Login| Sign Up| Help| Contact|

Patent Searching and Data


Title:
VARIABLE-STROKE SELF-ADAPTIVE ADJUSTMENT QUASI-ZERO STIFFNESS DEVICE AND PARAMETER CHECKING METHOD
Document Type and Number:
WIPO Patent Application WO/2023/024968
Kind Code:
A1
Abstract:
A variable-stroke self-adaptive adjustment quasi-zero stiffness device and a parameter checking method, comprising: an integrating sphere, a target, a collimator, a pointing measuring instrument, disturbance sources, an inertia simulation tool, a quasi-zero stiffness suspension adjustment device, and an optical air floating platform. The integrating sphere, the target, and the collimator are mounted on the air floating platform; the integrating sphere provides a light source, the target provides point target information, and the collimator simulates infinity; the pointing measuring instrument is a measured object, and the pointing measuring instrument is fixedly connected to the inertia simulation tool; the three disturbance sources are mounted on the inertia simulation tool and provide tiny disturbance and inertia for the pointing measuring instrument; the quasi-zero stiffness suspension adjustment device suspends the inertia simulation tool and provides a free boundary environment; the quasi-zero stiffness suspension adjustment device, the pointing measuring instrument, the disturbance sources, and the inertia simulation tool integrally form a two-pendulum system set. In the present invention, comprehensive evaluation and quantitative analysis are carried out on the influence of an extremely-high-precision spatial pointing measuring instrument in a platform micro-vibration environment.

Inventors:
YUAN LI (CN)
WANG LI (CN)
LI LIN (CN)
WU YANPENG (CN)
ZHONG JUN (CN)
ZHAO QIN (CN)
ZHENG RAN (CN)
QI JINGYA (CN)
ZHANG CHENGYU (CN)
Application Number:
PCT/CN2022/112709
Publication Date:
March 02, 2023
Filing Date:
August 16, 2022
Export Citation:
Click for automatic bibliography generation   Help
Assignee:
BEIJING INST CONTROL ENG (CN)
International Classes:
G06F30/23; B64G7/00; F16D7/00; G01M13/00
Foreign References:
CN112504595A2021-03-16
CN109540493A2019-03-29
CN106477074A2017-03-08
US9920793B12018-03-20
CN113919190A2022-01-11
Attorney, Agent or Firm:
PATENT AGENT OF CHINA AEROSPACE TECHNOLOGY (CN)
Download PDF: