Honda Motor Co., Ltd.

Yuya Ishihara

Tomohiro Fukazu

Akinori Kita

Takeshi Matsumoto

Daiko Tsutsumi

Daisuke Komazawa

Takanori Suzuki

Masashi Eto

Yuji Ishitsuka

Takuro Tominaga

Daichi Yamanaka

Shosei Nishikawa

Koji Muraoka

A control systemincludes: a VTOL rotorand a cruise rotorconfigured to generate a thrust; a power unit that has a power generation deviceconfigured to generate power and supply the power to the rotors, and a batteryconfigured to store power which is supplied from the power generation device, and supply stored power to the rotors; and a control unitconfigured to calculate a charging time of the battery based on a required amount of power storage that should be stored in the battery when the aircraft flies in a predetermined flight condition, and a state of the battery, and determine a charge start time of the battery based on the charging time and a flight time it takes to reach the predetermined flight condition. With this, it is possible to suppress a deterioration.

Control system and control method, and aircraft

A battery module includes a plurality of battery cells connected in series. Each of the battery cells has a rectangular thin plate shape, and includes a thin plate-shaped positive electrode tab and a thin plate-shaped negative electrode tab, which are provided on one side of the battery cell. Among the battery cells, the side of one battery cell where the positive electrode tab and the negative electrode tab are provided and the side of another battery cell where the positive electrode tab and the negative electrode tab are provided, are arranged so as to face each other. The positive electrode tab of the one battery cell and the negative electrode tab of the other battery cell are overlapped with each other in a thickness direction of the battery cells and in contact with each other.

Battery module

A hybrid aircraft that flies by using a plurality of rotors (takeoff and landing rotors and cruise rotors) includes a generator, a battery charged with power generated by the generator, a plurality of electric motors that rotate the respective rotors by the power generated by the generator and power supplied from the battery, and a controller that sets a target remaining capacity of the battery according to a flight state of the aircraft and controls charging and discharging of the battery so that the remaining capacity of the battery approaches the target remaining capacity.

Hybrid aircraft

In a battery pack, a housing includes an exhaust portion provided on an upper side in a gravity direction with respect to a housing portion that houses a live part. The exhaust portion includes: a storage portion configured to store a liquid; a first communication portion that communicates between an interior of the housing portion and an interior of the exhaust portion; and a second communication portion that communicates between an outside of a housing and an inside of the exhaust portion. When the battery pack is viewed from the upper side in the gravity direction, an opening of the second communication portion on an inner side of the exhaust portion is provided at a position that overlaps the storage portion and that does not overlap an opening of the first communication portion on the inner side of the exhaust portion.

Battery pack and aircraft

Before power is supplied to a load from a capacitor and a plurality of batteries, a battery for initially supplying power for charging to the capacitor is determined from among the plurality of batteries, based on a result of acquiring the voltage of each battery, and voltage equalization of the plurality of batteries is performed in response to power for charging being supplied to the capacitor from the determined battery.

Battery control apparatus for power supply system

A storage system for a flying object is equipped with a landing portion having a landing surface on which the flying object can land, and a storage main body for storing the flying object that has landed on the landing surface. The storage main body includes opening and closing portions that cover the landing surface. The storage system is further equipped with retaining mechanisms adapted to retain the flying object in a state of having landed on the landing surface from a direction perpendicular to the landing surface.

Storage system for flying object

To provide a power unit structure for an electrically driven vehicle which can decrease design man-hours, as well as raise the rigidity of the unit. A control device unit for an electrically driven vehicle includes: a first mounting part which is a mounting part of a power supply unit that supplies electric power to an electric motor, and a second mounting part which fixes the control device unit to an electric motor unit; and the control device unit is mounted from a transmission case side of the electric motor unit towards an electric motor case side, the first mounting part being mounted to a central case, and the second mounting part being mounted to the transmission case.

Power unit structure for electrically driven vehicle

Disclosed are a bus bar unit capable of being easily manufactured while preventing a bus bar from being separated from a magnetic core and also capable of being reduced in size, and a manufacturing method thereof. The bus bar unit includes a magnetic core having a through-hole and covered with an insulating material, U-phase, V-phase and W-phase bus bars of which main body portions are arranged in parallel with each other in a predetermined direction within the through-hole and one side connecting portions provided on one side in an axial direction of the through-hole from the main body portions are bent in a direction crossing the axial direction, and a base member formed of an insulating material and to which the magnetic core is fixed, wherein the one side connecting portions of the bus bars are held while being disposed between the base member and the magnetic core.

Bus bar unit and manufacturing method thereof

A cable structure includes a first cable, a second cable, a communicating portion, and a ventilation-tube connecting portion. The first cable includes a first power line, a first connector, a second connector, and a first tube. The first tube covers the first power line and has a first space. The second cable includes a second power line, a third connector, a fourth connector, and a second tube. The second tube covers the second power line and has a second space. The first space communicates with the second space via the communicating portion. The ventilation-tube connecting portion is provided at the first tube or the second tube. The ventilation-tube connecting portion is connected to a ventilation tube through which the first space and the second space are ventilated.

Cable structure and vehicle

Disclosed is a vehicle body lower structure which is capable of suppressing an increase in a vehicle weight, ensuring a degree of freedom of a layout of vehicle parts and also protecting an electric power converter. In the vehicle body lower structure, the electric power converter is provided between a first cross member and a second cross member. The electric power converter includes an electric power converter body, a first support portion and a second support portion. The electric power converter is disposed between the first cross member and the second cross member. The first support portion is provided at the electric power converter body and supported by the first cross member. The second support portion is provided at the electric power converter body and supported by the second cross member. The second support portion has a weak portion which is deformable by an impact load.

Growing community of inventors

Wako, Japan

Yuya Ishihara