公开(公告)号：US20190291599A1

公开(公告)日：2019-09-26

申请号：US16297881

申请日：2019-03-11

Applicant: DENSO CORPORATION

Inventor： Shinji ANDOU ,  Satoru YOSHIKAWA ,  Tetsuji MITSUDA

IPC: B60L53/24 ,  H02J7/00 ,  H02J7/14 ,  B64C39/02 ,  G05D1/00 ,  B60L50/10 ,  B60L50/50

Abstract: An electric power supply apparatus includes a first power supply unit, a second power supply unit, diodes, detection units, and an electric power control unit. The first power supply unit and the second power supply unit supply electric power to a thruster which is a load. The diodes are provided in the first power supply unit and the second power supply unit, respectively, to restrict reverse flow of currents to the power supply units. The detection units are provided between the first power supply unit and the thruster and between the second power supply unit and the thruster, respectively, to detect at least one of a voltage and a current. The electric power control unit controls electric power transmission between the first power supply unit and the second power supply unit based on detection values of the detection units.

公开(公告)号：US20130069591A1

公开(公告)日：2013-03-21

申请号：US13624049

申请日：2012-09-21

Applicant: DENSO CORPORATION ,  NIPPON SOKEN, INC.

Inventor： Seiji IYASU ,  Shinji ANDOU ,  Sadahisa ONIMARU ,  Kazuyoshi OBAYASHI

IPC: H02J7/00

CPC classification number: H02J7/1461 ,  H02J7/1453 ,  Y02T10/7005

Abstract: A battery charger of a battery charging apparatus is disposed on an exterior case of an engine in such a manner that a generated heat is transferred therebetween. An ECU drives a cooling system when an engine temperature and temperature of the battery charger satisfy a predetermined cooling temperature condition. A cooling capacity for cooling the battery charger is improved by establishing a heat radiation passage to radiate a heat from the battery charger efficiently.

Abstract translation: 电池充电装置的电池充电器以发生的热量传递到发动机的外壳上。 当电池充电器的发动机温度和温度满足预定的冷却温度条件时，ECU驱动冷却系统。 通过建立热辐射通道来有效地辐射来自电池充电器的热量来提高用于冷却电池充电器的冷却能力。

公开(公告)号：US20170158342A1

公开(公告)日：2017-06-08

申请号：US15367247

申请日：2016-12-02

Applicant: NIPPON SOKEN, INC. ,  DENSO CORPORATION

Inventor： Hiroki ISHII ,  Koji KAWASAKI ,  Takenori MATSUE ,  Shinji ANDOU ,  Hiroyasu BABA

IPC: B64D31/10 ,  B64C27/08 ,  G05D1/04 ,  G05D1/08 ,  G07C5/08

CPC classification number: B64D31/10 ,  B64C27/08 ,  B64C39/024 ,  B64C2201/024 ,  B64C2201/027 ,  B64C2201/108 ,  B64C2201/141 ,  G05D1/0072 ,  G05D1/042 ,  G05D1/0816 ,  G07C5/0808

Abstract: In an aerial vehicle, a malfunction determiner determines whether there is a malfunction in one of thrusters of the aerial vehicle. A flight controller activates the thrusters, and controls the output of each of the thrusters. The flight controller deactivates, when it is determined that there is a malfunction in one of the thrusters as a malfunctioned thruster, the malfunctioned thruster. The flight controller deactivates a selected thruster in the thrusters; the selected thruster being paired to the malfunctioned thruster, and controls the active thrusters except for the deactivated thrusters in all the thrusters to make the flight attitude of the aerial vehicle stable. The flight controller controls the active thrusters to cause the aerial vehicle to land while maintaining the flight attitude of the aerial vehicle being stable.