CN109050937A - A kind of adjustable lightweight aero seat - Google Patents
A kind of adjustable lightweight aero seat Download PDFInfo
- Publication number
- CN109050937A CN109050937A CN201810788121.5A CN201810788121A CN109050937A CN 109050937 A CN109050937 A CN 109050937A CN 201810788121 A CN201810788121 A CN 201810788121A CN 109050937 A CN109050937 A CN 109050937A
- Authority
- CN
- China
- Prior art keywords
- main body
- bottom plate
- seat
- seat main
- cushion
- 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
- 230000001681 protective effect Effects 0.000 claims abstract description 11
- 238000000034 method Methods 0.000 description 5
- 238000010586 diagram Methods 0.000 description 3
- 230000008901 benefit Effects 0.000 description 2
- 230000000694 effects Effects 0.000 description 2
- 239000007788 liquid Substances 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- 238000012986 modification Methods 0.000 description 2
- 239000007779 soft material Substances 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000007812 deficiency Effects 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 230000003014 reinforcing effect Effects 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
- B64D11/0639—Arrangements of seats, or adaptations or details specially adapted for aircraft seats with features for adjustment or converting of seats
-
- 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
- B64D11/064—Adjustable inclination or position of seats
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Seats For Vehicles (AREA)
Abstract
The invention discloses a kind of adjustable lightweight aero seats, including seat main body, elastic backrest is provided at the top of the seat main body, and the both ends of elastic backrest are equipped with the clamping headrest, the two sides of the seat main body are provided with protective pad, and one end of protective pad is equipped with safety belt buckle, cushion is installed below the seat main body, and cushion is internally provided with bottom plate, the two sides of the cushion are provided with baffle, and handle hand is installed on baffle, one end of the baffle is equipped with adjusting knob, one end of the bottom plate is fixedly connected by adjusting bracket with hang plate, one end of the hang plate is connected by movable rotation-shaft with bottom plate, the bottom base plate is connected by hydraulic telescopic rod with hydraulic cylinder.The problems such as the present invention by being provided with elastic backrest, adjusting knob, adjusting bracket, hang plate and hydraulic telescopic rod, it is single to solve current aero seat regulative mode, cannot carry out effective protection to astronaut.
Description
Technical field
The present invention relates to aero seat equipment technical field, specially a kind of adjustable lightweight aero seat.
Background technique
Aero seat and its crash equipment on aircraft are in-flight to ensure passenger life safety and travelling comfort
One of most important airborne equipment in key equipment, and civil aircraft project.The aircraft of earliest period is mainly used for military and postal industry
Business, there is no the requirements in terms of too many safety and comfort level to seat for aircraft at that time.Since the 1930s, aircraft is opened
Begin to become a kind of mass transportation.Thus the first generation airline passengers seat of civilian science and technology is also born, but aero seat at that time
Chair or basket chair.Since the high speed of aircraft and strong air-flow jolt, the seat on aircraft must be securely fixed.At that time
Stewardesses carry spanner and screwdriver, and chair is fixed on the floor of cabin with screw nut and reinforcing bar.If boat
Class's delay eliminates, they must adjust sliding rail, according at the time of flight and passenger number adjust the seat of aircraft.
Current aero seat regulative mode is single, cannot carry out effective protection to astronaut, be unable to satisfy the life of people
Production and application demand, therefore a kind of novel adjustable lightweight aero seat is developed in market in urgent need.
Summary of the invention
(1) the technical issues of solving
In view of the deficiencies of the prior art, the present invention provides a kind of adjustable lightweight aero seat, current aviation is solved
The problems such as seat regulative mode is single, cannot carry out effective protection to astronaut.
(2) technical solution
To achieve the above object, the invention provides the following technical scheme: a kind of adjustable lightweight aero seat, including seat
Main body, the seat main body top is provided with elastic backrest, and the both ends of elastic backrest are equipped with the clamping headrest, the seat master
The two sides of body are provided with protective pad, and one end of protective pad is equipped with safety belt buckle, is equipped with below the seat main body
Cushion, and cushion is internally provided with bottom plate, the two sides of the cushion are provided with baffle, and handle hand is equipped on baffle, institute
The one end for stating baffle is equipped with adjusting knob, and one end of the bottom plate is fixedly connected by adjusting bracket with hang plate, described to incline
One end of inclined plate is connected by movable rotation-shaft with bottom plate, and the bottom base plate is connected by hydraulic telescopic rod with hydraulic cylinder.
Preferably, the junction of the adjusting bracket and hang plate is provided with adjusting bolt.
Preferably, one end of the movable rotation-shaft is connected by fastener with adjusting knob.
Preferably, it is provided with lifting storehouse below the bottom plate, and goes up and down and hydraulic cylinder is installed inside storehouse.
Preferably, it is connected by guide post with fixing sucking disk below the lifting storehouse.
(3) beneficial effect
The present invention provides a kind of adjustable lightweight aero seat, have it is following the utility model has the advantages that
(1) present invention is turned by being provided with the clamping headrest, safety belt buckle, adjusting knob, hang plate, adjusting bracket and activity
Axis, seat main body top are provided with elastic backrest, are that soft material is made outside seat main body, people can be improved in elastic backrest
Comfort when seating has certain elastic force, can carry out ballistic support to people back, the both ends of elastic backrest are equipped with folder
The headrest is held, head can be fixed in the clamping headrest, and one end of bottom plate is fixedly connected by adjusting bracket with hang plate, hang plate
One end be connected by movable rotation-shaft with bottom plate, one end of movable rotation-shaft is connected by fastener with adjusting knob, is passed through
The rotation angle of movable rotation-shaft is controlled using adjusting knob, to change the tilt angle of hang plate, is realized to seat main body
Back tilt adjustment, operate simple and convenient；
(2) present invention passes through liquid by being provided with hydraulic telescopic rod, lifting storehouse, guide post, fixing sucking disk and hydraulic cylinder, bottom base plate
Pressure telescopic rod is connected with hydraulic cylinder, by being equipped with hydraulic cylinder, using hydraulic lifting principle, drives bottom by hydraulic telescopic rod
Plate is gone up and down, to carry out height adjustment to cushion, lifting is connected by guide post with fixing sucking disk below storehouse, fixing sucking disk
Seat main body can be securely fixed, improve the stability of seat.
Detailed description of the invention
Fig. 1 is the structural diagram of the present invention；
Fig. 2 is adjusting bracket structural schematic diagram of the invention；
Fig. 3 is lifting chamber structure schematic diagram of the invention.
In figure: 1 elastic backrest, 2 clamping the headrests, 3 protective pads, 4 safety belt buckles, 5 handle hands, 6 cushions, 7 seat main bodies,
8 baffles, 9 adjusting knobs, 10 bottom plates, 11 hang plates, 12 adjust bolt, 13 adjusting brackets, 14 movable rotation-shafts, 15 hydraulically extensibles
Bar, 16 lifting storehouses, 17 guide posts, 18 fixing sucking disks, 19 hydraulic cylinders.
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.
As shown in Figure 1-3, the present invention provides a kind of technical solution: a kind of adjustable lightweight aero seat, including seat
Chair main body 7 is provided with elastic backrest 1 at the top of seat main body 7, and the both ends of elastic backrest 1 are equipped with the clamping headrest 2, seat master
The two sides of body 7 are provided with protective pad 3, and one end of protective pad 3 is equipped with safety belt buckle 4, is equipped with below seat main body 7
Cushion 6, and cushion 6 is internally provided with bottom plate 10, the two sides of cushion 6 are provided with baffle 8, and handle hand is equipped on baffle 8
5, one end of baffle 8 is equipped with adjusting knob 9, and one end of bottom plate 10 is fixedly connected with hang plate 11 by adjusting bracket 13, is inclined
One end of inclined plate 11 is connected by movable rotation-shaft 14 with bottom plate 10, and 10 bottom of bottom plate passes through hydraulic telescopic rod 15 and hydraulic cylinder 19
It is connected, the junction of adjusting bracket 13 and hang plate 11, which is provided with, adjusts bolt 12, and one end of movable rotation-shaft 14 passes through fastening
Part is connected with adjusting knob 9, and lifting storehouse 16 is provided with below bottom plate 10, and goes up and down and be equipped with hydraulic cylinder 19 inside storehouse 16, rises
Drop is connected by guide post 17 with fixing sucking disk 18 below storehouse 16.
It is that soft material is made outside seat main body 7 in use, being provided with elastic backrest 1 at the top of seat main body 7, elasticity
Comfort when people take can be improved in backrest 1, has certain elastic force, and ballistic support, elasticity can be carried out to people back
The both ends of backrest 1 are equipped with the clamping headrest 2, and head can be fixed in the clamping headrest 2, and the two sides of seat main body 7 are provided with
Protective pad 3, one end of protective pad 3 is equipped with safety belt buckle 4, when taking seat, safety belt buckle 4 can be fastened, can
Security protection is carried out to astronaut, cushion 6 is installed below seat main body 7, cushion 6 is internally provided with bottom plate 10, bottom plate 10
One end is fixedly connected by adjusting bracket 13 with hang plate 11, and one end of hang plate 11 is connected by movable rotation-shaft 14 with bottom plate 10
It connects, one end of movable rotation-shaft 14 is connected by fastener with adjusting knob 9, and activity is controlled by using adjusting knob 9 and is turned
The rotation angle of axis 14 realizes the back tilt adjustment to seat main body 7, operation to change the tilt angle of hang plate 11
To get up simple and convenient, 10 bottom of bottom plate is connected by hydraulic telescopic rod 15 with hydraulic cylinder 19, by being equipped with hydraulic cylinder 19, benefit
With hydraulic lifting principle, bottom plate 10 is driven to be gone up and down by hydraulic telescopic rod 15, to carry out height adjustment, lifting to cushion
It is connected by guide post 17 with fixing sucking disk 18 below storehouse 16, fixing sucking disk 18 can securely fix seat main body 7, mention
The high stability of seat.
It can to sum up obtain, the present invention is by being provided with elastic backrest 1, adjusting knob 9, adjusting bracket 13, hang plate 11 and liquid
Telescopic rod 15 is pressed, it is single to solve current aero seat regulative mode, the problems such as cannot carrying out effective protection to astronaut.
It should be noted that, in this document, relational terms such as first and second and the like are used merely to a reality
Body or operation are distinguished with another entity or operation, are deposited without necessarily requiring or implying between these entities or operation
In any actual relationship or order or sequence.Moreover, the terms "include", "comprise" or its any other variant are intended to
Non-exclusive inclusion, so that the process, method, article or equipment including a series of elements is not only wanted including those
Element, but also including other elements that are not explicitly listed, or further include for this process, method, article or equipment
Intrinsic element.
It although an embodiment of the present invention has been shown and described, for the ordinary skill in the art, can be with
A variety of variations, modification, replacement can be carried out to these embodiments without departing from the principles and spirit of the present invention by understanding
And modification, the scope of the present invention is defined by the appended.
Claims (5)
1. a kind of adjustable lightweight aero seat, including seat main body (7), it is characterised in that: seat main body (7) top
Portion is provided with elastic backrest (1), and the both ends of elastic backrest (1) are equipped with and clamp the headrest (2), and the two of the seat main body (7)
Side is provided with protective pad (3), and one end of protective pad (3) is equipped with safety belt buckle (4), below the seat main body (7)
It being equipped with cushion (6), and cushion (6) is internally provided with bottom plate (10), the two sides of the cushion (6) are provided with baffle (8), and
It being equipped on baffle (8) handle hand (5), one end of the baffle (8) is equipped with adjusting knob (9), and the one of the bottom plate (10)
End is fixedly connected by adjusting bracket (13) with hang plate (11), one end of the hang plate (11) by movable rotation-shaft (14) and
Bottom plate (10) is connected, and bottom plate (10) bottom is connected by hydraulic telescopic rod (15) with hydraulic cylinder (19).
2. a kind of adjustable lightweight aero seat according to claim 1, it is characterised in that: the adjusting bracket
(13) it is provided with the junction of hang plate (11) and adjusts bolt (12).
3. a kind of adjustable lightweight aero seat according to claim 1, it is characterised in that: the movable rotation-shaft
(14) one end is connected by fastener with adjusting knob (9).
4. a kind of adjustable lightweight aero seat according to claim 1, it is characterised in that: under the bottom plate (10)
Side is provided with lifting storehouse (16), and goes up and down and be equipped with hydraulic cylinder (19) inside storehouse (16).
5. a kind of adjustable lightweight aero seat according to claim 1, it is characterised in that: the lifting storehouse (16)
Lower section is connected by guide post (17) with fixing sucking disk (18).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810788121.5A CN109050937A (en) | 2018-07-18 | 2018-07-18 | A kind of adjustable lightweight aero seat |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810788121.5A CN109050937A (en) | 2018-07-18 | 2018-07-18 | A kind of adjustable lightweight aero seat |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN109050937A true CN109050937A (en) | 2018-12-21 |
Family
ID=64817060
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201810788121.5A Pending CN109050937A (en) | 2018-07-18 | 2018-07-18 | A kind of adjustable lightweight aero seat |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN109050937A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112744359A (en) * | 2021-03-03 | 2021-05-04 | 崔凯 | Aircraft anti-load seat |
Citations (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPH07205690A (en) * | 1994-01-19 | 1995-08-08 | Kinshidou:Kk | Installation structure of seat for automobile |
| CN202414166U (en) * | 2011-12-12 | 2012-09-05 | 中国科学院对地观测与数字地球科学中心 | Fast-fixed-detached seat for aerial photograph plane |
| CN205626401U (en) * | 2016-04-20 | 2016-10-12 | 温大鹏 | Chair is diagnose to novel internal medicine based on linkage structure |
| CN205801522U (en) * | 2016-06-13 | 2016-12-14 | 郑州航空工业管理学院 | A kind of airliner seat |
| CN106414240A (en) * | 2014-04-02 | 2017-02-15 | Be航天公司 | Cradle recline mechanism for fixed-shell aircraft seat |
| DE102016219045A1 (en) * | 2015-10-01 | 2017-04-06 | Toyota Boshoku Kabushiki Kaisha | vehicle seat |
| CN206166350U (en) * | 2016-07-03 | 2017-05-17 | 广州中匠福家具有限公司 | Upholstered armchair subassembly |
| US9719768B2 (en) * | 2015-07-21 | 2017-08-01 | Honda Motor Co., Ltd. | Methods and apparatus for aligning vehicle components |
-
2018
- 2018-07-18 CN CN201810788121.5A patent/CN109050937A/en active Pending
Patent Citations (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPH07205690A (en) * | 1994-01-19 | 1995-08-08 | Kinshidou:Kk | Installation structure of seat for automobile |
| CN202414166U (en) * | 2011-12-12 | 2012-09-05 | 中国科学院对地观测与数字地球科学中心 | Fast-fixed-detached seat for aerial photograph plane |
| CN106414240A (en) * | 2014-04-02 | 2017-02-15 | Be航天公司 | Cradle recline mechanism for fixed-shell aircraft seat |
| US9719768B2 (en) * | 2015-07-21 | 2017-08-01 | Honda Motor Co., Ltd. | Methods and apparatus for aligning vehicle components |
| DE102016219045A1 (en) * | 2015-10-01 | 2017-04-06 | Toyota Boshoku Kabushiki Kaisha | vehicle seat |
| CN205626401U (en) * | 2016-04-20 | 2016-10-12 | 温大鹏 | Chair is diagnose to novel internal medicine based on linkage structure |
| CN205801522U (en) * | 2016-06-13 | 2016-12-14 | 郑州航空工业管理学院 | A kind of airliner seat |
| CN206166350U (en) * | 2016-07-03 | 2017-05-17 | 广州中匠福家具有限公司 | Upholstered armchair subassembly |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112744359A (en) * | 2021-03-03 | 2021-05-04 | 崔凯 | Aircraft anti-load 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 | ||
| WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20181221 |
|
| WD01 | Invention patent application deemed withdrawn after publication |