发明名称 ELECTRO-RHEOLOGICAL ELASTOMERIC, VARIABLE-STIFFNESS FLIGHT CONTROL DEVICE
摘要 According to one embodiment, a flight control device includes a grip, a stick associated with the grip, and a gimbal. The stick defines a first axis. The gimbal includes a first platform, a second platform, a first electro-rheological elastomeric bearing, and a second electro-rheological elastomeric bearing. The first platform is coupled to the stick and configured to rotate on a second axis that is perpendicular to the first axis. The second platform is in mechanical communication with the first platform and configured to rotate on a third axis that is perpendicular to the second axis. The first electro-rheological elastomeric bearing defines the second axis, and the second electro-rheological elastomeric bearing defines the third axis. The first and second electro-rheological elastomeric bearing being configured to each have a variable stiffness.
申请公布号 US2016375996(A1) 申请公布日期 2016.12.29
申请号 US201514749208 申请日期 2015.06.24
申请人 Bell Helicopter Textron Inc. 发明人 Modrzejewski Brian Stanley
分类号 B64C27/57;G05G9/047;G05G5/02;B64C27/04 主分类号 B64C27/57
代理机构 代理人
主权项 1. A flight control device, comprising: a grip; a stick associated with the grip, the stick defining a first axis; and a gimbal comprising: a first platform coupled to the stick, the first platform configured to rotate on a second axis that is perpendicular to the first axis;a second platform in mechanical communication with the first platform, the second platform configured to rotate on a third axis that is perpendicular to the second axis;a first electro-rheological elastomeric bearing defining the second axis, the first electro-rheological elastomeric bearing being configured to have a variable stiffness; anda second electro-rheological elastomeric bearing defining the third axis, the second electro-rheological elastomeric bearing being configured to have a variable stiffness.
地址 Fort Worth TX US