The patent badge is an abbreviated version of the USPTO patent document. The patent badge does contain a link to the full patent document.
The patent badge is an abbreviated version of the USPTO patent document. The patent badge covers the following: Patent number, Date patent was issued, Date patent was filed, Title of the patent, Applicant, Inventor, Assignee, Attorney firm, Primary examiner, Assistant examiner, CPCs, and Abstract. The patent badge does contain a link to the full patent document (in Adobe Acrobat format, aka pdf). To download or print any patent click here.
Patent No.:
Date of Patent:
Sep. 02, 1986
Filed:
Apr. 25, 1983
Andrew H Logan, Rancho Palos Verdes, CA (US);
John D Graves, Palos Verdes Estates, CA (US);
Hughes Helicopters, Inc., Culver City, CA (US);
Abstract
Autorotation in helicopters at low altitudes can be achieved even when the inherent design of the helicopter would prohibit successful entry into the autorotation mode. Angular kinetic energy from the main propulsion engine is stored in a flywheel which automatically transfers this energy to the main drive shaft in the event of engine failure. During normal operation, the flywheel is driven through the main drive shaft by coupling to a secondary drive shaft. The main drive shaft in turn is driven by the engine through an overrunning clutch assembly. The flywheel is maintained within an evacuated housing whereby air drag is substantially eliminated. In the event of engine failure, the overrunning clutch disengages the engine from the main drive shaft and flywheel will continue to apply energy to the main drive shaft through the secondary drive shaft to permit autorotation and a no-damage landing even at low altitude flight levels.