Title:
AIRCRAFT
Document Type and Number:
Japanese Patent JP2023179127
Kind Code:
A
Abstract:
To provide an aircraft of electrically-driven multiple rotors with an engine for electric power generation in which respective components are arranged in consideration of contacting with scattered engine debris in a case of rotor burst of the engine.SOLUTION: An aircraft 10 comprises: a gas turbine 44 which drives an electric generator 46; an electric motor 20 V5_1 which drives a rotor 18 V5; and an electric motor 20 V7_2 which drives a rotor 18 V7. The gas turbine 44 is arranged at a position overlapping with a rear wing 14b in a front-back direction of an airframe 12, and a high voltage harness 80 V5_1 transmitting electric power to the electric motor 20 V5_1 inside of the rear wing 14b is alienated from a high voltage harness 80 V7_2 transmitting electric power to the electric motor 20 V7_2 in the front-back direction of the airframe 12.SELECTED DRAWING: Figure 3
Inventors:
TOMIMATSU SUSUMU
Application Number:
JP2022092227A
Publication Date:
December 19, 2023
Filing Date:
June 07, 2022
Export Citation:
Assignee:
HONDA MOTOR CO LTD
International Classes:
B64D27/26; B64C11/46; B64D27/10; B64D27/24
Attorney, Agent or Firm:
Takehiro Chiba
Toshiyuki Miyadera
Takayuki Chima
Yasuharu Nakasone
Shiro Sakai
Tosuke Sekiguchi
Toshiyuki Miyadera
Takayuki Chima
Yasuharu Nakasone
Shiro Sakai
Tosuke Sekiguchi