发明名称 Control moment gyroscopes including torsionally-stiff spoked rotors and methods for the manufacture thereof
摘要 Embodiments of control moment gyroscopes (CMGs 20) are provided, as are embodiments of methods (100) for fabricating CMGs (20). In one embodiment, a CMG (20) includes a stator housing (56), an inner gimbal assembly (IGA 24), and a torque motor (58) configured to rotate the IGA (24) about a gimbal axis (60) to selectively generate a desired output torque during CMG operation. The IGA (24) includes, in turn, an IGA support structure (28) rotatably coupled to the stator housing (56), a CMG rotor (22) rotatably mounted to the IGA support structure (28), and a spin motor (48, 50) coupled to the IGA support structure (28) and configured to rotate the monolithic CMG rotor about a spin axis (52). The CMG rotor (22) is formed as a monolithic body comprising a rotor shaft (34), a rotor rim (72), and a plurality of torsionally-stiff radial spokes (74).
申请公布号 EP2666724(A1) 申请公布日期 2013.11.27
申请号 EP20130165670 申请日期 2013.04.26
申请人 HONEYWELL INTERNATIONAL INC. 发明人 DAVIS, PORTER;JOHNSON, THEODIS;STEVENS, CARLOS J.
分类号 B64G1/28;G01C19/06;G01C25/00 主分类号 B64G1/28
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