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Fatigue life tester of dynamic load of working ladder of military aircraft

A dynamic load and fatigue life technology, applied in the direction of machine/structural component testing, measuring devices, instruments, etc., can solve the fatigue and service life management of ladder structures, cannot effectively guarantee the safety of ladder use, and is not used for testing Ladder fatigue life technology and other issues

Inactive Publication Date: 2017-12-22
WEIHAI GUANGWEI COMPOSITES
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

At present, the troops mostly use light non-metal composite material working ladders and aluminum alloy working ladders. However, there is no fatigue life detection technology for ladders in the prior art, which cannot effectively guarantee the safety of ladders, and cannot effectively and timely check the ladder structure. Fatigue and service life managed

Method used

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  • Fatigue life tester of dynamic load of working ladder of military aircraft
  • Fatigue life tester of dynamic load of working ladder of military aircraft

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Experimental program
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Embodiment Construction

[0011] exist figure 1 , figure 2 Among them, the present invention is provided with a ladder hanger 1, and a fixed frame 11 is installed on one side of the ladder hanger 1, and a horizontal slide rail 10 is arranged on both sides of the fixed frame 11, and a horizontally movable frame 7 is installed on the horizontal slide rail 10, and the horizontally movable The frame 7 is controlled by the horizontal frequency conversion motor 15, the horizontal gear chain 9, and the limit block 12 to move laterally on the horizontal slide rail 10; Movable frame 4, vertically movable frame 4 is controlled by longitudinal variable frequency motor 13, longitudinal gear chain 14, positioning block 5 to move longitudinally on the longitudinal slide rail 6; the lower side of the front end of longitudinally movable frame 4 is hinged with the middle part of loading lever 17, and the loading lever 17 rear end is hinged with electric push rod 16, loading head 19 is installed on the front end of lo...

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Abstract

The invention, which belongs to the detection equipment field, relates to a fatigue life tester of a dynamic load of a working ladder of a military aircraft. The tester is provided with a ladder hanging rack. A fixed frame is installed at one side of the ladder hanging rack; horizontal sliding rails are arranged at the two sides of the fixed frame; and a horizontal movable frame is installed on the horizontal sliding rails and is controlled by a horizontal variable frequency motor, a horizontal gear chain, and a limiting block to move horizontally on the horizontal sliding rails. Besides, longitudinal sliding rails are arranged vertically at the two sides of the horizontal movable frame; a longitudinal moving frame is installed on the longitudinal sliding rails and is controlled by a longitudinal variable frequency motor, a longitudinal gear chain, and a positioning block to move longitudinally on the longitudinal sliding rails. The lower side of the front end of the longitudinal moving frame is hinged with the middle part of a loaded lever; the rear end of the loaded lever is hinged to an electric push rod; a loading head is installed at the front end of the loaded lever by a pressure sensor; and an infrared counter is installed at the loaded lever.

Description

technical field [0001] The invention relates to the field of testing equipment, in particular to a dynamic load fatigue life testing machine for military aircraft working ladders. Background technique [0002] As we all know, at military airports, pilots and maintenance personnel often use working ladders with various functions such as boarding ladders, ground working ladders, and fuselage maintenance ladders. Due to the high frequency of use of military aircraft working ladders and long life expectancy (about 30 years), the use status, safety performance and fatigue life of working ladders are directly related to the personal safety of pilots and maintenance personnel. Since modern warfare has the characteristics of fast response, light equipment, and quick transition, ground support equipment is also required to be light and easy to carry. The lightweight of the working ladder must be optimized in terms of structural design, multi-purpose in terms of use, and lightweight ...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G01M99/00
CPCG01M99/007
Inventor 朱有欣刘清刚王鹏远温泉韩克谦刘昌波林凤森
Owner WEIHAI GUANGWEI COMPOSITES
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