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An aircraft mooring device and mooring method

A tethering and aircraft technology, which is applied to ground devices, ground devices, aircraft parts, etc. for mooring aircraft, can solve the problems of inconvenient adjustment of the length of the mooring device and the inability to obtain the mooring tension, etc., to achieve convenient application, Simple structure and safe effect

Active Publication Date: 2022-03-01
CHINA AIRPLANT STRENGTH RES INST
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0004] The technical problem solved by the present invention is: the length adjustment of the aircraft ground mooring device in the prior art is inconvenient, and the mooring tension cannot be obtained directly from the mooring device.

Method used

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  • An aircraft mooring device and mooring method
  • An aircraft mooring device and mooring method
  • An aircraft mooring device and mooring method

Examples

Experimental program
Comparison scheme
Effect test

Embodiment 1

[0047] like figure 2 An aircraft mooring device shown includes a length module 1 connected to an aircraft mooring point at one end, a measurement module 2 arranged at the other end of the length module 1, one end is connected to the measurement module 2, and the other end is connected to the ground mooring point The adjustment module 3, and the connection module 4 arranged at the end connection of the length module 1, the measurement module 2, and the adjustment module 3;

[0048] The connecting module 4 is a butterfly buckle.

[0049] The length module 1 is formed by connecting five metal chains with a length of 500mm.

[0050] like image 3 As shown, the measurement module 2 includes a first pull ring 20, a first pull rod 21 arranged at one end on the first pull ring 20, a first flange 22 arranged at the other end of the first pull rod 21, and the first flange 22 corresponding to the second flange 23, three linear spring elements 24 arranged between the first flange 22 a...

Embodiment 2

[0063] like figure 1 An aircraft mooring device shown includes a length module 1 connected to an aircraft mooring point at one end, a measurement module 2 arranged at the other end of the length module 1, one end is connected to the measurement module 2, and the other end is connected to the ground mooring point The adjustment module 3, and the connection module 4 arranged at the end connection of the length module 1, the measurement module 2, and the adjustment module 3;

[0064] The connecting module 4 is a butterfly buckle.

[0065] The length module 1 is formed by connecting three metal chains with a length of 1000mm.

[0066] The measuring module 2 includes a first pull ring 20, a first pull rod 21 arranged on the first pull ring 20 at one end, and a first flange 22 arranged at the other end of the first pull rod 21, corresponding to the first flange 22 The second flange 23, 4 linear spring elements 24 arranged between the first flange 22 and the second flange 23, 3 one...

Embodiment 3

[0083] like figure 2 An aircraft mooring device shown includes a length module 1 connected to an aircraft mooring point at one end, a measurement module 2 arranged at the other end of the length module 1, one end is connected to the measurement module 2, and the other end is connected to the ground mooring point The adjustment module 3, and the connection module 4 arranged at the end connection of the length module 1, the measurement module 2, and the adjustment module 3;

[0084] The connecting module 4 is a butterfly buckle.

[0085] Length module 1 is formed by connecting 5 metal chains with a length of 800mm

[0086] The measuring module 2 includes a first pull ring 20, a first pull rod 21 arranged on the first pull ring 20 at one end, and a first flange 22 arranged at the other end of the first pull rod 21, corresponding to the first flange 22 The second flange 23, 5 linear spring elements 24 arranged between the first flange 22 and the second flange 23, 3 one ends are...

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Abstract

The present invention relates to the technical field of ground devices associated with aircraft, in particular to an aircraft mooring device and a mooring method. The mooring device includes a length module, a measurement module, an adjustment module, and a connection module; the measurement module includes The first pull ring, the first tie rod, the first flange, the second flange, and the linear spring element; the mooring method includes: determining the mooring method of the aircraft; calculating the mooring load; calculating the material under extreme temperature by experiment The difference in tethering tension caused by the thermal expansion and contraction effect; the tethering pre-tightening force and the set sliding friction; calculation of the pounds and elastic coefficients of the linear spring elements in the measurement module; mooring the aircraft and the mooring point on the ground; The mooring device provided by the invention can not only automatically adjust the length, but also can intuitively obtain the mooring tension in the mooring tension state.

Description

technical field [0001] The invention relates to the technical field of ground devices associated with aircraft, in particular to an aircraft mooring device and a mooring method. Background technique [0002] For aircraft testing, it is often required that the position of the test aircraft remains fixed. Therefore, in this test, the aircraft is often connected with the ground anchors arranged in the laboratory through mooring devices, so as to ensure the fixed position of the aircraft. In the climate test of the aircraft laboratory, it is generally required that the test aircraft is a complete aircraft including all systems and equipment, and operations such as starting the auxiliary power unit or starting the engine are often performed during the test. In addition, some test items need to blow the aircraft (including wind blowing rain, wind blowing snow, freezing clouds, etc.). These characteristics make the aircraft laboratory climate test have higher requirements for air...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): B64F3/00B64F5/60
CPCB64F3/00B64F5/60
Inventor 王彬文成竹吴敬涛雷凯邓文亮
Owner CHINA AIRPLANT STRENGTH RES INST
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