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发明授权
CN101522523B 用于飞行器的具有多个能量转换器的推进装置 有权

用于飞行器的具有多个能量转换器的推进装置
摘要：
本发明涉及一种用于飞行器的推进装置。该推进装置包括第一能量转换器(4)，第二能量转换器(5)和推进单元(1)。第一能量转换器(4)提供第一推进能量，并且第二能量转换器(5)提供第二推进能量。第一能量转换器(4)和第二能量转换器(5)适于为推进单元(1)提供第一推进能量和第二推进能量。
摘要（英）：

The present invention relates to a propulsion device for an aircraft. The propulsion device comprises a first energy converter (4), a second energy converter (5) and a propulsion unit (1). The first eThe present invention relates to a propulsion device for an aircraft. The propulsion device comprises a first energy converter (4), a second energy converter (5) and a propulsion unit (1). The first energy converter (4) provides first propulsion energy, and the second energy converter (5) provides second propulsion energy. The first energy converter (4) and the second energy converter (5) are adapnergy converter (4) provides first propulsion energy, and the second energy converter (5) provides second propulsion energy. The first energy converter (4) and the second energy converter (5) are adapted to provide the first propulsion energy and the second propulsion energy to the propulsion device (1).ted to provide the first propulsion energy and the second propulsion energy to the propulsion device (1).

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