发明名称 Rotary switch assembly for ion propulsion system
摘要 A gridded ion propulsion system comprising two power controllers, four ion thrusters, and two switch assemblies. One switch assembly is connected to the two power controllers and to two of the four ion thrusters. The other switch assembly is connected to the two power controllers and to the other two ion thrusters. Each switch assembly has first and second switching states which can be selected to enable either power controller to supply power to any one of the four ion thrusters. Each switch assembly comprises a respective movable body and a respective multiplicity of switches which change state in unison when the movable body changes position. For example, the movable body may be a rotatable hollow shaft driven by a stepper motor.
申请公布号 EP2735736(A2) 申请公布日期 2014.05.28
申请号 EP20130184087 申请日期 2013.09.12
申请人 THE BOEING COMPANY 发明人 STICKELMAIER, JOHN F.;ZIAVRAS, JOHN;PERKINS, JULIE MARIE;KREINER, KURT B.;CAPLIN, GLENN N.;SMITH, BRIAN K.;LAUENSTEIN, PETER S.
分类号 F03H1/00;B64G1/42;H01H19/64 主分类号 F03H1/00
代理机构 代理人
主权项
地址