CN109911213A - 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 PDF

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Publication number
CN109911213A
CN109911213A CN201711321555.6A CN201711321555A CN109911213A CN 109911213 A CN109911213 A CN 109911213A CN 201711321555 A CN201711321555 A CN 201711321555A CN 109911213 A CN109911213 A CN 109911213A
Authority
CN
China
Prior art keywords
seat
speed reducer
motor
aviation
rotating disc
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
Application number
CN201711321555.6A
Other languages
Chinese (zh)
Inventor
戴兰英
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.)
Zhenjiang Yiyi Intelligent Technology Co Ltd
Original Assignee
Zhenjiang Yiyi Intelligent Technology Co 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 Zhenjiang Yiyi Intelligent Technology Co Ltd filed Critical Zhenjiang Yiyi Intelligent Technology Co Ltd
Priority to CN201711321555.6A priority Critical patent/CN109911213A/en
Publication of CN109911213A publication Critical patent/CN109911213A/en
Pending legal-status Critical Current

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  • Seats For Vehicles (AREA)
  • Chairs Characterized By Structure (AREA)

Abstract

Seat is replied certainly for aviation the invention discloses a kind of, including seat and pedestal, the upside of the pedestal is arranged in the seat, the inside of the pedestal is provided with motor, speed reducer and rotating disc, the speed reducer is set to the middle part of the rotating disc, and the speed reducer is connect with the rotation plate inlaid, the bottom of the speed reducer is arranged in the motor, it is fixedly connected in the middle part of the power output end of the speed reducer and the bottom surface of the seat, the bottom surface both side of the seat is to rotating block, the inside of the rotating disc is provided with rotation slot, the rotating block is embedded in the rotation slot.It drives seat to be rotated by motor and speed reducer, seat can be made more stable when rotation by rotating disc and rotating block cooperation, the rotation that limited block can prevent seat excessive increases the comfort of seat.

Description

It is a kind of to reply seat certainly for aviation
Technical field
It is specially a kind of to reply seat certainly for aviation the present invention relates to aero seat field.
Background technique
The considerations of existing aero seat is to human body sitting posture comfort is fewer, can be realized the function that backrest is adjusted forwards, backwards Can, but the rotation of level angle can not be carried out, human body is seated is easy to produce fatigue for a long time, can also hinder oxygen in blood The metabolism of diffusion and cell, causes human muscle and ischium joint stress excessive, comfort is poor.
Summary of the invention
The purpose of the present invention is to provide a kind of for aviation from seat is replied, and solves proposed in background technique Problem.
To achieve the above object, the invention provides the following technical scheme: a kind of reply seat, including seat for aviation certainly The upside of the pedestal is arranged in chair and pedestal, the seat, and the inside of the pedestal is provided with motor, speed reducer and rotation Disk, the speed reducer is set to the middle part of the rotating disc, and the speed reducer is connect with the rotation plate inlaid, and the motor is set It sets and is fixedly connected in the middle part of the bottom of the speed reducer, the power output end of the speed reducer and the bottom surface of the seat, it is described For the bottom surface both side of seat to rotating block, the inside of the rotating disc is provided with rotation slot, and the rotating block is embedded in described turn In dynamic slot.
As a kind of preferred embodiment of the invention, the motor and speed reducer is fixedly connected by bolt, and The power intake of the speed reducer is connect with the power output end of the motor.
As a kind of preferred embodiment of the invention, limited block, institute are provided at left and right sides of the inside of the rotation slot The upper inside for stating rotation slot is provided with sensor.
As a kind of preferred embodiment of the invention, the right side of the seat is provided with control panel, the control plane Plate connects the motor and sensor by conducting wire.
As a kind of preferred embodiment of the invention, the limited block uses rubber material.
Compared with prior art, beneficial effects of the present invention: the present invention carries out seat using motor in the bottom of seat Rotation improves the stability of seat rotation by rotating block and rotating disc cooperation, and limited block can prevent seat from excessively rotating, Seat carries out the rotation of level angle, increases the comfort that passenger uses.
Detailed description of the invention
Fig. 1 is a kind of side elevational cross-section structure chart from reply seat for aviation of the present invention;
Fig. 2 is a kind of rotating disc structure chart from reply seat for aviation of the present invention.
In figure: seat 1, rotating block 2, rotating disc 3, motor 4, pedestal 5, control panel 6, speed reducer 7, limited block 8, sensing Device 9, rotation slot 10.
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.
The present invention provides a kind of technical solution referring to FIG. 1-2: a kind of to reply seat, including seat 1 certainly for aviation With pedestal 5, the upside of the pedestal 5 is arranged in the seat 1, and the inside of the pedestal 5 is provided with motor 4, speed reducer 7 and turns Moving plate 3, the speed reducer 7 is set to the middle part of the rotating disc 3, and the speed reducer 7 is inlayed with the rotating disc 3 and connect, institute The bottom that the speed reducer 7 is arranged in motor 4 is stated, the power output end of the speed reducer 7 and the bottom surface middle part of the seat 1 are solid Fixed connection, for the bottom surface both side of the seat 1 to rotating block 2, the inside of the rotating disc 3 is provided with rotation slot 10, and described turn Motion block 2 is embedded in the rotation slot 10.
As a preferred technical solution in the present embodiment, company is fixed by bolt in the motor 4 and speed reducer 7 It connects, and the power intake of the speed reducer 7 is connect with the power output end of the motor 4.The inside of the rotation slot 10 is left Right two sides are provided with limited block 8, and the upper inside of the rotation slot 10 is provided with sensor 9.The right side of the seat 1 is provided with Control panel 6, the control panel 6 connect the motor 4 and sensor 9 by conducting wire.The limited block 8 uses rubber material Matter.
Improvement of the invention is: after user is sitting on seat 1, the key on control panel 6 can be pressed with hand, Positive and negative rotation is carried out to control motor 4, motor 4 carries out reducing revolving speed raising torque by speed reducer 7 after rotating, then speed reducer 7 Seat 1 is driven to be rotated, seat 1 will drive rotating block 2 when rotation, and rotating block 2 can be revolved in rotation slot 10 Turn, improve the stability of the rotation of seat 1, while limited block 8 can be touched after rotating block 2 turns to certain angle, prevents Seat inordinate rotation is returned just if necessary to seat, is then operated by control panel 6, rotates motor 4, at this moment sensor 9 It starts to work, when rotating block 2 is displaced to 9 front side of sensor, sensor 9 sends a signal to motor 4, and so that motor 4 is stopped operating, That is restorable.
Finally, it should be noted that the foregoing is only a preferred embodiment of the present invention, it is not intended to restrict the invention, Although the present invention is described in detail referring to the foregoing embodiments, for those skilled in the art, still may be used To modify the technical solutions described in the foregoing embodiments or equivalent replacement of some of the technical features. All within the spirits and principles of the present invention, any modification, equivalent replacement, improvement and so on should be included in of the invention Within protection scope.

Claims (5)

1. a kind of reply seat, including seat (1) and pedestal (5) for aviation certainly, the seat (1) is arranged in the pedestal (5) upside, it is characterised in that: the inside of the pedestal (5) is provided with motor (4), speed reducer (7) and rotating disc (3), described Speed reducer (7) is set to the middle part of the rotating disc (3), and the speed reducer (7) is inlayed with the rotating disc (3) and connect, described Motor (4) setting is in the bottom of the speed reducer (7), the power output end of the speed reducer (7) and the bottom surface of the seat (1) Middle part is fixedly connected, and for the bottom surface both side of the seat (1) to rotating block (2), the inside of the rotating disc (3) is provided with rotation Slot (10), the rotating block (2) are embedded in the rotation slot (10).
2. it is according to claim 1 it is a kind of for aviation from replying seat, it is characterised in that: the motor (4) and subtract Fast machine (7) is fixedly connected by bolt, and the power intake of the speed reducer (7) and the power of the motor (4) are defeated Outlet connection.
3. a kind of reply seat certainly for aviation according to claim 1, it is characterised in that: the rotation slot (10) The internal left and right sides is provided with limited block (8), and the upper inside of the rotation slot (10) is provided with sensor (9).
4. a kind of reply seat certainly for aviation according to claim 1, it is characterised in that: the right side of the seat (1) Side is provided with control panel (6), and the control panel (6) connects the motor (4) and sensor (9) by conducting wire.
5. a kind of reply seat certainly for aviation according to claim 3, it is characterised in that: the limited block (8) is adopted With rubber material.
CN201711321555.6A 2017-12-12 2017-12-12 It is a kind of to reply seat certainly for aviation Pending CN109911213A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201711321555.6A CN109911213A (en) 2017-12-12 2017-12-12 It is a kind of to reply seat certainly for aviation

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201711321555.6A CN109911213A (en) 2017-12-12 2017-12-12 It is a kind of to reply seat certainly for aviation

Publications (1)

Publication Number Publication Date
CN109911213A true CN109911213A (en) 2019-06-21

Family

ID=66957941

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201711321555.6A Pending CN109911213A (en) 2017-12-12 2017-12-12 It is a kind of to reply seat certainly for aviation

Country Status (1)

Country Link
CN (1) CN109911213A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN112744359A (en) * 2021-03-03 2021-05-04 崔凯 Aircraft anti-load seat

Cited By (1)

* Cited by examiner, † Cited by third party
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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PB01 Publication
WD01 Invention patent application deemed withdrawn after publication
WD01 Invention patent application deemed withdrawn after publication

Application publication date: 20190621