Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
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Vickers Armstrongs Aircraft Ltd
Original Assignee
Vickers Armstrongs Aircraft Ltd
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Publication date
Application filed by Vickers Armstrongs Aircraft LtdfiledCriticalVickers Armstrongs Aircraft Ltd
Priority to ES0251802ApriorityCriticalpatent/ES251802A1/en
Publication of ES251802A1publicationCriticalpatent/ES251802A1/en
Aircraft having wings in an arrow, comprising jet propulsion units, which are mounted on the wings with their centers of mass and pressure centers located in front of the axis of flexion of the wings, and which are capable of movement around axes of pivoting which are substantially parallel to the axis oy and oz of the aircraft, respectively, having means provided by the pilot to effect said pivotable adjustments of the jet units in relation to the wings, which will initiate effective forces to produce pitching moments, rolling or yaw about the airplane. (Machine-translation by Google Translate, not legally binding)
ES0251802A1959-09-011959-09-01An aircraft (Machine-translation by Google Translate, not legally binding)
ExpiredES251802A1
(en)
Performance measurement using pilot controlled Gz maneuvering with simulated operational task(Measurements of acceleration stress effects on pilot maneuvering ability and flight control performance)
A compensation device for gyroscopic effects intended for aircraft and aerodines equipped with turbo-machines (Machine-translation by Google Translate, not legally binding)