Title:
CONTROL DEVICE FOR STEERING BLADE
Document Type and Number:
Japanese Patent JP3565811
Kind Code:
B2
Abstract:
PROBLEM TO BE SOLVED: To enhance fuel consumption efficiency by reducing air resistance of an aircraft in flight.
SOLUTION: Since the steering blade 23 is rocked using a rocking actuator 25 in which a carrier 48 (final output shaft) is coaxial to a rocking center of the steering blade 23, a conversion mechanism (fixed link or the like) for converting the linear motion of a cylinder to rotational motion is not required as is different from a prior art. As a result, fairing for covering the conversion mechanism is not required. Accordingly, the air resistance of the aircraft in flight is reduced, thereby enhancing the fuel consumption efficiency.
Inventors:
Takashi Koizumi
Toshio Kamimura
Toshio Kamimura
Application Number:
JP2001311003A
Publication Date:
September 15, 2004
Filing Date:
October 09, 2001
Export Citation:
Assignee:
TS Corporation
International Classes:
B64C9/02; B64C13/24; B64C13/28; B64C13/34; B64C13/50; F16H1/28; H02K7/10; (IPC1-7): B64C13/50; F16H1/28; H02K7/10
Domestic Patent References:
| JP3292292A | ||||
| JP2001074121A | ||||
| JP5069895A | ||||
| JP2283938A | ||||
| JP9328098A |
Attorney, Agent or Firm:
Toshio Tada
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