发明名称 |
ROTORCRAFT WITH AT LEAST ONE MAIN ROTOR AND AT LEAST ONE COUNTER-TORQUE ROTOR |
摘要 |
A rotorcraft with at least one main rotor 1a and at least one counter-torque rotor, comprising: at least one duct-type portion provided with a shroud that defines at least one transverse duct, the at least one counter-torque rotor comprising a plurality of counter-torque rotor blades and being rotatably arranged within the at least one transverse duct, and a drive shaft fairing that is fixedly supported within the at least one transverse duct and that rotatably supports the at least one counter-torque rotor, the drive shaft fairing comprising a leading edge facing the at least one counter-torque rotor, the leading edge being at least partially equipped with associated acoustical damping means. |
申请公布号 |
US2015246726(A1) |
申请公布日期 |
2015.09.03 |
申请号 |
US201514630980 |
申请日期 |
2015.02.25 |
申请人 |
AIRBUS HELICOPTERS DEUTSCHLAND GMBH ;EADS DEUTSCHLAND GMBH |
发明人 |
PONGRATZ Reinhard;SCHNEIDER Sascha |
分类号 |
B64C27/82;B64C27/32;B64C27/00 |
主分类号 |
B64C27/82 |
代理机构 |
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代理人 |
|
主权项 |
1. A rotorcraft with at least one main rotor and at least one counter-torque rotor, comprising:
at least one duct-type portion provided with a shroud that defines at least one transverse duct, the at least one counter-torque rotor comprising a plurality of counter-torque rotor blades and being rotatably arranged within the at least one transverse duct, and a drive shaft fairing that is fixedly supported within the at least one transverse duct and that rotatably supports the at least one counter-torque rotor, the drive shaft fairing comprising a leading edge facing the at least one counter-torque rotor, the leading edge being at least partially equipped with associated acoustical damping means. |
地址 |
Donauworth DE |