CN104129507A - Aircraft tire clamping and fixing device arranged on aircraft carrier deck - Google Patents

Aircraft tire clamping and fixing device arranged on aircraft carrier deck Download PDF

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Publication number
CN104129507A
CN104129507A CN201410272038.4A CN201410272038A CN104129507A CN 104129507 A CN104129507 A CN 104129507A CN 201410272038 A CN201410272038 A CN 201410272038A CN 104129507 A CN104129507 A CN 104129507A
Authority
CN
China
Prior art keywords
aircraft
fixing device
device arranged
carrier deck
tire clamping
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
CN201410272038.4A
Other languages
Chinese (zh)
Inventor
李竟儒
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 CN201410272038.4A priority Critical patent/CN104129507A/en
Publication of CN104129507A publication Critical patent/CN104129507A/en
Priority to CN201510015659.9A priority patent/CN104590580B/en
Pending legal-status Critical Current

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Abstract

The invention discloses an aircraft tire clamping and fixing device arranged on an aircraft carrier deck. Cam clamps capable of being overturned by 0 degree to 90 degrees are arranged on the two sides of an aircraft tire, and the central parts of the cam clamps are sequentially connected with a cross coupling and a double-acting type oil gas buffer into a whole. The aircraft tire clamping and fixing device arranged on the aircraft carrier deck has the advantages that in typhoon weather, an aircraft can be fixed and protected against damage, and time and labor are saved.

Description

A kind of aircraft tyre clamping and fixing device being arranged on aircraft-carrier-deck
Technical field
The present invention relates to aircraft tyre anchor fitting, specifically a kind of aircraft tyre clamping and fixing device being arranged on aircraft-carrier-deck.
Background technology
Ship-board aircraft on aircraft carrier, in the time running into typhoon, need to be fixed aircraft, and existing fixing means is to fix with many ropes, and not only labour's intensity is large, and fixed effect is not good.
Summary of the invention
The object of the invention is to provide a kind of aircraft tyre clamping and fixing device being arranged on aircraft-carrier-deck.
Realizing object scheme of the present invention is:
Being arranged on the aircraft tyre clamping and fixing device on aircraft-carrier-deck, is that the cam card that can do the upset of 0-90 degree is set in aircraft tyre both sides, and the centre of cam card and cross drive coupling, double acting oil gas bumper are linked in sequence and are integrated.
Described cross drive coupling and double acting oil gas bumper are prior art.
When use, start double acting oil gas bumper, the cam card of tire both sides is slowly risen, by cam card, aircraft tyre is fixedly clamped; While use, cam card and connected double acting oil gas bumper and deck maintain an equal level.
Advantage of the present invention is: in the time running into typhoon weather, aircraft can be fixed, not be damaged, and also time saving and energy saving.
Brief description of the drawings
Fig. 1 is the structural representation of aircraft tyre clamping and fixing device of the present invention.
In figure: 1. trapezoidal cam card 2. cross drive coupling 3. double acting oil gas bumpers.
Detailed description of the invention
With reference to Fig. 1, a kind of aircraft tyre clamping and fixing device being arranged on aircraft-carrier-deck, be that the trapezoidal cam card 1 that can do the upset of 0-90 degree is set in aircraft tyre both sides, the centre of trapezoidal cam card 1 and cross drive coupling 2, double acting oil gas bumper 3 are linked in sequence and are integrated.

Claims (1)

1. the aircraft tyre clamping and fixing device being arranged on aircraft-carrier-deck, it is characterized in that: the cam card that can do the upset of 0-90 degree is set in aircraft tyre both sides, and the centre of cam card and cross drive coupling, double acting oil gas bumper are linked in sequence and are integrated.
CN201410272038.4A 2014-06-18 2014-06-18 Aircraft tire clamping and fixing device arranged on aircraft carrier deck Pending CN104129507A (en)

Priority Applications (2)

Application Number Priority Date Filing Date Title
CN201410272038.4A CN104129507A (en) 2014-06-18 2014-06-18 Aircraft tire clamping and fixing device arranged on aircraft carrier deck
CN201510015659.9A CN104590580B (en) 2014-06-18 2015-01-13 A kind of aero tyre clamping and fixing device being arranged on aircraft-carrier-deck

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201410272038.4A CN104129507A (en) 2014-06-18 2014-06-18 Aircraft tire clamping and fixing device arranged on aircraft carrier deck

Publications (1)

Publication Number Publication Date
CN104129507A true CN104129507A (en) 2014-11-05

Family

ID=51802442

Family Applications (2)

Application Number Title Priority Date Filing Date
CN201410272038.4A Pending CN104129507A (en) 2014-06-18 2014-06-18 Aircraft tire clamping and fixing device arranged on aircraft carrier deck
CN201510015659.9A Active CN104590580B (en) 2014-06-18 2015-01-13 A kind of aero tyre clamping and fixing device being arranged on aircraft-carrier-deck

Family Applications After (1)

Application Number Title Priority Date Filing Date
CN201510015659.9A Active CN104590580B (en) 2014-06-18 2015-01-13 A kind of aero tyre clamping and fixing device being arranged on aircraft-carrier-deck

Country Status (1)

Country Link
CN (2) CN104129507A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN112644740A (en) * 2020-12-31 2021-04-13 中国科学院长春光学精密机械与物理研究所 Locking mechanism of aerospace device

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN2818424Y (en) * 2005-07-11 2006-09-20 天津港第一港埠公司 Tyre catcher on site bridge
CN201531535U (en) * 2009-05-19 2010-07-21 中国船舶重工集团公司第七○二研究所 Compact double-cross joint universal coupling
NO334631B1 (en) * 2011-11-24 2014-04-28 Marine Aluminium As Anchoring device in a helicopter deck
CN103847978A (en) * 2014-03-24 2014-06-11 青岛德瑞高机械有限公司 Nose plug assembly for airship releasing mooring device

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN112644740A (en) * 2020-12-31 2021-04-13 中国科学院长春光学精密机械与物理研究所 Locking mechanism of aerospace device

Also Published As

Publication number Publication date
CN104590580A (en) 2015-05-06
CN104590580B (en) 2016-08-17

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Legal Events

Date Code Title Description
C06 Publication
PB01 Publication
C10 Entry into substantive examination
SE01 Entry into force of request for substantive examination
C02 Deemed withdrawal of patent application after publication (patent law 2001)
WD01 Invention patent application deemed withdrawn after publication

Application publication date: 20141105