二重機能航空機 - GENERAL ELECTRIC COMPANY

Title:

二重機能航空機

Document Type and Number:

Japanese Patent JP7214349

Kind Code:

B2

Abstract:

An aircraft 10 includes an electric power source 40 having a combustion engine 94 and an electric generator 96. The electric generator 96 is powered by the combustion engine 94. The aircraft 10 also includes a propulsion assembly 38 including a propulsor and an electric motor 86, the electric motor 86 configured for rotating the propulsor. The aircraft 10 also includes an electrical outlet 92 configured for connection with an outside power sink. The electrical outlet 92 and the propulsion assembly 38 are selectively in electrical communication with the electric power source 40 such that the electric power source 40 selectively provides electrical power to one of the electrical outlet 92 or the propulsion assembly 38.

More Like This:

WO/2022/146943	SYSTEM DEFINING A HYBRID POWER UNIT FOR THRUST GENERATION IN AN AERIAL VEHICLE AND METHOD FOR CONTROLLING THE SAME
WO/2020/184934	VERTICAL TAKE-OFF AND LANDING AIRCRAFT USING HYBRID ELECTRIC PROPULSION SYSTEM
JP6281740	Electric wave deception device

Inventors:

Randy M Bondrel
Glen David Crabtree
Dominique Baron

Application Number:

JP2018018792A

Publication Date:

January 30, 2023

Filing Date:

February 06, 2018

Export Citation:

Click for automatic bibliography generation Help

Assignee:

GENERAL ELECTRIC COMPANY

International Classes:

B64D27/24; B60L50/10; B64C29/00; B64C39/02

Domestic Patent References:

JP5085362A
JP2013505172A
JP2016534939A
JP2011528637A

Foreign References:

US20160137304
US20160375994
US20140248168
US20130099065
US20100252691
WO2015103013A1
WO2016196831A1

Attorney, Agent or Firm:

Masato Iida
Choe Yun
Kenji Tanaka
Satoshi Arakawa
Hiroshi Ogura
Takuto Tanaka

Previous Patent: Method for drying medical instruments

Next Patent: Compositions and methods for treating skin disorders using light and polycarboxylic acids