发明名称 Control Quadrant
摘要 An aircraft with a control system having joint control for a throttle and a propeller of an aircraft may be modified to decouple the joint control of a throttle and a propeller. Control of the throttle and propeller may be independent of the other. Exemplary modification of a control system may use new structures, existing structures, repurpose existing structures, or use a combination thereof. Additionally or alternatively, modification of a control system may provide controls with tactile distinction to a user.
申请公布号 US2013037659(A1) 申请公布日期 2013.02.14
申请号 US201213571573 申请日期 2012.08.10
申请人 TAMARACK AEROSPACE GROUP, INC.;GUIDA NICHOLAS R.;KOEHLER DIETER;GATES HALDAN R.;BABIN STEPHEN L.;MITCHELL DWIGHT W.;HRDINA CHASE 发明人 GUIDA NICHOLAS R.;KOEHLER DIETER;GATES HALDAN R.;BABIN STEPHEN L.;MITCHELL DWIGHT W.;HRDINA CHASE
分类号 B64C19/02;B23P17/00 主分类号 B64C19/02
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