To provide a power system architecture for aircraft.SOLUTION: An electrical power system 100 for regenerative loads includes a DC bus 110, 160 and an electrical actuator load 112, 162, where back-driving the electrical actuator load generates regenerative electrical energy, and where the electrical actuator load is configured to transmit the regenerative electrical energy to the DC bus. The system may also include at least one additional load 114, 164, where at least a portion of the regenerative electrical energy is transmitted to the at least one load.SELECTED DRAWING: Figure 1
【課題】航空機用の電力システム構造を提供する。【解決手段】回生負荷のための電力システム100は、DCバス110、160及び電気アクチュエータ負荷112、162を含み、電気アクチュエータ負荷を逆駆動することにより回生電気エネルギーを生成し、電気アクチュエータ負荷は、回生電気エネルギーをDCバスへ伝達する。本システムはまた、少なくとも一つの追加の負荷114、164を含み、回生電気エネルギーの少なくとも一部が、少なくとも一つの負荷へ伝達される。【選択図】図1
POWER SYSTEM ARCHITECTURE FOR AIRCRAFT WITH ELECTRICAL ACTUATION
電気作動を有する航空機用の電力システム構造
2019-10-17
Patent
Electronic Resource
Japanese
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