A Micro Thrust Measuring Device Based on Cam Rotation Angle Measurement
Patent Information
- Authority / Receiving Office
- CN · China
- Patent Type
- Patents(China)
- Current Assignee / Owner
- PLA PEOPLES LIBERATION ARMY OF CHINA STRATEGIC SUPPORT FORCE AEROSPACE ENG UNIV
- Publication Date
- 2022-06-24
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Abstract
Description
technical field
[0001] The invention belongs to the technical field of devices or methods for measuring force, work, mechanical power or torque generated by impact, and relates to a micro thrust measuring device based on cam rotation angle measurement, with the international patent classification number: G01L 5 / 00. Background technique
[0002] Micro-nano satellites have very broad application prospects in both military and civilian areas, and also promote the development of micro thrusters. The thrust performance of the micro thruster is usually in the tens of millinewtons, hundreds of micronewtons, or even tens of micronewtons or a few micronewtons, which places very high requirements on the measurement system. At present, in order to measure the micro thrust, many scholars have been working on the design and experiment of the micro thrust measurement system. At present, the micro-thrust measuring device based on the horizontal torsion pendulum is the most commonly used m...