Title:
ROTOR-REVOLUTION CONTROLLER FOR ROTOR AIRCRAFT
Document Type and Number:
Japanese Patent JPS62155199
Kind Code:
A
Abstract:
The present invention relates to a circulation flow control rotor system for an aircraft which includes rotor blades provided with slit shaped blower nozzles further comprising control devices for obtaining a cyclic or multicyclic or collective rotor blade angle control under utilization of individual pressure gas flow from a pressure chamber to the nozzle slits; further including deformable control members which are going to be deformed in accordance with certain rules underlying the requisite control.
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Inventors:
HERUBERUTO TSUIMAA
Application Number:
JP26440086A
Publication Date:
July 10, 1987
Filing Date:
November 06, 1986
Export Citation:
Assignee:
DORNIER GMBH
International Classes:
B64C27/06; B64C27/32; B64C27/46; B64C27/467; B64C27/82; (IPC1-7): B64C27/46
Attorney, Agent or Firm:
Kazuo Sato