CN202935401U - Aviation folding trolley - Google Patents

Aviation folding trolley Download PDF

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Publication number
CN202935401U
CN202935401U CN 201220635722 CN201220635722U CN202935401U CN 202935401 U CN202935401 U CN 202935401U CN 201220635722 CN201220635722 CN 201220635722 CN 201220635722 U CN201220635722 U CN 201220635722U CN 202935401 U CN202935401 U CN 202935401U
Authority
CN
China
Prior art keywords
aviation
framework
trolley
layer plate
folded bicycle
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
CN 201220635722
Other languages
Chinese (zh)
Inventor
史旭东
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 LUXIANG AVIATION EQUIPMENT CO Ltd
Original Assignee
SUZHOU LUXIANG AVIATION EQUIPMENT 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 LUXIANG AVIATION EQUIPMENT CO Ltd filed Critical SUZHOU LUXIANG AVIATION EQUIPMENT CO Ltd
Priority to CN 201220635722 priority Critical patent/CN202935401U/en
Application granted granted Critical
Publication of CN202935401U publication Critical patent/CN202935401U/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

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Abstract

The utility model relates to the technical field of aviation dining equipment, in particular to an aviation folding trolley. The top of a framework is connected with a top plate through a rotary component, a cotter pin for fixing the top plate is positioned on the rotary component, a middle layer plate is arranged in the middle of the framework, a bottom layer plate is arranged at the lower portion of the middle layer plate, location mechanisms are arranged at the lower portions of the middle layer plate and the bottom layer plate, trundles are arranged at the bottom of the framework, and brakes are arranged on the trundles. The top plate is not grooved to be fixed so as to remain attractiveness of the folding trolley and reduce the folded size of the folding trolley. Due to the location mechanisms, when the folding trolley is unfolded, trolley type location can be guaranteed, and the trolley is not prone to deform.

Description

A kind of aviation folded bicycle
Technical field
The utility model relates to the in-flight catering equipment technical field, specifically a kind of aviation folded bicycle.
Background technology
The aviation dining car is the special device of store food aboard, because the particularity of environment for use, the aviation dining car there is very strict requirement, the aviation dining car all needs folding saving the space obsolete the time, the folded bicycle of usually same model all in the above on plate perforate fix, not attractive in appearance, when folded bicycle is folded up, size is bigger than normal, and is when folded bicycle launches, loaded down with trivial details without fixed mechanism or fixed mechanism.
Therefore, designing for the deficiency that overcomes above-mentioned technology can not perforate on panel, keep the attractive in appearance and folded bicycle of folded bicycle to fold up rear size less, easily place and with a kind of aviation folded bicycle of fixed mechanism, contriver's problem to be solved just.
Summary of the invention
For the deficiencies in the prior art, the purpose of this utility model is to provide a kind of aviation folded bicycle, it is simple in structure, easy to use, can not perforate on panel, it is less that the attractive in appearance and folded bicycle of maintenance folded bicycle is folded up rear size, easily places and with fixed mechanism, extraordinary practical value arranged.
The technical scheme that its technical matters that solves the utility model adopts is: a kind of aviation folded bicycle, comprise framework, top board, turning unit, la m, bottom plate, castor, brake, spring cotter, it is characterized in that: described frame roof is connected with top board by turning unit, be provided with on turning unit for the fixing spring cotter of top board, the centre of framework is provided with la m, the la m bottom is equipped with the bottom plate, bottom at la m and bottom plate is provided with detent mechanism, bottom at framework is equipped with castor, and brake is installed on castor.
The beneficial effects of the utility model are:
1, not be used on upper plate fluting fixing, kept the attractive in appearance of folded bicycle;
2, reduced the size that folded bicycle is folded up;
3, when folded bicycle is opened, detent mechanism is arranged, guarantee the vehicle location when folded bicycle launches, not yielding;
Description of drawings
Fig. 1 is the utility model structural representation.
Description of reference numerals: 1-framework; The 2-top board; The 3-turning unit; The 4-la m; 5-bottom plate; The 6-castor; The 7-brake; The 8-spring cotter; The 9-detent mechanism.
The specific embodiment
Below in conjunction with specific embodiment, further set forth the utility model, should be understood that these embodiment only are used for explanation the utility model and are not used in restriction scope of the present utility model.Should be understood that in addition those skilled in the art can make various changes or modifications the utility model after the content of having read the utility model instruction, these equivalent form of values drop on application appended claims limited range equally.
Fig. 1 is a kind of aviation of the utility model folding car structure schematic diagram, comprise framework 1, top board 2, turning unit 3, la m 4, bottom plate 5, castor 6, brake 7, spring cotter 8, detent mechanism 9, described framework 1 top is connected with top board 2 by turning unit 3, be provided with on turning unit 3 for the fixing spring cotter 8 of top board 2, the centre of framework 1 is provided with la m 4, la m 4 bottoms are equipped with bottom plate 5, bottom at la m 4 and bottom plate 5 is provided with detent mechanism 9, in the bottom of framework 1, castor 6 is installed, brake 7 is installed on castor 6.
The utility model, noting be used in slots on upper plate 2 fixes, and has kept the attractive in appearance of folded bicycle, has reduced the size that folded bicycle is folded up, and when folded bicycle is opened, by detent mechanism 9 designs are arranged, guarantees that the vehicle when folded bicycle launches is located, not yielding.

Claims (1)

1. aviation folded bicycle, comprise framework, top board, turning unit, la m, bottom plate, castor, brake, spring cotter, it is characterized in that: described frame roof is connected with top board by turning unit, be provided with on turning unit for the fixing spring cotter of top board, the centre of framework is provided with la m, and the la m bottom is equipped with the bottom plate, is provided with detent mechanism in the bottom of la m and bottom plate, bottom at framework is equipped with castor, and brake is installed on castor.
CN 201220635722 2012-11-28 2012-11-28 Aviation folding trolley Expired - Fee Related CN202935401U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN 201220635722 CN202935401U (en) 2012-11-28 2012-11-28 Aviation folding trolley

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN 201220635722 CN202935401U (en) 2012-11-28 2012-11-28 Aviation folding trolley

Publications (1)

Publication Number Publication Date
CN202935401U true CN202935401U (en) 2013-05-15

Family

ID=48319656

Family Applications (1)

Application Number Title Priority Date Filing Date
CN 201220635722 Expired - Fee Related CN202935401U (en) 2012-11-28 2012-11-28 Aviation folding trolley

Country Status (1)

Country Link
CN (1) CN202935401U (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN113602333A (en) * 2021-08-26 2021-11-05 苏州鹭翔航空设备有限公司 General aviation folding vehicle

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN113602333A (en) * 2021-08-26 2021-11-05 苏州鹭翔航空设备有限公司 General aviation folding vehicle
CN113602333B (en) * 2021-08-26 2022-06-28 苏州鹭翔航空设备有限公司 General aviation folding vehicle

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Legal Events

Date Code Title Description
C14 Grant of patent or utility model
GR01 Patent grant
CF01 Termination of patent right due to non-payment of annual fee

Granted publication date: 20130515

Termination date: 20211128

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