公开(公告)号：EP2252506A4

公开(公告)日：2013-05-01

申请号：EP09758838

申请日：2009-03-11

申请人： USERCENTRIX LLC

发明人： ROZOVSKI DAVID

IPC分类号： B64C13/04 ,  B64C29/00 ,  B64D31/04 ,  G05G9/04

CPC分类号： B64C13/04 ,  B64C29/0033 ,  B64D31/04 ,  G05G9/04

公开(公告)号：EP2252506A1

公开(公告)日：2010-11-24

申请号：EP09758838.8

申请日：2009-03-11

申请人： UserCentrix LLC

发明人： Rozovski, david

IPC分类号： B64C13/04

CPC分类号： B64C13/04 ,  B64C29/0033 ,  B64D31/04 ,  G05G9/04

摘要： An aircraft control input apparatus is configured to accept and provide to the aircraft control inputs from a user regarding the magnitude and direction of the aircraft's thrust vector. The present invention enables a user to continually provide control inputs to an aircraft in which both the magnitude and the direction of thrust vary. A rotational throttle interface is configured to alter its orientation within the aircraft based on the directional component of the aircraft's thrust vector. The rotational throttle interface enables the user to provide continual control inputs to command both the directional component of the thrust as well as the magnitude component. Accordingly the user can provide inputs regarding direction and magnitude throughout the operating envelope of the aircraft's thrust vector while maintaining continuous physical contact with the throttle.