发明名称 Multi-axis, complex mode pneumatically actuated annular frame shaker for quasi-random pneumatic vibration facility
摘要 Pneumatically driven vibrators coupled to resonating, self-attenuating structures define a shaker which, when included in a vibration system, enables a test item to be vibration tested under controlled conditions of multi-frequency, multi-degree-of-freedom acceleration history, to achieve a frequency spectrum and acceleration-level control of a broadband quasi-random vibration output in the frequency range, for example, from 40 Hz to 2 kHz for vibration testing of equipment. The driving set of annular structure responds to an intense vibration spectrum, created by the attached pneumatic vibrators, with multi-modal forced and resonant frequencies in limited directions. The driven set of annular structure, holding the test hardware, responds with forced and harmonic oscillations to a vibration field transmitted from the driving set of structure through a specially designed elastomeric path. Specific design of the size, mass, and resonant behavior of the driving and driven structure sets with appropriate transmissibility characteristics of the elastomeric interface results in a controlled multi-modal, uniform RMS acceleration, multi-degree-of-freedom, wide-frequency-range vibration testing method. The annular arrangement of structure takes advantage of the complex amplitude-displacement behavior of the circumference of a ring excited into multi-modal in-plane and out-of-plane bending and torsional activity by the attached vibrators. Changes in pneumatic vibrator operating pressure change vibrator frequencies and expand available modal density.
申请公布号 US4181029(A) 申请公布日期 1980.01.01
申请号 US19780897824 申请日期 1978.04.19
申请人 HUGHES AIRCRAFT 发明人 TALBOTT, CHARLES F JR
分类号 G01M7/02;G01M7/06;(IPC1-7):G01N29/00 主分类号 G01M7/02
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