Invention Grant
US08109728B2 Adjusting apparatus for adjusting the pitch angle of propeller blades, variable-pitch propeller, control function which can be implemented in a computer, and method for adjusting the pitch angle of propeller blades
有权
用于调节螺旋桨叶片的俯仰角的调节装置,可变桨距螺旋桨,可在计算机中实现的控制功能以及用于调节螺旋桨叶片的俯仰角的方法
- Patent Title: Adjusting apparatus for adjusting the pitch angle of propeller blades, variable-pitch propeller, control function which can be implemented in a computer, and method for adjusting the pitch angle of propeller blades
- Patent Title (中): 用于调节螺旋桨叶片的俯仰角的调节装置,可变桨距螺旋桨,可在计算机中实现的控制功能以及用于调节螺旋桨叶片的俯仰角的方法
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Application No.: US12306429Application Date: 2007-06-25
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Publication No.: US08109728B2Publication Date: 2012-02-07
- Inventor: Klaus-Peter Neitzke , Andreas Ulrich
- Applicant: Klaus-Peter Neitzke , Andreas Ulrich
- Applicant Address: DE Hamburg
- Assignee: Airbus Deutschland GmbH
- Current Assignee: Airbus Deutschland GmbH
- Current Assignee Address: DE Hamburg
- Agency: Greenblum & Bernstein, P.L.C.
- Priority: DE102006029057 20060624
- International Application: PCT/IB2007/052451 WO 20070625
- International Announcement: WO2008/001299 WO 20080103
- Main IPC: B64C27/00
- IPC: B64C27/00 ; B64C11/06 ; B64C11/30 ; B63H1/06 ; F01D7/00 ; F03B3/14 ; F04D29/36

Abstract:
Apparatus for adjusting pitch angle of propeller blades of a variable-pitch propeller. The blades being adjustable in a first blade pitch-angle range with positive pitch angles, in a second blade pitch-angle range, and in a third blade pitch-angle range with negative pitch angles. The second blade pitch-angle range is an intermediate range located between the first and the third blade pitch-angle range, which includes the pitch-angle range where blade drag is a minimum, and ranges of positive pitch angles with low thrust and of negative pitch angles with low reverse thrust. The apparatus provides adjustment of the propeller blades from the first to the third blade pitch-angle range and vice versa, and is designed to be operated so that at least a first group of propeller blades can be rotated through the second blade pitch-angle range, while propeller blades in another group are in a positive blade pitch-angle range.
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