Angle of attack and sideslip indicator
阅读：225发布：2022-02-13
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15. APPARATUS FOR MEASURING THE AERODYNAMIC ANGLE OF AN AIRCRAFT HAVING A REFERENCE AXIS COMPRISING FIRST AND SECOND FORCE SENSING MEANS, INCLUDING LONGITUDINALLY EXTENDING PORTIONS EXPOSED IN FLIGHT TO AN AIRSTREAM, FOR GENERATING FIRST AND SECOND FORCE SIGNALS RESPECTIVELY INDICATIVE OF AERODYNAMIC FORCES ACTING ON SAID PORTIONS, SAID PORTIONS BEING ORIENTED IN FIRST AND SECOND DIRECTIONS WHICH HAVE DIFFERENT PREDETERMINED ANGULAR RELATIONS TO THE REFERENCE AXIS OF THE AIRCRAFT, AND COMPUTING MEANS RESPONSIVE TO SAID SIGNALS FOR CALCULATING THE RATIO OF ONE OF SAID FORCE SIGNALS TO THE DIFFERENCE BETWEEN SAID FORCE SIGNALS, AND MEANS FOR COMPUTING AN OUTPUT SIGNAL INDICATIVE OF SAID AERODYNAMIC ANGLE OF SAID AIRCRAFT ACCORDING TO THE DIFFERENCE BETWEEN ONE OF SAID PREDETERMINED ANGULAR RELATIONS AND THE PRODUCT OF (A) SAID RATIO AND (B) THE DIFFERENCE BETWEEN SAID PREDETERMINED ANGULAR RELATIONS.
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