Throttle Interface for Variable Thrust Vector Aircraft
AssigneeUserCentrix, LLC
InventorDavid Rozovski
Life of this patent
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AssigneeUserCentrix, LLC
InventorDavid Rozovski
Estimating the term…
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.
A method for providing a user interface for an aircraft having a longitudinal axis, a vertical axis and a resultant variable thrust vector within a geometric plane defined by the longitudinal axis and the vertical axis wherein the resultant variable thrust vector includes a magnitude and a direction, the method comprising:
A resultant variable thrust vector user interface for an aircraft having a longitudinal axis, a vertical axis and a resultant variable thrust vector within a geometric plane defined by the longitudinal axis and the vertical axis wherein the resultant variable thrust vector includes a magnitude and a direction, the resultant variable thrust vector user interface comprising:
An aircraft resultant variable thrust vector interface wherein the aircraft includes a longitudinal axis, a vertical axis, a geometric plane defined by the longitudinal axis and the vertical axis and a resultant variable thrust vector within the geometric plane and wherein the resultant variable thrust vector includes a magnitude and a direction, the resultant variable thrust vector user interface comprising:
Dependencies are inferred from the claim text.