发明名称 Vertical direction spacecraft vibration test system with pseudo-free boundary conditions
摘要 A method, apparatus, for subjecting a test object to vibrational energy testing is disclosed. The apparatus comprises a rotatable joint such as a hydrostatic ball joint for transmitting energy from a force generator to the test object, and a support structure, coupled to the test object and the rotatable joint, for flexibly restraining the test object from rotating about the center of rotation of the rotatable joint. In one embodiment of the invention, the support structure comprises a support member and at least one suspension device disposed between the support member and a ground datum. In another embodiment, the suspension device applies a suspension force to the support member in a direction substantially perpendicular to a vector from the center of rotation to the suspending force. In this embodiment the suspension devices are subjected primarily to compression and tension forces. The method comprises the steps of coupling a test object to a rotatable joint having a center of rotation, flexibly restraining the test object from rotating about the center of rotation, and applying vibrational energy substantially along a first axis passing through the center of rotation to the rotatable joint.
申请公布号 US6257067(B1) 申请公布日期 2001.07.10
申请号 US19990301444 申请日期 1999.04.28
申请人 HUGHES ELECTRONICS CORPORATION 发明人 ANKROM MARK E.;PANO SCOTT B.;VICARI LAWRENCE C.
分类号 G01M7/04;(IPC1-7):G01N29/00;B06B3/00 主分类号 G01M7/04
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