Load mechanism for aircraft anti-G tester

A technology of loading mechanism and tester, applied in the direction of aircraft component testing, etc., can solve the problems of inability to load weights, hidden dangers of product quality, high labor intensity, etc., to verify the normality of work, improve the efficiency of test work, and ensure flight. safe effect

Inactive Publication Date: 2018-06-01
AVIC GUIZHOU AIRPLANE
View PDF3 Cites 4 Cited by
  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

Due to the limited installation position of the anti-gauge pressure regulator on the aircraft, it is located in a place with a small space. The traditional direct loading detection method cannot be loaded due to the space limitation

Method used

the structure of the environmentally friendly knitted fabric provided by the present invention; figure 2 Flow chart of the yarn wrapping machine for environmentally friendly knitted fabrics and storage devices; image 3 Is the parameter map of the yarn covering machine
View more

Image

Smart Image Click on the blue labels to locate them in the text.
Viewing Examples
Smart Image
  • Load mechanism for aircraft anti-G tester

Examples

Experimental program
Comparison scheme
Effect test

Embodiment Construction

[0011] The principles and features of the present invention will be described below in conjunction with the accompanying drawings.

[0012] A loading mechanism for an aircraft anti-load tester, comprising a rod body 1, a counterweight 2, a ring 3, a screw 4, a collar 5, a round nut 6, a strut 9, a bearing 10, a shaft pin 11, a nut 12, a top Rod 13, hook 14 and weight body 16, the counterweight 2 is fixed on the rear of the rod body 1 by screws 4, the strut 9 is installed on the tail of the rod body 1 through the bearing 10 and the shaft pin 11, and the round nut 6 passes through the nut 12 is connected with the strut 9, the collar 5 is welded with the round nut 6, the open end of the collar 5 is provided with a wing nut 7 and a screw 8, and the upper tip of the ejector rod 13 rests on the bottom of the rear groove of the rod body 1 Placed on the anti-load pressure regulator of the aircraft, the ring 3 is set at the front end of the rod body 1, the weight body 16 is a cavity an...

the structure of the environmentally friendly knitted fabric provided by the present invention; figure 2 Flow chart of the yarn wrapping machine for environmentally friendly knitted fabrics and storage devices; image 3 Is the parameter map of the yarn covering machine
Login to view more

PUM

No PUM Login to view more

Abstract

Provided is a load mechanism for an aircraft anti-G tester. The load mechanism for the aircraft anti-G tester includes a rod, a counterweight block, a rings, bolts, a clamp collar, a circular nut, a support rod, a bearing, a shaft pin, a nut, a jacking rod, a hook and a weight; the counterweight block is fixed to the rear portion of the rod through the bolts, the support rod is mounted on the tailportion of the rod through the bearing and the shaft pin, the circular nut is connected with the support rod through the nut, the ring is arranged at the front end of the rod, the weight is hollow, and a screw plug is arranged on the weight and is hooked on the ring through the hook. According to the load mechanism for the aircraft anti-G tester, by using a lever principle, a loading process is conducted outside a finished product, and a lever amplification principle is adopted to reduce the size of the weight, so that the problem is solved that due to small and narrow space, loading cannot be carried out, and aircraft anti-G system tests can be conducted smoothly, working normality of an aircraft anti-G system is effectively verified, the test efficiency is improved, and air safety of aircrafts is ensured.

Description

technical field [0001] The invention relates to the technical field of debugging test equipment for an aircraft anti-G system, in particular to a loading mechanism for an aircraft anti-G tester. Background technique [0002] The aircraft anti-gauge system is the basic guarantee system to ensure that the pilot provides load reduction and decompression during overload flight and provides comfortable flight conditions. Whether the system is normal directly affects the normal flight of the pilot and the flight safety of the aircraft. How to verify whether it is normal, you need to simulate air flight on the ground to check whether its system working indicators are normal. The designed and manufactured anti-load tester is a test tool used to test whether the system is normal. Due to the limited installation position of the anti-gauge pressure regulator on the aircraft, it is located in a place with a small space. The traditional direct loading detection method cannot be loaded ...

Claims

the structure of the environmentally friendly knitted fabric provided by the present invention; figure 2 Flow chart of the yarn wrapping machine for environmentally friendly knitted fabrics and storage devices; image 3 Is the parameter map of the yarn covering machine
Login to view more

Application Information

Patent Timeline
no application Login to view more
IPC IPC(8): B64F5/60
Inventor 徐萌苏峰李凯旋
Owner AVIC GUIZHOU AIRPLANE
Who we serve
  • R&D Engineer
  • R&D Manager
  • IP Professional
Why Eureka
  • Industry Leading Data Capabilities
  • Powerful AI technology
  • Patent DNA Extraction
Social media
Try Eureka
PatSnap group products

Browse by: Latest US Patents, China's latest patents, Technical Efficacy Thesaurus, Application Domain, Technology Topic.

© 2024 PatSnap. All rights reserved.Legal|Privacy policy|Modern Slavery Act Transparency Statement|Sitemap