Check patentability & draft patents in minutes with Patsnap Eureka AI!

Rocket engine thrust testing device

A rocket engine and testing device technology, applied in jet engine testing, gas turbine engine testing, measuring devices, etc., can solve the problems of inaccurate test results, eccentric thrust, limited application range, etc., and achieve good static performance indicators, repeatability Good performance and hysteresis, accurate test results

Inactive Publication Date: 2019-09-10
NORTHWESTERN POLYTECHNICAL UNIV
View PDF9 Cites 11 Cited by
  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

I understand that the current rocket engine thrust test mostly uses a separate test device. During the experiment, due to the tangential movement of the moving frame, the thrust eccentricity is likely to occur, resulting in inaccurate test results. In addition, the separate test device is used in each test. At present, it takes a lot of time to install the test frame. At the same time, most of the current test devices are model-specific, so they are highly targeted, resulting in limited application range, reducing the versatility of the experimental test system, and thus increasing the experimental cost.
For example, the thrust plate of the existing test device is used for the positioning of the engine, and the thrust plate is fixed at one end of the engine; while the solid-liquid engine is provided with an oxidant supply pipeline at one end, if the test device in the prior art is used, it will interfere and affect the test experiment , resulting in a test setup that is not universal

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
  • Rocket engine thrust testing device
  • Rocket engine thrust testing device
  • Rocket engine thrust testing device

Examples

Experimental program
Comparison scheme
Effect test

example 1

[0041] The thrust test of a small rocket engine, for a solid-liquid hybrid rocket engine with a diameter of 100mm, first select a 600mm-long engine fixed plate, and install the solid-liquid mixed engine fixed plate on the moving frame so that the left and right distances are exactly the same, so as to achieve the engine’s The axis is consistent with the axis of the overall moving frame, and then select the engine fixing frame with a diameter of 100mm, fix the engine fixing frame on the engine fixing plate through bolts, fix the assembled solid-liquid hybrid engine on the engine fixing plate, and connect the oxidant pipeline Connect well with the solid-liquid mixing engine injector.

[0042] Insert the guide rod between the moving frame and the guide frame, screw on the nut to prevent it from falling off during the experiment, remove the support seat to force the leaf spring; adjust the height of the power transmission shaft so that the axis of the power transmission shaft is in...

example 2

[0044] For the thrust test of a medium-sized rocket motor, for a solid rocket motor with a diameter of 1000mm, first select an engine fixing plate with a length of 1800mm, and install the engine fixing plate on the moving frame so that the left and right distances are exactly the same, so that the axis of the engine is consistent with the overall moving frame. The axes are consistent, and then select the engine fixing frame with a diameter of 1000mm, fix the engine fixing frame on the engine fixing plate, and fix the assembled hybrid engine on the engine fixing plate.

[0045] Insert the guide rod between the moving frame and the guide frame, screw on the nut to prevent it from falling off during the experiment, remove the support seat to force the leaf spring; adjust the height of the power transmission shaft so that the axis of the power transmission shaft is in line with the solid-liquid mixing engine Keep the axis of the axis consistent, fix the sensor on the sensor seat, a...

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 puts forward a rocket engine thrust testing device, which comprises a sensor fixing table, a sensor fixing plate, a force transmission shaft, a thrust plate, a guidance rod, a guidance frame, a movable frame, a fixed frame, a plate spring, an engine fixing plate and an engine fixing frame, wherein the sensor is fixed on the sensor fixing table on one end of the testing device; on theother hand of the testing device, the movable frame is fixed just above the fixed frame through the plate spring; the guidance rod performs a guidance function for the axial displacement of the movable frame; the displacement of the movable frame in other directions is restricted; the force transmission shaft is fixed just above the movable frame to guarantee that the force transmission shaft andthe sensor are coaxial and are free from stress contact; and before an experiment, a testing frame is integral and does not need to be assembled, after the experiment is finished, a supporting seat is installed, and the plate spring guarantees to be free from stress under a non-experiment state. An engine fixing frame and the movable frame adopt a detachable fixing way, different engines can be replaced according to experiment requirements, the device can be suitable for engines of different sizes by replacing the engine fixing frame, and the universality of the testing device is realized.

Description

technical field [0001] The invention belongs to the field of engine testing, and in particular relates to a rocket engine thrust testing device. Background technique [0002] The rocket engine testing technology is the core key technology in the engine development process. It runs through the entire engine experimental research process. The working process of the rocket engine is very complicated. It requires a combination of theoretical analysis and experiments to understand its comprehensive characteristics. Thrust is the main parameter to reflect the performance of a rocket engine. In order to accurately test the thrust of a rocket engine, it is necessary to study thrust testing technology. The ground experiment can provide the most intuitive data for the performance appraisal of the engine, and conclusions can be drawn through the analysis of the data, so as to accurately obtain the thrust of the rocket engine during the ground test. The performance of the test system d...

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): G01M15/14G01L5/00
CPCG01L5/00G01M15/14
Inventor 刘林林郭泉胡松启
Owner NORTHWESTERN POLYTECHNICAL UNIV
Features
  • R&D
  • Intellectual Property
  • Life Sciences
  • Materials
  • Tech Scout
Why Patsnap Eureka
  • Unparalleled Data Quality
  • Higher Quality Content
  • 60% Fewer Hallucinations
Social media
Patsnap Eureka Blog
Learn More