CN204279958U - A kind of arm supports frame of aircraft business class seat - Google Patents

A kind of arm supports frame of aircraft business class seat Download PDF

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Publication number
CN204279958U
CN204279958U CN201420612208.4U CN201420612208U CN204279958U CN 204279958 U CN204279958 U CN 204279958U CN 201420612208 U CN201420612208 U CN 201420612208U CN 204279958 U CN204279958 U CN 204279958U
Authority
CN
China
Prior art keywords
supports frame
arm supports
support
business class
pipe link
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
CN201420612208.4U
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Chinese (zh)
Inventor
付冲
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.)
Suzhou Huachong Precision Machinery Co Ltd
Original Assignee
Suzhou Huachong Precision Machinery 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 Suzhou Huachong Precision Machinery Co Ltd filed Critical Suzhou Huachong Precision Machinery Co Ltd
Priority to CN201420612208.4U priority Critical patent/CN204279958U/en
Application granted granted Critical
Publication of CN204279958U publication Critical patent/CN204279958U/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

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Abstract

The utility model discloses a kind of arm supports frame of aircraft business class seat, connected and composed by support and pipe link, described pipe link is bending type cross bar, adopt V-shaped structure, be arranged in the middle of two stands, described support adopts arc-shaped structure, be arranged on upper and lower two outer layer surfaces, the junction of described each support and pipe link adopts bolt to fix, by the way, not only enable very comfortable being put on arm supports frame of the arm of passenger, and integral firmness, stationarity can obtain very significantly promoting.

Description

A kind of arm supports frame of aircraft business class seat
Technical field
The utility model relates to a kind of bracing frame, particularly a kind of arm supports frame of aircraft business class seat.
Background technology
Along with improving constantly of people's living standard, aircraft to have become at present fashion, popular, the vehicle efficiently the most, and aircraft seat is requisite thing in whole aircraft, when people sit on the seat, arm is just certain to touch handrail, but the traveling comfort of common handrail, stability and fastness are general, can not bring the satisfaction of passenger 100%.
Utility model content
The technical matters that the utility model mainly solves is to provide a kind of arm supports frame of aircraft business class seat, not only enables very comfortable being put on arm supports frame of the arm of passenger, and integral firmness, stationarity can obtain very significantly promoting.
For solving the problems of the technologies described above, the technical scheme that the utility model adopts is: the arm supports frame providing a kind of aircraft business class, connected and composed by support and pipe link, described support is bending type cross bar, adopt the structure that V-shaped and perpendicular type combine, be arranged in the middle of two pipe links, described pipe link adopts arc-shaped structure.
In a preferred embodiment of the present utility model, the support of described perpendicular type structure is positioned at the angle position that arm supports frame has radian.
In another preferred embodiment of the utility model volume, the support of described V-shape structure is positioned at midway location and the outermost end position of arm supports frame.
In another preferred embodiment of the present utility model, the support of described each support and pipe link adopts high strength bolt to fix.
The beneficial effects of the utility model: it is more comfortable on arm supports frame, more natural to be that the arm of passenger is put in, and the fastness of entirety, stationarity can obtain very significantly promoting.
Accompanying drawing explanation
Fig. 1 is the utility model structural representation in a preferred embodiment.
Fig. 2 be the utility model in a better enforcement in formal figure.
In figure, each assembly and Reference numeral are respectively: 1, pipe link, and 2, bolt, 3, support.
Detailed description of the invention
Below in conjunction with accompanying drawing, preferred embodiment of the present utility model is described in detail, to make advantage of the present utility model and feature can be easier to be readily appreciated by one skilled in the art, thus more explicit defining is made to protection domain of the present utility model.
Please refer to Fig. 1 and Fig. 2 in embodiment of the present utility model, a kind of arm supports frame of aircraft business class seat, connected and composed by support and pipe link, each described support is bending type cross bar, adopt the structure that V-shape and perpendicular type combine, be arranged in the middle of two pipe links, described pipe link adopts arc-shaped structure, is arranged on outer layer surface.
Further illustrate, adopt the method that V-shape and perpendicular type combine, make integral structure more stable, vertical tremor amplitude is little, considers the traveling comfort of passenger's arm simultaneously, so adopt the pipe link of circular arc type structure at outer layer surface.
In another preferred embodiment of the present utility model, tell V-shape structure support be positioned at midway location and the outermost end connection location of arm supports frame.
Further illustrate, because V-shape form touch scope is large, and fit together, surface is straight, so should be used for the connection location that outermost end is drunk in by-level position.
In another preferred embodiment of the present utility model, the support of described perpendicular type structure is positioned at the angle position that arm supports frame has radian.
Further illustrate, due to perpendicular type Stability Analysis of Structures, after fitting together, anti-vibration, compressive resistance effect are very remarkable, so should be used for the angle position of radian.
In another preferred embodiment of the present utility model, the junction of described each support and pipe link adopts high strength bolt to fix.
Be different from prior art, after the point of connection of each support and pipe link adopts high strength bolt fixing, overall structure is more firm, not easily loose.
It is more comfortable on arm supports frame, more natural that the utility model can not only be that the arm of passenger is put in, and the fastness of entirety, stationarity can obtain very significantly promoting.
The foregoing is only embodiment of the present utility model; not thereby the scope of the claims of the present utility model is limited; every utilize the utility model specification sheets and accompanying drawing content to do equivalent structure or equivalent flow process conversion; or be directly or indirectly used in other relevant technical fields, be all in like manner included in scope of patent protection of the present utility model.

Claims (4)

1. the arm supports frame of an aircraft business class seat, it is characterized in that: connected and composed by pipe link (1) and support (3), described support (3) is bending type cross bar, adopt V-shaped structure and the interlaced mode be formed by connecting of perpendicular type structure, be arranged in the middle of two pipe links, described pipe link (1) adopts arc-shaped structure.
2. the arm supports frame of aircraft business class seat according to claim 1, is characterized in that: tell V-shape structure support be positioned at midway location and the outermost end connection location of arm supports frame.
3. the arm supports frame of aircraft business class seat according to claim 1, is characterized in that: the support of described perpendicular type structure is positioned at the angle position that arm supports frame has radian.
4. the arm supports frame of aircraft business class seat according to claim 1, is characterized in that: described each support (3) and the junction of pipe link (1) adopt high strength bolt (2) to fix.
CN201420612208.4U 2014-10-22 2014-10-22 A kind of arm supports frame of aircraft business class seat Expired - Fee Related CN204279958U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201420612208.4U CN204279958U (en) 2014-10-22 2014-10-22 A kind of arm supports frame of aircraft business class seat

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201420612208.4U CN204279958U (en) 2014-10-22 2014-10-22 A kind of arm supports frame of aircraft business class seat

Publications (1)

Publication Number Publication Date
CN204279958U true CN204279958U (en) 2015-04-22

Family

ID=52863145

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201420612208.4U Expired - Fee Related CN204279958U (en) 2014-10-22 2014-10-22 A kind of arm supports frame of aircraft business class seat

Country Status (1)

Country Link
CN (1) CN204279958U (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN104309807A (en) * 2014-10-22 2015-01-28 苏州华冲精密机械有限公司 Handrail support of business class seat of airplane

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN104309807A (en) * 2014-10-22 2015-01-28 苏州华冲精密机械有限公司 Handrail support of business class seat of airplane

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Legal Events

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

Granted publication date: 20150422

Termination date: 20151022

EXPY Termination of patent right or utility model