发明名称 |
Hybrid drive for helicopters |
摘要 |
The rotors of a helicopter are powered by electric motors. The electrical energy required for this purpose is produced by a motor-generator unit, which comprises one or more internal combustion engines. The motor-generator unit can be secured under the cabin floor. This yields a hybrid helicopter that can set the rotational frequency of the rotors within a large interval. |
申请公布号 |
US8870114(B2) |
申请公布日期 |
2014.10.28 |
申请号 |
US201213679209 |
申请日期 |
2012.11.16 |
申请人 |
EADS Deutschland GmbH;Airbus Helicopters Deutschland GmbH |
发明人 |
Botti Jean;Stuhlberger Johannes;Jänker Peter;Klöppel Valentin;Niesl Georg |
分类号 |
B64D27/00;B64D35/02;B64D27/04;B64D27/24;B64C27/14;B64D27/02;B64C27/04 |
主分类号 |
B64D27/00 |
代理机构 |
Lerner, David, Littenberg, Krumholz & Mentlik, LLP |
代理人 |
Lerner, David, Littenberg, Krumholz & Mentlik, LLP |
主权项 |
1. A hybrid helicopter comprising:
a hybrid drive; and a cabin floor; wherein the hybrid drive comprises:
a first motor;a second motor; anda generator unit; wherein the first motor is configured to power the generator unit; wherein the generator unit is configured to produce electrical energy for supplying the second motor; and wherein the second motor is an electric motor configured to power a rotor of the helicopter; wherein the first motor and the generator unit are arranged under the cabin floor of the helicopter. |
地址 |
DE |