CN207015591U - A kind of new aero seat - Google Patents

A kind of new aero seat Download PDF

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Publication number
CN207015591U
CN207015591U CN201720464276.4U CN201720464276U CN207015591U CN 207015591 U CN207015591 U CN 207015591U CN 201720464276 U CN201720464276 U CN 201720464276U CN 207015591 U CN207015591 U CN 207015591U
Authority
CN
China
Prior art keywords
fastener
plate
backrest
torsion spring
seat
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
CN201720464276.4U
Other languages
Chinese (zh)
Inventor
王伟
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.)
Shenzhen Maudley Aerospace Mstar Technology Ltd
Original Assignee
Shenzhen Maudley Aerospace Mstar Technology Ltd
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 Shenzhen Maudley Aerospace Mstar Technology Ltd filed Critical Shenzhen Maudley Aerospace Mstar Technology Ltd
Priority to CN201720464276.4U priority Critical patent/CN207015591U/en
Application granted granted Critical
Publication of CN207015591U publication Critical patent/CN207015591U/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

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Abstract

The utility model provides a kind of new aero seat.Including seat body, seat body includes chair leg, cushion and backrest, and return mechanism is embedded with inside seat body, and return mechanism is three stage structure, includes three pieces of supporting plates, and for connecting two torsion spring groups of three pieces of supporting plates;Three pieces of described supporting plates are respectively the upper plate, the middle plate in cushion, the lower plate in chair leg being arranged in backrest, the left and right ends of wherein middle plate are installed by two torsion spring groups, two torsion spring groups connect and reverse upper plate and lower plate respectively, the end of upper plate and lower plate is respectively arranged with fastener and lower fastener, upper plate is fixed on backrest bottom surface by upper fastener, and lower plate is fixed on the inside of chair leg by lower fastener.The utility model is simple in construction, and it is easy to make, by increasing capacitance it is possible to increase the elasticity recovery of backrest, reduces the manufacturing cost of seat, while can carry out reinforcement support to seat, improves impact resistance and security performance.

Description

A kind of new aero seat
Technical field
Aero seat equipment technical field is the utility model is related to, is related specifically to a kind of new with stronger elasticity recovery Type aero seat.
Background technology
Seat is indispensable part in train, and the resilient characteristic of backrest directly influences the ride comfort of occupant Property and then have influence on drive safety.Passenger sit down backward rear backrest when, had to the backrest spring on backrest larger Elastic deformation, the backside pressure of passenger is reduced by the deformation of backrest, therefore backrest is the portion to be played a key effect in seat One of part, its recoverability have directly influenced the comfort level of passenger.
In current aero seat, the reply of backrest is typically all to pass through mechanical structure, and its structure is more complicated, cost It is higher, and repair and change very inconvenient, while response agency can only play simple return action, for backrest It can not be supported with seat, in the case where seat receives impulsive force, be easily damaged, not possess protection for passenger and make With.
The content of the invention
Technical problem to be solved in the utility model is the defects of overcoming prior art, there is provided a kind of simple in construction, system It is easy to make, and increases the elasticity recovery of backrest, reduces the manufacturing cost of seat, while can carry out reinforcement support to seat, improves The new aero seat of impact resistance and security performance.
To achieve these goals, the utility model uses following technical scheme:
A kind of new aero seat, include seat body, seat body includes chair leg, cushion and backrest, its feature It is, return mechanism is embedded with inside seat body, and return mechanism is three stage structure, includes three pieces of supporting plates, and be used for Connect two torsion spring groups of three pieces of supporting plates;Three pieces of described supporting plates be respectively be arranged on backrest in upper plate, installed in seat Middle plate in pad, the lower plate in chair leg, wherein two torsion spring groups, two torsion spring group difference are installed in the left and right ends of middle plate Connect and reverse upper plate and lower plate, the end of upper plate and lower plate is respectively arranged with fastener and lower fastener, upper fastening Upper plate is fixed on backrest bottom surface by device, and lower plate is fixed on the inside of chair leg by lower fastener.
In such scheme, described torsion spring group includes a pair of torsion springs and is symmetrical arranged, and is connected among torsion spring by main shaft, A pair of torsion springs reverse synchronous application pressure jointly.
In such scheme, described upper fastener and lower fastener are adjustable structure, and upper fastener is used Angle between regulation upper plate and backrest, lower fastener are used to adjust the angle between lower plate and chair leg.
Principle of the present utility model is that torsion spring device is loaded into seat body, using the reset principle of torsion spring, strengthens backrest Recovery, while plank frame can also strengthen the support to seat.
The utility model is by adopting the above-described technical solution, have the advantages that:
The utility model is simple in construction, and it is easy to make, by increasing capacitance it is possible to increase the elasticity recovery of backrest, reduces being manufactured into for seat This, while reinforcement support can be carried out to seat, improve impact resistance and security performance.
Brief description of the drawings
Fig. 1 is the structure chart of the utility model embodiment;
Fig. 2 is the utility model embodiment upper plate structure chart;
Fig. 3 is the utility model embodiment lower plate structure figure;
In figure:Fastener in torsion spring group 8 in the lower plate 7 of plate 6 in the upper plate 5 of 1 chair leg, 2 cushion, 3 backrest 4 9 times fasteners, 10 times torsion spring groups.
Embodiment
In order that content of the present utility model is readily apparent understood, below according to specific embodiment and combine attached Figure, is described in further detail to the utility model.
The new aero seat as shown in Fig. 1 Fig. 2 Fig. 3, includes seat body, and seat body includes chair leg 1, cushion 2 With backrest 3, return mechanism is embedded with inside seat body, and return mechanism is three stage structure, includes three pieces of supporting plates, and use In two torsion spring groups for connecting three pieces of supporting plates;Three pieces of described supporting plates are respectively upper plate 4, the installation being arranged in backrest 3 Middle plate 5 in cushion 2, the lower plate 6 in chair leg 1, wherein two torsion spring groups are installed in the left and right ends of middle plate 5, respectively For upper torsion spring group 7 and lower torsion spring group 10, two torsion spring groups connect and reverse the end of upper plate 4 and lower plate 6, upper plate 4 and lower plate 6 respectively End is respectively arranged with fastener 8 and lower fastener 9, and upper plate 4 is fixed on the bottom surface of backrest 3, lower fastening by upper fastener 8 Lower plate 6 is fixed on the inner side of chair leg 1 by device 9.
In the present embodiment, described upper torsion spring group 7 and lower torsion spring group 10 include a pair of torsion springs and are symmetrical arranged, torsion spring Centre is connected by main shaft, and a pair of torsion springs reverse synchronous application pressure jointly.
In the present embodiment, described upper fastener 8 and lower fastener 9 are adjustable structure, upper fastener 8 For adjusting the angle between upper plate 4 and backrest 3, lower fastener 9 is used to adjust the angle between lower plate 6 and chair leg 1.
Particular embodiments described above, technical problem, technical scheme and the beneficial effect solved to the utility model are entered Further description is gone, should be understood that and the foregoing is only specific embodiment of the utility model, and do not have to In limitation the utility model, all within the spirit and principles of the utility model, any modification, equivalent substitution and improvements done Deng should be included within the scope of protection of the utility model.

Claims (3)

1. a kind of new aero seat, including seat body, seat body includes chair leg, cushion and backrest, and its feature exists In, return mechanism is embedded with inside seat body, return mechanism is three stage structure, includes three pieces of supporting plates, and for even Connect two torsion spring groups of three pieces of supporting plates;Three pieces of described supporting plates be respectively be arranged on backrest in upper plate, installed in cushion Interior middle plate, the lower plate in chair leg, wherein two torsion spring groups are installed in the left and right ends of middle plate, two torsion spring groups connect respectively Connect and reverse upper plate and lower plate, the end of upper plate and lower plate is respectively arranged with fastener and lower fastener, tightens and is fixedly mounted with Put and upper plate is fixed on backrest bottom surface, lower plate is fixed on the inside of chair leg by lower fastener.
2. new aero seat as claimed in claim 1, it is characterised in that it is symmetrical that described torsion spring group includes a pair of torsion springs Set, connected among torsion spring by main shaft, a pair of torsion springs reverse synchronous application pressure jointly.
3. new aero seat as claimed in claim 1, it is characterised in that described upper fastener and lower fastener are equal For adjustable structure, upper fastener is used to adjusting the angle between upper plate and backrest, lower fastener be used to adjusting lower plate with Angle between chair leg.
CN201720464276.4U 2017-04-28 2017-04-28 A kind of new aero seat Expired - Fee Related CN207015591U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201720464276.4U CN207015591U (en) 2017-04-28 2017-04-28 A kind of new aero seat

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201720464276.4U CN207015591U (en) 2017-04-28 2017-04-28 A kind of new aero seat

Publications (1)

Publication Number Publication Date
CN207015591U true CN207015591U (en) 2018-02-16

Family

ID=61461453

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201720464276.4U Expired - Fee Related CN207015591U (en) 2017-04-28 2017-04-28 A kind of new aero seat

Country Status (1)

Country Link
CN (1) CN207015591U (en)

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GR01 Patent grant
GR01 Patent grant
CF01 Termination of patent right due to non-payment of annual fee
CF01 Termination of patent right due to non-payment of annual fee

Granted publication date: 20180216

Termination date: 20180428