Looking for breakthrough ideas for innovation challenges? Try Patsnap Eureka!

Airplane seat constraint system function and airtight testing bench

A technology of restraint system and aircraft seat, which is applied in the testing of mechanical components, testing of machine/structural components, liquid tightness measurement using liquid/vacuum degree, etc. It can solve the problem of insufficient supply of winch tension, sensor force value decay, Low work efficiency and other problems, to achieve the effect of stable product function inspection, reasonable structural design, and saving production time

Inactive Publication Date: 2016-10-12
国营芜湖机械厂
View PDF6 Cites 2 Cited by
  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] The early test equipment was manufactured according to the drawings imported from Ukraine, and the loading method was winch loading. During the above two tests, there were the following problems: 1. The seat leg straps and shoulder straps are made of textiles. The internal deformation of the winch leads to insufficient supply of winch tension, and the force value on the sensor declines significantly; 2. Due to the space limitation in the design of the test bench, it is difficult for the winch to reach the specified force value range within 10-20 seconds, combined with multiple adjustments of the shoulder strap Length inspection requirements, this structure is a serious waste of physical strength of workers, low work efficiency

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
  • Airplane seat constraint system function and airtight testing bench
  • Airplane seat constraint system function and airtight testing bench
  • Airplane seat constraint system function and airtight testing bench

Examples

Experimental program
Comparison scheme
Effect test

Embodiment Construction

[0016] In order to make the purpose, technical solutions and beneficial effects of the present invention more clear, the preferred embodiments of the present invention will be described in detail below in conjunction with the accompanying drawings, and the present invention will be further described to facilitate the understanding of technical personnel.

[0017] Such as Figure 1 to Figure 3 Shown, a kind of aircraft seat restraint system function and airtightness test bench, comprise hanging lug 4, hanging beam 5, boom 6, butterfly nut 7, fixed pulley 12, bracket 14, described fixed pulley 12 is fixed on the bracket 14, one end of the suspension beam 5 is hinged with the support 14 through the connecting assembly, the lifting lug 4 is installed on the suspension beam 5 near the upper end of the support 14, and the suspension rod 6 is located on the suspension beam 5 close to the support 14 One end of the suspension rod 6 is connected with the suspension beam 5 through a wing...

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

The invention discloses an airplane seat constraint system function and airtight testing bench. The testing bench comprises a hanger, a hanging beam, a hanger rod, a bufferfly-like nut, a fixed pulley and a support, wherein the fixed pulley is fixed on the upper end of the support, one end of the hanging beam is hinged to the support through a connection assembly, the hanger is installed at the upper portion of one end, closer to the support, of the hanging beam, the hanger rod is disposed at one end, closer to the support, on the hanging beam, the hanger rod is connected with the hanging beam through the bufferfly-like nut, and the lower end of the hanger rod is suspended with a counterweight. The airplane seat constraint system function and airtight testing bench has the advantages of reasonable structural design, convenient application and the like, can rapidly and accurately realize airplane seat test requirements, is low in fault rate and convenient to operate, greatly improves the airplane seat repair efficiency, saves enormous production time, gets rid of restrictions of air pressure, hydraulic pressure and motor parts, is safe and environmentally friendly and can stably carry out product function examination.

Description

technical field [0001] The invention relates to the technical field of repairing aviation accessories, in particular to an aircraft seat restraint system function and airtight test bench. Background technique [0002] After the aircraft seat is repaired and assembled, it is necessary to conduct functional and sealing tests such as the seat restraint system to verify the working performance and reliability of the entire product. Among them, in order to verify the performance of the leg tension rope and the reliability of the matching ball lock, it is necessary to add a load of 1176N to each process cylinder through the tension rope for 3 minutes. In addition, it is necessary to increase the load on the shoulder belt to check the working ability of the shoulder belt tensioning device. During the inspection, it is necessary to adjust the length of the shoulder belt several times, and add it to the belt within 10 to 20 seconds. Force, keep for 5-8s. [0003] The early test eq...

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
Patent Type & Authority Applications(China)
IPC IPC(8): G01M13/00G01M3/02
CPCG01M13/00G01M3/02
Inventor 姚广超曾晓利吕博
Owner 国营芜湖机械厂
Who we serve
  • R&D Engineer
  • R&D Manager
  • IP Professional
Why Patsnap Eureka
  • Industry Leading Data Capabilities
  • Powerful AI technology
  • Patent DNA Extraction
Social media
Patsnap Eureka Blog
Learn More
PatSnap group products