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Aircraft control with ailerons that can be operated independently of the rudder and a device to compensate for the yaw moments around the vertical axis when the ailerons deflect

Assignee: August Wilhlem Quick
•
Filing: 1942-03-01
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Granted: 1944-11-24
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Expires: 1962-03-01
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Abstract

No abstract record available.

Inventors

  • 👤 August Wilhlem Quick

Bibliographic Details

Application Number —
Jurisdiction DE
Data Source google_patents
Last Synchronized 2026-10-26 22:13
CPC Classifications
B; B64; B64C; B64C13/00

Claims Analysis

Total Claims: 0
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References Cited (Backward Citations)

DE323881C Cited
DE585107C Cited
DE586410C Cited

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