Design and performance test of spacecraft test and operation software

Wang, Guohua; Cui, Yan Xiang; Wang, Shuo; Meng, Xiaofeng

doi:10.1016/j.actaastro.2011.02.002

Cited by 10 publications

(4 citation statements)

References 2 publications

Supporting

Mentioning

Contrasting

Order By: Relevance

“…However when the rotate speed reaches to 800r/min, the torque decreases slightly, resulting from the shear thining. The experimental result once again proves the correctness of the formula (1).…”

Section: Experiments Results Analysissupporting

confidence: 59%

Research on Magneto-Rheological Torque Servo Devices

Han

Shan

et al. 2012

AMR

View full text Add to dashboard Cite

The dual characteristic of magnetorheological rheology and phase transitions is studied and its rheological principle is also described. By using the ANSYS finite element method, a simulation analysis of the torque transmission model is conducted. By selecting the magnetorheological fluid SG-MRF2035, a magneto-rheological torque servo device prototype (Gap of 1.5mm) is developed. And a performance testing platform is built for the torque output characteristics of prototype. The test results show that the device could provide supple output torque and the torque is continuously adjustable. This paper provides a new way for the wide application of magnetorheological fluids.

show abstract

Section: Experiments Results Analysissupporting

confidence: 59%

Research on Magneto-Rheological Torque Servo Devices

Han

Shan

et al. 2012

AMR

View full text Add to dashboard Cite

show abstract

“…Where available, component tests should be performed on the aircraft. Using the aircraft as a support for the test piece, applying loads to the test component and balancing loads to the rest of the aircraft, this kind of test is advantageous in terms of real connection and real force transmission [5]. However, at the stage of aircraft R&D, this idea simply cannot be realized.…”

Section: Design Principle and Application Of Proposed Support Methods...mentioning

confidence: 99%

Simulation experiment on support strength of aircraft structural components

Chen,

2024

Vib. proced.

View full text Add to dashboard Cite

The design principles of strength test support methods for aircraft structural components were introduced in this paper. Aiming at the vertical tail static test of a certain type of aircraft, a supporting stiffness simulation method was invented, and a support fixture was designed. The supporting stiffness was accurately simulated by stiffness strength. The research results of this paper provide an important reference for the research of static test support methods for similar aircraft structural components.

show abstract

“…Though magnetorheological elastomer damper has very strong nonlinearity in extrusion mode, the structure of damper is simple and the damper can withstand larger load. So we design the magnetorheological elastomer damper according to extrusion mode [5]. The specific structure of magnetorheological elastomer damper is shown in Fig.…”

Section: Mre Dampermentioning

confidence: 99%

The Application of Magnetorheological Damper in Machining the Impeller Blades of High Temperature Alloy

Zhao¹,

Zhong²,

Tang³

et al. 2012

MSF

View full text Add to dashboard Cite

In this paper, it is described the vibration problems in machining the impeller blades of high temperature alloy and some Solution about Vibration Problems at present.Then in allusion to vibration and low efficiency in machining the impeller blades of high temperature alloy, a new and stiffness adjustable damper is designed according to extrusion mode. And we compose the performance of magnetorheological elastomers and the operating mode of magnetorheological elastomers. Then we experiment on the damper which we have designed using the test systems which has been erected. The experiments show that we can suppress the vibration through changing the current. And when the coil windings of magnetorheological elastomer damper are set as current, the stiffness of magnetorheological elastomer damper is adjusted and the vibration is suppressed. Therefore,we can suppress the vibration through changing the current. And the magnetorheological damper can meet the design requirements.

show abstract

Design and performance test of spacecraft test and operation software

Cited by 10 publications

References 2 publications

Research on Magneto-Rheological Torque Servo Devices

Research on Magneto-Rheological Torque Servo Devices

Simulation experiment on support strength of aircraft structural components

The Application of Magnetorheological Damper in Machining the Impeller Blades of High Temperature Alloy

Contact Info

Product

Resources

About