CN206939086U - A kind of aircraft seat - Google Patents

A kind of aircraft seat Download PDF

Info

Publication number
CN206939086U
CN206939086U CN201720339425.4U CN201720339425U CN206939086U CN 206939086 U CN206939086 U CN 206939086U CN 201720339425 U CN201720339425 U CN 201720339425U CN 206939086 U CN206939086 U CN 206939086U
Authority
CN
China
Prior art keywords
backrest
base
cushion
aircraft seat
screwed
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.)
Expired - Fee Related
Application number
CN201720339425.4U
Other languages
Chinese (zh)
Inventor
韩熠鹏
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Individual
Original Assignee
Individual
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Individual filed Critical Individual
Priority to CN201720339425.4U priority Critical patent/CN206939086U/en
Application granted granted Critical
Publication of CN206939086U publication Critical patent/CN206939086U/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Landscapes

  • Seats For Vehicles (AREA)

Abstract

The utility model discloses a kind of aircraft seat,Including apparatus main body,The side of described device main body is provided with base,The top of the base is provided with backrest,The bottom of the backrest is provided with angle adjuster,And the backrest is flexibly connected with base by angle adjuster,The side of the base is provided with lean forward adjustment switch and hypsokinesis adjustment switch,And the adjustment of leaning forward switchs and hypsokinesis adjustment switch is connected with angle adjuster signal,This kind of aircraft seat,The side of backrest is provided with automatic recoverer for recovering and latch box,Using bolt-type safety belt,Enough guarantees can be provided for the safety of passenger,And the both sides of backing cushion are separately installed with left side protection pad and right side protection pad,The security performance of this kind of aircraft seat can be improved again while ride experience is provided for passenger,Top is also equipped with top shield pillow,The brain of passenger can effectively be protected,The comfort level that passenger takes this kind of aircraft seat can be improved simultaneously.

Description

A kind of aircraft seat
Technical field
The technical field of the seat is the utility model is related to, specially a kind of aircraft seat.
Background technology
So-called seat, course refers to the product that can be used on the similar vehicles such as automobile or aircraft, and people pass through The various vehicles are ridden instead of walk, and seat can then provide a comfortable rest environment for journey, while also can be passenger Safety certain guarantee is provided, everybody is most commonly that aircraft seat, automotive seat, bus seat etc., with science and technology Development, seat is also more and more, and function is also stronger and stronger, and wherein aircraft is also more with seat.
But existing aircraft seat poor safety performance, it is impossible to which enough safety guarantee, and comfort level are provided for passenger Also it has been short of, narrow space, the space for placing small article is not provided for passenger.
So how to design a kind of aircraft seat, turning into us will currently solve the problems, such as.
Utility model content
The purpose of this utility model is to provide a kind of aircraft seat, asked with solve to propose in above-mentioned background technology Topic.
To achieve the above object, the utility model provides following technical scheme:A kind of aircraft seat, including device master Body, the side of described device main body are provided with base, and the top of the base is provided with backrest, and the bottom installation of the backrest is angled Adjuster, and the backrest is flexibly connected with base by angle adjuster, the side of the base is provided with the adjustment switch that leans forward Adjust and switch with hypsokinesis, and the adjustment of leaning forward switchs and hypsokinesis adjustment switch is connected with angle adjuster signal, it is described to lean on Back of the body side is provided with automatic recoverer for recovering, and the automatic recoverer for recovering welds with backrest, and the side of the backrest is provided with latch box, And the latch box and backrest weld, the bottom of the backrest is provided with the fixed handrail in right side, and the right side fix handrail with Backrest is screwed connection, and the side of the backrest is provided with angle fixer, and the angle fixer welds with backrest Connect, cushion is installed at the top of the base, and the cushion is screwed with base and is connected, the inside peace of the cushion Equipped with heating cushion, and the heating cushion is screwed with cushion and is connected, and the side of the cushion is provided with backing cushion, and described Backing cushion is screwed with backrest and is connected, and the side of the backing cushion is provided with right side protection pad, and the right side protection pad with Backing cushion is screwed connection, and the side of the backing cushion is provided with left side protection pad, and the left side protection pad and backing cushion Connection is screwed, the bottom of the base is provided with bottom plate, and the bottom plate and tube chamber welds with base, the bottom of the bottom plate Support frame is installed, and the bottom plate welds with support frame, the bottom of the bottom plate is provided with connecting shaft and bracket, and the bottom plate It is fixedly connected with bracket by connecting shaft, battery, and described device main body and storage battery is installed at the top of the bracket Property connection, the side of the bottom plate is provided with bottom baffle, and the bottom plate and bottom baffle welding.
Further, the side of the base is provided with parcel tray, and the parcel tray is screwed company with base Connect.
Further, the side of the automatic recoverer for recovering is provided with fixing band and latch, and the latch and automatic recoverer for recovering It is flexibly connected by fixing band.
Further, left armrests are installed, and the left armrests pass through with backrest at the top of the angle fixer Angle fixer is flexibly connected.
Further, the top of the backing cushion is provided with top shield pillow, and top shield pillow passes through screw with backing cushion It is fixedly connected.
Further, the bottom of the bottom baffle is provided with connection hinge and foot pad frame, and the bottom baffle and foot pad Frame is flexibly connected by connecting hinge.
Compared with prior art, the beneficial effects of the utility model are:This kind of aircraft seat, the side of backrest are provided with Automatic recoverer for recovering and latch box, using bolt-type safety belt, enough guarantees, and backrest can be provided for the safety of passenger The both sides of pad are separately installed with left side protection pad and right side protection pad, can be improved again while ride experience is provided for passenger The security performance of this kind of aircraft seat, top are also equipped with top shield pillow, can effectively protect the brain of passenger, while can The comfort level that passenger takes this kind of aircraft seat is improved, heating cushion is installed inside cushion, heating effect, bottom can be played Be also equipped with foot pad frame, can convenient for children and old man take, improve security.
Brief description of the drawings
Fig. 1 is overall structure diagram of the present utility model;
Fig. 2 is cushion partial structural diagram of the present utility model;
Fig. 3 is bottom plate partial structural diagram of the present utility model;
Fig. 4 is bottom baffle partial structural diagram of the present utility model;
In figure:1- device bodies;2- bases;3- parcel trays;Fixed handrail on the right side of 4-;5- backrests;6- latches;7- is fixed Band;8- automatic recoverer for recovering;9- bottom plates;10- latch boxes;11- left armrests;12-, which leans forward, adjusts switch;13- hypsokinesis adjustment switch; 14- angle adjusters;15- angle fixers;16- cushions;17- heating cushions;Protection pad on the right side of 18-;19- backing cushions;Protected on the left of 20- Pad;Shield pillow at the top of 21-;22- support frames;23- connecting shafts;24- batteries;25- brackets;26- bottom baffles;27- connection hinges; 28- foot pad framves.
Embodiment
Below in conjunction with the accompanying drawing in the utility model embodiment, the technical scheme in the embodiment of the utility model is carried out Clearly and completely describing, it is clear that described embodiment is only the utility model part of the embodiment, rather than whole Embodiment.Based on the embodiment in the utility model, those of ordinary skill in the art are not under the premise of creative work is made The every other embodiment obtained, belong to the scope of the utility model protection.
Fig. 1-4 are referred to, the utility model provides a kind of technical scheme:A kind of aircraft seat, including apparatus main body 1, The side of described device main body 1 is provided with base 2, and the top of the base 2 is provided with backrest 5, and the bottom of the backrest 5 is provided with angle Adjuster 14 is spent, and the backrest 5 is flexibly connected with base 2 by angle adjuster 14, the side of the base 2, which is provided with, leans forward Adjustment switch 12 and hypsokinesis adjustment switch 13, and described lean forward adjustment switch 12 and hypsokinesis adjustment switch 13 and angle adjuster 14 signals connect, and the side of backrest 5 is provided with automatic recoverer for recovering 8, and the automatic recoverer for recovering 8 welds with backrest 5, described to lean on The side of the back of the body 5 is provided with latch box 10, and the latch box 10 welds with backrest 5, and the bottom of the backrest 5 is provided with right side admittedly Determine handrail 4, and right side fixation handrail 4 is screwed with backrest 5 and is connected, the side installation of the backrest 5 is angled Fixator 15, and the angle fixer 15 welds with backrest 5, the top of the base 2 is provided with cushion 16, and the cushion 16 are screwed with base 2 and are connected, and the inside of the cushion 16 is provided with heating cushion 17, and the heating cushion 17 and cushion 16 are screwed connection, and the side of the cushion 16 is provided with backing cushion 19, and the backing cushion 19 passes through screw with backrest 5 It is fixedly connected, the side of the backing cushion 19 is provided with right side protection pad 18, and the right side protection pad 18 passes through spiral shell with backing cushion 19 Silk is fixedly connected, and the side of the backing cushion 19 is provided with left side protection pad 20, and the left side protection pad 20 passes through with backing cushion 19 Screw is fixedly connected, and the bottom of the base 2 is provided with bottom plate 9, and the bottom plate 9 welds with base 2, the bottom of the bottom plate 9 Portion is provided with support frame 22, and the bottom plate 9 welds with support frame 22, and the bottom of the bottom plate 9 is provided with connecting shaft 23 and bracket 25, and the bottom plate 9 is fixedly connected with bracket 25 by connecting shaft 23, the top of the bracket 25 is provided with battery 24, and Described device main body 1 is electrically connected with battery 24, and the side of the bottom plate 9 is provided with bottom baffle 26, and the bottom plate 9 and bottom Portion's baffle plate 26 welds.
Further, the side of the base 2 is provided with parcel tray 3, and the parcel tray 3 is consolidated with base 2 by screw Fixed connection, the parcel tray 3 can facilitate passenger to place article, improve the practicality of product.
Further, the side of the automatic recoverer for recovering 8 is provided with fixing band 7 and latch 6, and the latch 6 returns with automatic Receive device 8 to be flexibly connected by fixing band 7, the automatic recoverer for recovering 8 can improve the security performance of product.
Further, the top of the angle fixer 15 is provided with left armrests 11, and the left armrests 11 are with leaning on The back of the body 5 is flexibly connected by angle fixer 15, and setting angle fixator 15 can improve 11 practicality of left armrests.
Further, the top of the backing cushion 19 is provided with top shield pillow 21, and top shield pillow 21 and backing cushion 19 Connection is screwed, installation top shield pillow 21 can effectively protect passenger's brain, improve the security of product.
Further, the bottom of the bottom baffle 26 is provided with connection hinge 27 and foot pad frame 28, and the bottom baffle 26 are flexibly connected with foot pad frame 28 by being connected hinge 27, and installation foot poppet 28 enhances the feature of product, moreover it is possible to which raising multiplies The comfort of visitor.
Operation principle:First, passenger is sitting on this kind of aircraft seat with correct posture, and latch 6 is reclaimed from automatic 8 inner extraction of device, is inserted into the latch box 10 on the left of backrest, and latch 6 is flexibly connected with automatic recoverer for recovering 8 by fixing band 7, Fixed passenger's sitting posture can be played a part of, provide guarantee for the safety of passenger, the left side of apparatus main body 1, which is provided with, leans forward Adjustment switch 12 and hypsokinesis adjustment switch 13, adjustment switch 12 and the control angle adjustment of hypsokinesis adjustment switch 13 of leaning forward can be passed through Device 14, so as to adjust the angle of backrest 5, the right side of cushion 16 is provided with parcel tray 3, and passenger can put the small article carried with Enter in parcel tray 3, left armrests 11 are separately installed with left and right sides of cushion and handrail 4 is fixed on right side, it is possible to increase passenger's relaxes Appropriateness, while the security performance of this kind of aircraft seat can be also improved, passenger can be as desired by angle fixer 15 Adjust the angle of left armrests 11.
While there has been shown and described that embodiment of the present utility model, for the ordinary skill in the art, It is appreciated that these embodiments can be carried out with a variety of changes in the case where not departing from principle of the present utility model and spirit, repaiied Change, replace and modification, the scope of the utility model are defined by the appended claims and the equivalents thereof.

Claims (6)

1. a kind of aircraft seat, including apparatus main body (1), it is characterised in that:The side of described device main body (1) is provided with base (2), the top of the base (2) is provided with backrest (5), and the bottom of the backrest (5) is provided with angle adjuster (14), and described Backrest (5) is flexibly connected with base (2) by angle adjuster (14), and the side of the base (2) is provided with the adjustment switch that leans forward (12) switch (13) is adjusted with hypsokinesis, and described leans forward adjustment switch (12) and hypsokinesis adjustment switchs (13) and angle adjuster (14) signal connects, and backrest (5) side is provided with automatic recoverer for recovering (8), and the automatic recoverer for recovering (8) and backrest (5) Welding, the side of the backrest (5) is provided with latch box (10), and the latch box (10) welds with backrest (5), the backrest (5) bottom is provided with the fixed handrail (4) in right side, and handrail (4) and backrest (5) company of being screwed are fixed in the right side Connect, the side of the backrest (5) is provided with angle fixer (15), and the angle fixer (15) welds with backrest (5), institute State and cushion (16) is installed at the top of base (2), and the cushion (16) is screwed with base (2) and is connected, the seat The inside of pad (16) is provided with heating cushion (17), and the heating cushion (17) is screwed with cushion (16) and is connected, described The side of cushion (16) is provided with backing cushion (19), and the backing cushion (19) is screwed with backrest (5) and is connected, described to lean on The side of back pad (19) is provided with right side protection pad (18), and the right side protection pad (18) and backing cushion (19) company of being screwed Connect, the side of the backing cushion (19) is provided with left side protection pad (20), and the left side protection pad (20) passes through with backing cushion (19) Screw is fixedly connected, and the bottom of the base (2) is provided with bottom plate (9), and the bottom plate (9) welds with base (2), the bottom The bottom of plate (9) is provided with support frame (22), and the bottom plate (9) welds with support frame (22), and the bottom of the bottom plate (9) is set There are connecting shaft (23) and bracket (25), and the bottom plate (9) is fixedly connected with bracket (25) by connecting shaft (23), the bracket (25) battery (24) is installed, and described device main body (1) is electrically connected with battery (24), the bottom plate (9) at the top of Side be provided with bottom baffle (26), and the bottom plate (9) welds with bottom baffle (26).
A kind of 2. aircraft seat according to claim 1, it is characterised in that:The side of the base (2) is provided with storage Thing box (3), and the parcel tray (3) is screwed with base (2) and is connected.
A kind of 3. aircraft seat according to claim 1, it is characterised in that:The side of the automatic recoverer for recovering (8) is set There are fixing band (7) and latch (6), and the latch (6) is flexibly connected with automatic recoverer for recovering (8) by fixing band (7).
A kind of 4. aircraft seat according to claim 1, it is characterised in that:The top peace of the angle fixer (15) Equipped with left armrests (11), and the left armrests (11) are flexibly connected with backrest (5) by angle fixer (15).
A kind of 5. aircraft seat according to claim 1, it is characterised in that:The top of the backing cushion (19) is provided with top Portion's shield pillow (21), and top shield pillow (21) is screwed with backing cushion (19) and is connected.
A kind of 6. aircraft seat according to claim 1, it is characterised in that:The bottom of the bottom baffle (26) is provided with Hinge (27) and foot pad frame (28) are connected, and the bottom baffle (26) connects with foot pad frame (28) by being connected hinge (27) activity Connect.
CN201720339425.4U 2017-04-01 2017-04-01 A kind of aircraft seat Expired - Fee Related CN206939086U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201720339425.4U CN206939086U (en) 2017-04-01 2017-04-01 A kind of aircraft seat

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201720339425.4U CN206939086U (en) 2017-04-01 2017-04-01 A kind of aircraft seat

Publications (1)

Publication Number Publication Date
CN206939086U true CN206939086U (en) 2018-01-30

Family

ID=61359129

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201720339425.4U Expired - Fee Related CN206939086U (en) 2017-04-01 2017-04-01 A kind of aircraft seat

Country Status (1)

Country Link
CN (1) CN206939086U (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN110304256A (en) * 2019-07-10 2019-10-08 苏州标图高级座椅有限公司 It is a kind of can automatic swing backrest aircraft seat

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN110304256A (en) * 2019-07-10 2019-10-08 苏州标图高级座椅有限公司 It is a kind of can automatic swing backrest aircraft seat

Similar Documents

Publication Publication Date Title
EP0734901B1 (en) Vehicle seat with integrated child seat
CN204915355U (en) Car back -row seat
CN206939086U (en) A kind of aircraft seat
CN206383857U (en) Integrated automobile child safety seat
JPS57158128A (en) Headrest for car
CN105691252A (en) Child safety seat for automobile
CN207627901U (en) A kind of multiple degrees of freedom seat of racing car with attitude updating function
CN205239206U (en) Automobile seat
CN206242965U (en) A kind of automobile chair model and its chair framework
CN209600333U (en) A kind of middle row seat of automobile
CN209191745U (en) A kind of conjuncted back seat of two people
CN205523771U (en) Conjuncted car seat of four -player
CN207773486U (en) A kind of safety seat of general small-size aircraft
CN207535747U (en) A kind of Novel car seat backrest
CN206231255U (en) For the child safety seat of business car
CN106143233B (en) A kind of dedicated Riding Accommodation of baby for the vehicles
CN206067973U (en) A kind of electric bicycle children's seat
CN205930348U (en) Automobile seat
CN213734703U (en) Novel electric automobile seat with heating function
CN205417877U (en) Chair for children
CN205256101U (en) Automobile -used side direction back cushion
CN205952151U (en) Comfortable type motorcycle seat
CN214189401U (en) Anti-scalding and cooling device for automobile seat
CN207984634U (en) A kind of new energy power safety school auto use chair
CN206086451U (en) Automobile safety seat

Legal Events

Date Code Title Description
GR01 Patent grant
GR01 Patent grant
CF01 Termination of patent right due to non-payment of annual fee

Granted publication date: 20180130

Termination date: 20190401

CF01 Termination of patent right due to non-payment of annual fee