TRANSLATIONAL WING AIRCRAFT

PROBLEM TO BE SOLVED: To provide a translational wing aircraft simplifying mechanism, reducing weight, improving reliability, and reducing a manufacturing cost. SOLUTION: This translational wing aircraft employs a method for controlling output not by pitch angle control but by rotational speed contr...

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Bibliographische Detailangaben
Hauptverfasser:	KUBOMURA KENJI, UCHIDA TAKASHI
Format:	Patent
Sprache:	eng
Schlagworte:	BLASTING HEATING LIGHTING MACHINES OR ENGINES FOR LIQUIDS MECHANICAL ENGINEERING NON-POSITIVE DISPLACEMENT PUMPS OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR POSITIVE DISPLACEMENT MACHINES FOR LIQUIDS PRODUCING MECHANICAL POWER PUMPS FOR LIQUIDS OR ELASTIC FLUIDS WEAPONS WIND MOTORS WIND, SPRING WEIGHT AND MISCELLANEOUS MOTORS
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Beschreibung
Zusammenfassung:	PROBLEM TO BE SOLVED: To provide a translational wing aircraft simplifying mechanism, reducing weight, improving reliability, and reducing a manufacturing cost. SOLUTION: This translational wing aircraft employs a method for controlling output not by pitch angle control but by rotational speed control, a method for positioning a blade by pinching the upper part of one guide plate by more than one roller, and a method for changing a pitch angle by changing the angles of two arms installed fixedly on a blade shaft when pitch angle control is unescapable. COPYRIGHT: (C)2007,JPO&INPIT