首页>
外国专利>
Dual cam control mechanism for coordinated deployment and retraction of an air-craft's leading and trailing edge wing flaps
Dual cam control mechanism for coordinated deployment and retraction of an air-craft's leading and trailing edge wing flaps
展开▼
机译:双凸轮控制机构可协调部署和收回飞机的前缘和后缘机翼襟翼
展开▼
页面导航
摘要
著录项
相似文献
摘要
In the disclosed mechanism a primary position control cam has first and second camming surfaces for cooperating with separate followers that in turn act through a hydraulic subsystem to position the leading and trailing edge wing flaps in response to a single, pilot operated control lever. A secondary cam also having first and second camming surfaces correspondingly shaped to those of the primary cam, is slaved to the actual, hydraulically effected movement of the trailing edge flaps. Cooperating with the first surface of the secondary cam is a feedback follower for providing a mechanical feedback signal that assists the primary cam and the associated hydraulics in positioning the trailing edge flaps. An override follower cooperates with the second camming surface on the secondary cam and mechanically overrides the ability of the primary cam's second surface follower to position the leading edge flaps under certain conditions, so as to ensure a predetermined, aerodynamically critical sequencing of the hydraulically effected movements of the leading and trailing edge flaps as they seek the positions commanded by the single, pilot operated lever.
展开▼