Multi-gradient human-sensing device and its design method

A gradient man and sleeve technology, which is applied to the power plant, transportation and packaging, and aircraft parts of the aircraft, can solve the problems of lack of effective and standardized methods for the aircraft control system, large amount of rework, complex load mechanism, etc., and achieve shortening The effect of system adjustment period, reduction of repeated work, and simplification of adjustment process

Active Publication Date: 2018-07-24
SHAANXI AIRCRAFT CORPORATION
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

Due to the shortcomings in the design of the load mechanism, such as complexity, long cycle, large amount of rework, and difficult state guarantee, it has caused many problems in design and production. The existing technology lacks effective and standardized methods for aircraft control systems.

Method used

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  • Multi-gradient human-sensing device and its design method
  • Multi-gradient human-sensing device and its design method
  • Multi-gradient human-sensing device and its design method

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Embodiment Construction

[0031] The human sensory device design method of the present invention comprises the human sensory device parts single-ear threaded sleeve single-eared threaded sleeve 1, a first retainer 6, a second retainer 9, a third retainer 16, a fourth retainer 30, The first steel ball 7, the second steel ball 10, the third steel ball 17, the fourth steel ball 20, the fifth steel ball 31, the action rod 8, the first prestress regulator 11, the second prestress regulator 26, the third prestress regulator Device 33, first sleeve 12, second sleeve 15, third sleeve 18, fourth sleeve 22, fifth sleeve 23, sixth sleeve 25, seventh sleeve 28, large spring 13, outer Barrel 14, stroke adjuster 19, middle spring 21, small spring 24, eighth sleeve 29, end cap 34, ear joint 36.

[0032] Among them, vent holes are arranged between the closed cavities of different moving parts to reduce the damping of the gas during movement, and the steel ball and the cage reduce the friction force of the load mechani...

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Abstract

The invention relates to a design technology of a human-sensing system of an aircraft control system, and relates to a design method of a multi-gradient human-sensing device of an aircraft control system. The invention provides a human-sensing system design technology for an aircraft operating system. The design error of the sensory force provided by the human-sensing device is greatly reduced, an excellent operating force feeling is obtained, and the design, installation and debugging cycle of the human-sensing system is greatly shortened. In addition, the present invention also provides examples of human sensing devices in various aircraft operating systems.

Description

technical field [0001] The invention relates to the design technology of a human-sensing system of an aircraft control system, and relates to a design method of a multi-gradient human-sensing device of an aircraft control system. Background technique [0002] The artificial flight control system includes aileron control system, elevator control system and rudder control system, which are used to control the aircraft to achieve roll, pitch and yaw. As an important functional system of the aircraft, it directly affects the flight safety of the aircraft, so the design of the flight control system is very important. In the irreversible control system, the function of the human-sensing device is to simulate the action of the hinge moment and provide the pilot with the feeling of the control force; in the two systems with cross-linking relationship, the function of the human-sensing device is to block when one system is stuck. , another set of normal systems can still be manipula...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): B64D31/04
Inventor 车意彬何志国宋娟妮石强军吕明骆李平李晓茹陈丰华徐鸿洋朱永岗何松青崔海东杨曦袁志敏史振良
Owner SHAANXI AIRCRAFT CORPORATION
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