Test device for vibration test of aviation suspension launcher

A launch device and vibration test technology, which is applied in vibration test, measuring device, machine/structural component test, etc., can solve the problems of poor versatility of test tooling, untrue installation boundary, insufficient assessment of test pieces, etc., to achieve accurate Performance assessment, good transfer characteristics, and large load-carrying capacity

Active Publication Date: 2021-02-23
TIANJIN AEROSPACE RELIA TECH
View PDF9 Cites 1 Cited by
  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

However, there are several problems as follows: (1) The installation boundary is not true; (2) The test tooling for steel plate welding processing has poor transfer characteristics and insufficient evaluation of test pieces; (3) The specificity of the test tooling leads to different types of The suspension launching device needs to design a set of special matching tooling during the vibration test, and the test tooling has poor versatility; (4) The test device currently used is limited in terms of load-bearing quality, and it is impossible to test some of the suspension launching devices with heavy simulated bombs. Test conditions for effective assessment

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
  • Test device for vibration test of aviation suspension launcher
  • Test device for vibration test of aviation suspension launcher
  • Test device for vibration test of aviation suspension launcher

Examples

Experimental program
Comparison scheme
Effect test

Embodiment Construction

[0020] The present invention will be described in further detail below in conjunction with the accompanying drawings and specific embodiments. It should be understood that the specific embodiments described here are only used to explain the present invention, not to limit the present invention.

[0021] Such as Figure 1-2 As shown, the present invention is used for the test device of the vibration test of the aerial suspension launcher, and the suspension launcher transfer platform 2, the suspension beam tooling 3, the transition beam 4, the air spring 8 and the linear guide Bearing 9, suspension launching device 5, simulated projectile 6 and vibration table form a vibration test system; cage tooling is composed of cage tooling upper cover 1 and cage tooling base 7, and the inner and outer tops of cage tooling upper cover 1 form a plane structure to It is convenient to connect with the adapter platform 2 of the suspension launching device. The outer surface of the bottom of ...

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 a test device for the vibration test of an aviation suspension launcher. The device comprises a vibration table and a vibration test tool disposed at the upper end of the vibration table, wherein the vibration test tool comprises a cage-type tool with a reinforcing rib disposed on the surface, and the cage-type tool comprises a cage-type tool pedestal and a cage-type tool upper cover; the cage type tool base and the cage type tool upper cover are connected through a butt joint face row bolt. Threaded holes are evenly distributed in the top of the plane structure of thecage type tool upper cover in the length direction and the width direction and used for being connected with a suspended launcher transfer platform, and a balancing weight is installed at the top of the cage type tool upper cover. A suspension launching device switching platform connected to the top plane in the cage type tool upper cover is connected with a suspension beam tool of a suspension launching device used for hanging a simulation bomb through bolts. Air springs and linear guide bearings are arranged on the periphery of an upper end of a vibration table expansion table base of the vibration table and used for supporting a vibration test tool. The test device is advantaged in that a purpose of checking accuracy of the vibration test of the suspended launcher can be achieved.

Description

technical field [0001] The invention relates to the technical field of vibration tests, in particular to a test device for vibration tests of aerial suspension launching devices. Background technique [0002] Vibration test is often used to evaluate the anti-vibration ability of equipment in the use environment. It is an important part of the environmental qualification test of military equipment and is used to assess the adaptability of the military equipment to the vibration environment. Suspension launching device is used as an external hanger for aircraft carrying missiles in combat flight, and its reliability assessment in vibration environment is of great significance to the safety of aircraft. When performing vibration test assessment on the suspension launching device, it is necessary to design vibration test tooling to simulate the actual installation boundary of the suspension launching device on the aircraft, and complete the vibration test together with the vibra...

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): G01M7/02
CPCG01M7/02G01M7/027
Inventor 邵康王晓森王新杨立伟张庆昕罗旺雷霆宁薇薇周洁
Owner TIANJIN AEROSPACE RELIA TECH
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