ways to realize, activity limbs place is provided for passenger；Seat support, the chair back use flame-proof antibiotic material, are repeatedly once cleaned after flight；Handrail is integrated with entertainment systems and chair back layback governor motion, meets occupant comfort and entertainment requirements.
Description
Technical field
It is more particularly to a kind of to reply seat certainly for aviation the present invention relates to aviation interior trim field.
Background technology
At present, the seat support of the passenger seat of airline carriers of passengers can not all be turned down using fixed structure, i.e. seat support, can not be replied,
It is non-movable.Shown according to the investigation of International Civil Aviation Organization, for the passenger of long-range flight, its satisfaction it is minimum be to get over
Carry out more crowded seat.Research shows, the coach passenger for taking long-distance flight more focuses on health problem in-flight, expects to gather around
There are more activities and space of stretching one's legs.During long-range flight or after aircraft landing, passenger, which is more likely to stand up, suitably to be walked
It is dynamic lower for a long time in the both legs for stretching or bending to rest, and the non-movable seat support that can not be turned down turns into this idea of passenger
The huge obstacle of realization, standing up can all think that calf is withstood by seat forward position, and prolonged flight is unfavorable for passenger
It is healthy.
The content of the invention
The purpose of the present invention is exactly to overcome the deficiencies in the prior art to be used for the reply seat, chair certainly of aviation there is provided a kind of
Seat can be turned down, can automatically replied, and there is provided greater room for limb activity when being easy to the passenger to fly for long-distance.
The present invention it is a kind of for aviation from replying seat, including the chair back, seat support, handrail, in addition to rotary shaft, for will
The seat support be returned to vertical position from response agency, support bar, base, life-saving enclosing；
The seat support is fixed in the rotary shaft, and the seat support can be under the control from response agency, around the rotation
Axle rotates between horizontal level and vertical position, and the rotary shaft is close to the seat-back position, the rotary shaft and the bottom
Seat is fastenedly connected；
The support bar is arranged under the seat support, is fixedly connected with the base；
The life-saving enclosing is arranged under the seat support, is movably connected with the base.
Further, it is described from response agency be spring-return mechanism, flexure strip response agency, low resilience material links-and-links machine
Any of structure, gravity return mechanism or hydraulic accumulation energy response agency.
Further, the gravity return mechanism is sets counterweight in the seat support, and the counterweight is arranged at the branch
Between strut and the chair back.
Further, airborne synthetic recreation system is integrated with the handrail.
Further, chair back layback governor motion is provided with the handrail.
Further, the angular range of the seat support is 90-135o when the chair back is with horizontality.
Further, the chair back, seat support, the material of handrail are flame-proof antibiotic material.
Further, the seat support material meets the high intensity requirement of 16G acceleration.
Beneficial effects of the present invention are：
1st, seat support can be automatically replied, and automatically replying mechanism can take various ways to realize, activity limbs place is provided for passenger, be delayed
Solve limbs fatigue；
2nd, seat support, the chair back use fire proofing, to reach the airworthiness requirement of aircraft；
3rd, seat support, the chair back, handrail material have antibacterial characteristics, after multiple flight, it is only necessary to once clean, section
About the maintenance cost of aircraft while, greatly ensure that the health of passenger；
4th, handrail is integrated with chair back layback governor motion, and the chair back can be adjusted to human body the most comfortable with seat support into 135 ° and taken
Angle.
Brief description of the drawings
Fig. 1 show a kind of reply armchair structure schematic diagram certainly for aviation of the present invention.
Fig. 2 show the schematic diagram after adjustment backrest.
Fig. 3 show seat support and puts down schematic diagram.
Fig. 4 show seat support schematic diagram from after replying.
Wherein：The 1- chair back, 2- seat supports, 3- handrails, 4- support bars, 5- bases, 6- life-savings enclosing, 7- rotary shafts.
Embodiment
The specific embodiment of the invention is described in detail below in conjunction with specific accompanying drawing.It should be noted that in following embodiments
The combination of the technical characteristic or technical characteristic of description is not construed as isolated, and they can be mutually combined so as to reaching
To superior technique effect.In the accompanying drawing of following embodiments, the identical label that each accompanying drawing occurs represent identical feature or
Person's part, can be applied in not be the same as Example.
As shown in Figure 1-2, the embodiment of the present invention is a kind of replys seat, including the chair back 1, seat support 2, handrail certainly for aviation
3, support bar 4, base 5, life-saving enclosing 6, rotary shaft 7.Here to be introduced using gravity from exemplified by replying solution
Seat in the present embodiment replys principle certainly.The chair back 1 includes headrest and backrest two parts, and seat support 2 is based on seat support, the chair back 1
Flame-proof antibiotic material is used with seat support 2, can once clean after multiple airborne periods, greatly ensure that passenger
Health.The use of fire proofing, it is therefore intended that meet airworthiness requirement.Handrail 3 is integrated with airborne synthetic recreation system and the chair back
Layback governor motion, airborne synthetic recreation system is available for passenger to appreciate music, chair back layback regulation machine during long-range flight
Human body the most comfortable that the chair back can be adjusted to seat support into 135 ° by structure takes angle, as shown in Figure 3.Rotary shaft 7 is fastened with seat support
Install, can rotate freely, when seat support returns back to plumbness, be flipped up around rotary shaft 7.There is a support bar lower section of seat support 2
4, the supporting role to seat support is played when passenger sits down.Partial interior of the seat support 2 in the close chair back in the rear of support bar 4
Appropriate counterweight is added, when passenger stands up, seat support can automatically reply plumbness, as shown in Figure 4.Bottom is relied on below seat support
Seat 5 is provided to the overall support of seat.Be connected a U-shaped life-saving enclosing 6 forward with base, can place the things such as life vest
Product.
When passenger sits down, seat support 2 is horizontal, and the forward position of seat support 2 exceeds handrail 3, when passenger stands up, chair
Seat 2 returns back to plumbness, and the forward position of 2 distance from bottom handrail of seat support 3 also has larger space to be available for passenger's stretching exercise lower limb.
A kind of reply seat certainly for aviation that the present embodiment is provided, design meets human figure engineering principles, accorded with
Airworthiness requirement is closed, reduces the sense tired out of passenger's sitting, seat support uses flame-proof antibiotic material, meets the high intensity of 16G acceleration
It is required that, anti-biotic material has saved the maintenance cost of aircraft, it is ensured that passenger's body also provides the security of maximum while healthy,
Meet airworthiness requirement.Especially, when passenger stands, seat support returns back to upright position, and release greater room is given passenger's activity, protected
The limbs health of passenger is demonstrate,proved, this is particularly difficult for increasingly crowded aircraft passenger compartment.
Beneficial effects of the present invention are：
1. seat support can be automatically replied, automatically replying mechanism can take various ways to realize, activity limbs place is provided for passenger, delay
Solve limbs fatigue；
2. seat support, the chair back use fire proofing, to reach the airworthiness requirement of aircraft；
3. seat support, the chair back, handrail material have antibacterial characteristics, after multiple flight, it is only necessary to once clean, save
While the maintenance cost of aircraft, the health of passenger greatly ensure that；
4. handrail is integrated with chair back layback governor motion, the chair back can be adjusted to human body the most comfortable with seat support into 135 ° and take angle
Degree.
Although having been presented for several embodiments of the present invention herein, it will be appreciated by those of skill in the art that
Without departing from the spirit of the invention, the embodiments herein can be changed.Above-described embodiment be it is exemplary, no
The restriction of interest field of the present invention should be used as using the embodiments herein.
Claims (8)
1. a kind of reply seat, including the chair back, seat support, handrail certainly for aviation, it is characterised in that also including rotary shaft, uses
In by the seat support be returned to vertical position from response agency, support bar, base, life-saving enclosing；
The seat support is fixed in the rotary shaft, and the seat support can be under the control from response agency, around the rotation
Axle rotates between horizontal level and vertical position, and the rotary shaft is close to the seat-back position, the rotary shaft and the bottom
Seat is fastenedly connected；
The support bar is arranged under the seat support, is fixedly connected with the base；
The life-saving enclosing is arranged under the seat support, is movably connected with the base.
2. seat is replied certainly for aviation as claimed in claim 1, it is characterised in that described is that spring is returned from response agency
Answer a pager's call appointing in structure, flexure strip response agency, low resilience material response agency, gravity return mechanism or hydraulic accumulation energy response agency
It is a kind of.
3. seat is replied certainly for aviation as claimed in claim 1, it is characterised in that the gravity return mechanism is in institute
State and counterweight is set in seat support, the counterweight is arranged between the support bar and the chair back.
4. seat is replied certainly for aviation as claimed in claim 1, it is characterised in that be integrated with the handrail airborne comprehensive
Close entertainment systems.
5. seat is replied certainly for aviation as claimed in claim 1, it is characterised in that be provided with the handrail after the chair back
Face upward governor motion.
6. seat is replied certainly for aviation as claimed in claim 5, it is characterised in that the chair back and horizontality when institute
The angular range for stating seat support is 90-135o.
7. as described in claim any one of 1-6 be used for aviation from reply seat, it is characterised in that the chair back, seat support,
The material of handrail is flame-proof antibiotic material.
8. it is used for the reply seat certainly of aviation as described in claim any one of 1-6, it is characterised in that the seat support material is expired
The high intensity requirement of sufficient 16G acceleration.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710214499.XA CN107097960A (en) | 2017-04-01 | 2017-04-01 | It is a kind of to reply seat certainly for aviation |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710214499.XA CN107097960A (en) | 2017-04-01 | 2017-04-01 | It is a kind of to reply seat certainly for aviation |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN107097960A true CN107097960A (en) | 2017-08-29 |
Family
ID=59674830
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201710214499.XA Pending CN107097960A (en) | 2017-04-01 | 2017-04-01 | It is a kind of to reply seat certainly for aviation |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN107097960A (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107672814A (en) * | 2017-10-13 | 2018-02-09 | 中国商用飞机有限责任公司北京民用飞机技术研究中心 | A kind of ultimate control of aircraft and manipulation device and method |
| GB2580292A (en) * | 2018-10-30 | 2020-07-22 | Zodiac Seats Uk Ltd | Aircraft seat and cabin arrangement |
Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN1652709A (en) * | 2002-05-14 | 2005-08-10 | 东京座椅技术股份公司 | Vehicle seat |
| US20070145789A1 (en) * | 2005-12-22 | 2007-06-28 | Linero Luis G | Aircraft seat assembly |
| CN101291826A (en) * | 2005-10-17 | 2008-10-22 | 丰田自动车株式会社 | Seat structure, seat extension/retraction method, and vehicle |
| CN101909935A (en) * | 2008-01-17 | 2010-12-08 | 空中客车公司 | Device for stowable table and seat |
| CN104290614A (en) * | 2013-07-19 | 2015-01-21 | 株式会社塔捷斯 | Vehicle seat |
| CN207129159U (en) * | 2017-04-01 | 2018-03-23 | 中国商用飞机有限责任公司北京民用飞机技术研究中心 | It is a kind of to reply seat certainly for aviation |
-
2017
- 2017-04-01 CN CN201710214499.XA patent/CN107097960A/en active Pending
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN1652709A (en) * | 2002-05-14 | 2005-08-10 | 东京座椅技术股份公司 | Vehicle seat |
| CN101291826A (en) * | 2005-10-17 | 2008-10-22 | 丰田自动车株式会社 | Seat structure, seat extension/retraction method, and vehicle |
| US20070145789A1 (en) * | 2005-12-22 | 2007-06-28 | Linero Luis G | Aircraft seat assembly |
| CN101909935A (en) * | 2008-01-17 | 2010-12-08 | 空中客车公司 | Device for stowable table and seat |
| CN104290614A (en) * | 2013-07-19 | 2015-01-21 | 株式会社塔捷斯 | Vehicle seat |
| CN207129159U (en) * | 2017-04-01 | 2018-03-23 | 中国商用飞机有限责任公司北京民用飞机技术研究中心 | It is a kind of to reply seat certainly for aviation |
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107672814A (en) * | 2017-10-13 | 2018-02-09 | 中国商用飞机有限责任公司北京民用飞机技术研究中心 | A kind of ultimate control of aircraft and manipulation device and method |
| CN107672814B (en) * | 2017-10-13 | 2023-08-25 | 中国商用飞机有限责任公司北京民用飞机技术研究中心 | Device and method for controlling and operating aircraft final stage |
| GB2580292A (en) * | 2018-10-30 | 2020-07-22 | Zodiac Seats Uk Ltd | Aircraft seat and cabin arrangement |
| GB2580292B (en) * | 2018-10-30 | 2022-11-30 | Safran Seats Gb Ltd | Aircraft seat and cabin arrangement |
| US11518520B2 (en) | 2018-10-30 | 2022-12-06 | Safran Seats GB Limited | Aircraft seat and cabin arrangement |
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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 |
Application publication date: 20170829 |
|
| RJ01 | Rejection of invention patent application after publication |