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Force measuring device for aircraft throttle lever

A force measuring device and throttle lever technology, which is used in measuring devices, aircraft component testing, and measuring the force applied to control elements, etc. problems, to achieve stable measurement process, improve detection efficiency, and reduce labor intensity.

Active Publication Date: 2019-09-06
SHAANXI AIRCRAFT CORPORATION
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0004] The purpose of the present invention is to provide a force measuring device for the throttle lever of an aircraft, which solves the problem that in the prior art, manual pulling of the dynamometer is used to measure the throttle rod. Due to the uncertain force measuring direction and unstable force measuring process, there is scattered force value measurement data. Difficult problem in judging the detection conclusion

Method used

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  • Force measuring device for aircraft throttle lever
  • Force measuring device for aircraft throttle lever
  • Force measuring device for aircraft throttle lever

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Embodiment Construction

[0034] Attached below Figure 2 to Figure 8 Further description of the device: an aircraft throttle lever force measuring device is composed of five parts: an alignment assembly 1, a measurement assembly 2, a power assembly 3, an installation assembly 4, and a support assembly 5. First, the aligning assembly 1 aligns the central position of the throttle console 8 on the aircraft throttle console 6, and the installation assembly 4 and the support assembly 5 are respectively aligned with the locators 13 of the aligning assembly 1 to align the installation position. The installation assembly 4 and the support assembly 5 are fixed on the aircraft seat slide rails 7 on both sides of the aircraft throttle console 6 . Then install the power component 3 on the installation component 4, and finally connect the measurement component 2, the power component 3 and the support component 5 at the same time to use. The alignment assembly 1 is composed of a positioning block 11 , an alignment...

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PUM

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Abstract

The invention belongs to the technical field of mechanical manufacturing process equipment, and provides a force measuring device for an aircraft throttle lever. The force measuring device comprises an alignment assembly (1), a measuring assembly (2), a power assembly (3), a mounting assembly (4) and a supporting assembly (5); the alignment assembly (1) conducts alignment on the center of a throttle table (8) on an aircraft throttle operation table (6), the mounting assembly (4) and the supporting assembly (5) are aligned with a positioner (13) of the alignment assembly (1), the mounting position is aligned, and after alignment, the mounting assembly (4) and the supporting assembly (5) are fixed to aircraft seat sliding rails (7) in the two sides of the aircraft throttle operation table (6); and the power assembly (3) is mounted on the mounting assembly (4), and the measuring assembly (2) is connected with the power assembly (3) and the supporting assembly (5) simultaneously. The problems that in the prior art, the throttle pull lever is measured by manually pulling a force measurer, force value measuring data are scattered, and the test conclusion is difficult to judge are solved.

Description

technical field [0001] The invention belongs to the technical field of mechanical manufacturing process equipment, and relates to an aircraft throttle lever force measuring device. Background technique [0002] In the aircraft manufacturing and assembly process, after the throttle console is installed, it is necessary to detect the force value of the throttle lever in the three states of no-load, braking, and over the block, and judge whether the installation of the throttle console is qualified according to whether the force value meets the design requirements. In the prior art, the throttle rod is measured by manually pulling the dynamometer. Due to the uncertain force measurement direction and unstable force measurement process, there are problems such as scattered force value measurement data and difficult determination of detection conclusions. Contents of the invention [0003] Technical issues resolved [0004] The purpose of the present invention is to provide a f...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64F5/60G01L5/22
CPCB64F5/60G01L5/223
Inventor 黄蓉肖望东韩波刘炜何卫民吴军豪李春刚王宏明全力
Owner SHAANXI AIRCRAFT CORPORATION