Title:
FUEL SYSTEM AND AIRCRAFT
Document Type and Number:
Japanese Patent JP2015030447
Kind Code:
A
Abstract:
PROBLEM TO BE SOLVED: To provide a fuel system of a configuration simply formed with a small number of members for reducing the fuel amount stored in a second tank before the fuel amount stored in a first tank.SOLUTION: A fuel system 10 comprises: an outer tank 30 (first tank) and an inner tank (second tank) 40, which store fuel, respectively; a fuel supply pump 31 for supplying the fuel in at least the outer tank 30 of the outer tank 30 and the inner tank 40 to a fuel consumption part; a transfer pump 23 for transferring the fuel in the inner tank 40 into the outer tank 30; and a fuel passage 20 having an inlet 21 communicating with the inside of the outer tank 30 and an outlet 22 communicating with the inside of the inner tank 40. The fuel in the outer tank 30 is overflowed into the inner tank 40 through the fuel passage 20.
Inventors:
KOMODA USHIO
Application Number:
JP2013163987A
Publication Date:
February 16, 2015
Filing Date:
August 07, 2013
Export Citation:
Assignee:
MITSUBISHI AIRCRAFT CORP
International Classes:
B64D37/14
Foreign References:
| US20100051749A1 | 2010-03-04 | |||
| US20120193479A1 | 2012-08-02 |
Attorney, Agent or Firm:
Mitsuru Oba
beauty -- Yuki Horikawa
Otake Yuka child
beauty -- Yuki Horikawa
Otake Yuka child
Previous Patent: VEHICLE SLIDE WINDOW AND FIXING METHOD OF TRIM BOARD
Next Patent: METHOD FOR LOAD JET IN AIRCRAFT AND CONTROLLER
Next Patent: METHOD FOR LOAD JET IN AIRCRAFT AND CONTROLLER