Unlock instant, AI-driven research and patent intelligence for your innovation.

Mobile micro-friction solid rocket engine thrust measurement system and installation method thereof

A measurement system and solid rocket technology, applied in the direction of engine testing, jet engine testing, gas turbine engine testing, etc., can solve problems such as weak lateral stiffness of leaf springs, instability of leaf springs, and anisotropic damping of leaf springs, etc., to achieve Improve motion accuracy, high reliability, and smooth motion

Active Publication Date: 2021-01-01
北京灵动飞天动力科技有限公司
View PDF7 Cites 6 Cited by
  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0004]1. The friction force of the leaf spring is a variable value, which generally changes with the change of the engine mass, which affects the test accuracy;
[0005]2. During the test, the leaf spring is in an unstable state, which affects the test accuracy;
[0006]3. The lateral stiffness of the leaf spring is relatively weak, and distortion and deformation occur, which affects the test accuracy;
[0007]4. Generally, four leaf springs are used for connection, but the damping of each leaf spring is in all directions;
[0008]5. Generally, the test frame connected by leaf spring needs to be equipped with in-situ calibration device

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
  • Mobile micro-friction solid rocket engine thrust measurement system and installation method thereof
  • Mobile micro-friction solid rocket engine thrust measurement system and installation method thereof

Examples

Experimental program
Comparison scheme
Effect test

Embodiment Construction

[0031] The present invention will be described in detail below with reference to the accompanying drawings and examples.

[0032] The mobile micro-friction solid rocket motor thrust measurement system of the present invention consists of a fixed frame 12, a movable frame 13, a support frame 14, an engine 15, a ring 16, a transition frame 17, a force-measuring assembly 18, a load-bearing pier 19, and a push rod 20; the moving frame 13 and the bearing pier 19 are bolted to the fixed frame 12, the support frame 14 is bolted to the moving frame 13, and the ring 16 is connected to the supporting frame 14; the front end of the bearing pier 19 is bolted with a push rod 20. The rear end is connected to the force measuring assembly 18; the rear end of the force measuring assembly 18 is connected to the transition frame 17, and the transition frame 17 is fixedly connected to the front skirt of the engine 15 by bolts. The overall structure of the device eliminates the in-situ calibration...

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 relates to a mobile micro-friction solid rocket engine thrust measurement system and an installation method thereof. The measurement system is composed of a fixed frame, a movable frame,a supporting frame, an engine, a holding ring, a transition frame, a force measurement assembly, a force bearing pier and an ejector rod. The movable frame and the force bearing pier are both fixed to the fixed frame through bolts, the supporting frame is fixed to the movable frame through bolts, and the holding ring is connected to the supporting frame. An ejector rod is fixed at the front end of the force bearing pier through a bolt, and the force measuring assembly is connected at the rear end of the force bearing pier; and the rear end of the force measuring assembly is connected with thetransition frame which is fixedly connected with an engine front skirt through bolts. According to the overall structure of the device, an in-situ calibration device is omitted, and compared with a traditional fixed plate spring connecting structure, the structure is simpler, and the precision is higher.

Description

technical field [0001] The invention relates to a mobile micro-friction solid rocket motor thrust measurement system and an installation method thereof, belonging to the technical field of solid rocket motors. Background technique [0002] The solid rocket motor ground test is an irreversible, high-cost, high-risk test. The working time of the engine is short, the amount of information to be obtained is large, and the process control and key parameters require high precision. The solid rocket motor thrust test is the most important link in the ground test. In the thrust test, the test frame is the key equipment for the thrust test, which has a great impact on the test accuracy of the engine thrust, transient thrust and negative thrust. The reason is that During the test, the test frame must bear the pressure of the engine and all its accessories, and maintain a certain attitude for the engine to fix the position to ensure that the axis of the engine is aligned with the forc...

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): G01M15/14G01M15/02
CPCG01M15/14G01M15/02
Inventor 王志浩王君祺吴刚张庚辰
Owner 北京灵动飞天动力科技有限公司