FR427076A -
Method and device for reducing or increasing the curvature of the wings of airplanes even during their flight simultaneously on both sides of the aircraft (increase or decrease in speed) or vice versa on one side with respect to the other ( total warping)
- Google Patents
Method and device for reducing or increasing the curvature of the wings of airplanes even during their flight simultaneously on both sides of the aircraft (increase or decrease in speed) or vice versa on one side with respect to the other ( total warping)
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POL DE CZERNICHOWSKI
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POL DE CZERNICHOWSKI
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Application filed by POL DE CZERNICHOWSKIfiledCriticalPOL DE CZERNICHOWSKI
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Publication of FR427076ApublicationCriticalpatent/FR427076A/en
B64C3/38—Adjustment of complete wings or parts thereof
B64C3/44—Varying camber
B64C3/48—Varying camber by relatively-movable parts of wing structures
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Engineering & Computer Science
(AREA)
Mechanical Engineering
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Aviation & Aerospace Engineering
(AREA)
FR427076D1911-03-091911-03-09
Method and device for reducing or increasing the curvature of the wings of airplanes even during their flight simultaneously on both sides of the aircraft (increase or decrease in speed) or vice versa on one side with respect to the other ( total warping)
ExpiredFR427076A
(en)
Method and device for reducing or increasing the curvature of the wings of airplanes even during their flight simultaneously on both sides of the aircraft (increase or decrease in speed) or vice versa on one side with respect to the other ( total warping)
Method and device for reducing or increasing the curvature of the wings of airplanes even during their flight simultaneously on both sides of the aircraft (increase or decrease in speed) or vice versa on one side with respect to the other ( total warping)
Universal sight on aircraft (or ship) for derivometry, precision landing, piloting, dive bombing by bombs or rockets, target on the ground or aerial target and torpedoing