Honda Motor Co., Ltd.

Azuki Ichikawa

Yuichi Fukuchi

Takuya Kubota

Hikari Hirayanagi

Toshinori Tsukamoto

Kazutaka Nakada

Yuhei Noguchi

An aircraft including a fuselage with a cooling unit including a first radiator, a second radiator, a first cooling fan and a second cooling fan for taking air outside the fuselage into the fuselage and supplying air to the first radiator and the second radiator. The aircraft has an exhaust orifice for discharging air delivered into the interior of the fuselage, the cooling unit is arranged forward of the engine in the fuselage, and the exhaust orifice is positioned rearward of the engine in the fuselage.

Aircraft

The aircraft includes a fuselage, an engine disposed in the fuselage, an exhaust outlet provided at a tail of the fuselage for discharging exhaust gas from the engine to the outside, and a cruise rotor positioned rearward of the exhaust outlet and generating horizontal thrust on the fuselage. The exhaust outlet and the cruise rotor do not overlap each other when viewed from the direction in which the exhaust gas is discharged.

Freezing of an electrical component of a VTOL rotor is prevented. The aircraftincludes a fuselage, a VTOL rotorincluding one or more bladesthat is supported on the boomto be spaced apart from the fuselage for generating thrust in a vertical direction during take-off and landing, a motorthat is stored in the boom and is configured to cause the one or more blades to rotate, and an inverterfor controlling the motor, a detection unitconfigured to detect a temperature of at least one apparatus of the motor or the inverter, and a control unitconfigured to run the at least one apparatus based on a thrust request for a plurality of VTOL rotors and a detection result of the temperature.

Aircraft comprising a control unit to run at least one of rotational apparatus or control apparatus based on temperature

A gas mixing device for a moving object including a discharge flow path that discharges an exhaust gas from a gas turbine engine. The discharge flow path includes a tubular portion, a communication passage that allows an inside of the tubular portion and the gas turbine engine to communicate with each other, and a plurality of guide portions that extend radially inward from the tubular portion and guide the cooling gas to a radially central portion of the tubular portion. The plurality of guide portions are spaced from each other in a circumferential direction of the tubular portion, and the extended end portions of the plurality of guide portions are spaced from each other.

Gas mixing device and moving object

A mixer is mounted in an aircraft. A rear end part of a cylindrical portion of the mixer is divided by a guide vane into a plurality of divided tubular portions. In the plurality of divided tubular portions, a notch nozzle is formed on an outer wall of the cylindrical portion. A plurality of guide holes are formed to extend from the outer wall of the cylindrical portion to a rear end surface of the guide vane.

Mixer and mobile body

An internal combustion engine equipped with a turbocharger () including a turbine () and a compressor () that are arranged in a coaxial relationship, the internal combustion engine includes an exhaust pipe () extending from an outlet () of the turbine along a side of the compressor, an actuator () attached to a part of the compressor for controlling a flow path of the turbocharger, and a fluid pipe () conducting fluid and extending through a space defined between the exhaust pipe and the actuator.

Growing community of inventors

Wako, Japan

Azuki Ichikawa