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Title:
AIR CRAFT ROTOR BLADE HAVING SHAPE ADAPTED FOR IMPROVEMENTS ON ACOUSTIC ISSUE DURING FLYBY AND PERFORMANCES DURING FORWARD FLIGHT
Document Type and Number:
Japanese Patent JP2017141014
Kind Code:
A
Abstract:
PROBLEM TO BE SOLVED: To provide a rotor blade for a rotorcraft to reduce noise made by the blade during flyby, while enhancing aerodynamic performances.SOLUTION: A front edge of the blade forms a front first sweep angle α1, which is greater than 0° and less than 10°with respect to a blade axis B, between a proximal end 3 and a second boundary S2, while forming a front second sweep angle α2, which is between 1° and 15°with respect to the blade axis B between the second boundary S2 and a third boundary S3, and forming a rear third sweep angle α3, which is between -35° and -15°with respect to the blade axis B between the third boundary S3 and a blade tip 9.SELECTED DRAWING: Figure 2

Inventors:
DEBBIE LEUSINK
DAVID ALFANO
VINCENT GARETON
Application Number:
JP2016238637A
Publication Date:
August 17, 2017
Filing Date:
December 08, 2016
Export Citation:
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Assignee:
AIRBUS HELICOPTERS
International Classes:
B64C11/18; B64C27/467
Domestic Patent References:
JPH11139397A1999-05-25
JPH0616190A1994-01-25
JPH1199994A1999-04-13
JP2002284099A2002-10-03
JPH11139397A1999-05-25
JPH0616190A1994-01-25
JPH1199994A1999-04-13
JP2002284099A2002-10-03
JP2012116477A2012-06-21
JP2008542110A2008-11-27
JP2005206148A2005-08-04
JP2002308192A2002-10-23
JP2000118499A2000-04-25
JP2012116477A2012-06-21
JP2008542110A2008-11-27
JP2005206148A2005-08-04
JP2002308192A2002-10-23
JP2000118499A2000-04-25
Foreign References:
US7252479B22007-08-07
EP2505500A12012-10-03
EP0842846A11998-05-20
US7252479B22007-08-07
EP2505500A12012-10-03
EP0842846A11998-05-20
Attorney, Agent or Firm:
Yoshiyuki Inaba
Toshifumi Onuki
Akihiko Eguchi
Kazuhiko Naito