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) are provided, as are embodiments of a method for fabricating CMGs. In one embodiment, a CMG includes a stator housing, an inner gimbal assembly (IGA), and a torque motor coupled to the stator housing and configured to rotate the IGA about a gimbal axis to selectively generate a desired output torque during operation of the CMG. The IGA includes, in turn, an IGA support structure rotatably coupled to the stator housing, a monolithic CMG rotor rotatably mounted to the IGA support structure, and a spin motor coupled to the IGA support structure and configured to rotate the monolithic CMG rotor about a spin axis.
申请公布号 US9354079(B2) 申请公布日期 2016.05.31
申请号 US201213476699 申请日期 2012.05.21
申请人 Honeywell International Inc. 发明人 Davis Porter;Johnson Theodis;Stevens Carlos J.
分类号 G01C19/06;G01C25/00;B64G1/28 主分类号 G01C19/06
代理机构 Ingrassia Fisher & Lorenz, P.C. 代理人 Ingrassia Fisher & Lorenz, P.C.
主权项 1. A control moment gyroscope (CMG), comprising: a stator housing; an inner gimbal assembly (IGA), comprising: an IGA support structure rotatably coupled to the stator housing;a monolithic CMG rotor rotatably mounted to the IGA support structure; anda spin motor coupled to the IGA support structure and configured to rotate the monolithic CMG rotor about a spin axis; and a torque motor coupled to the stator housing and configured to rotate the IGA support structure about a gimbal axis to selectively generate a desired output torque during operation of the CMG; wherein the monolithic CMG rotor comprises a rotor rim, a rotor shaft, and a plurality of torsionally-stiff radial spokes integrally joined to the rotor rim and the rotor shaft as a single piece; and wherein each of the plurality of torsionally-stiff radial spokes is joined to the rotor shaft at a first spoke-shaft joinder interface and at a second spoke-shaft joinder interface, the first spoke-shaft joinder interface located closer to a first end of the rotor shaft than to the gimbal axis, and the second spoke-shaft joinder interface located closer to a second opposing end of the rotor shaft than to the gimbal axis.
地址 Morris Plains NJ US