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