Nitrogen enriched air supply system and aircraft

Patent metadata

Field	Value
Publication number	US-9963239-B2
Application number	US-201314070811-A
Country	US
Kind code	B2
Filing date	Nov 4, 2013
Priority date	Nov 9, 2012
Publication date	May 8, 2018
Grant date	May 8, 2018

Abstract

To provide a system which supplies nitrogen enriched air (NEA) produced by using bleed air as a supply source of the NEA to a fuel tank, and which can further improve the fuel consumption. The present invention employs an NEA supply system 10 that controls a supply in a flow control valve (FCV) 11 so as to obtain a supply flow rate Fs as a value obtained by adding a small margin flow rate Fm to a required amount Fn of nitrogen enriched air required to be supplied to a first fuel tank 15 , in at least a part of a descent phase of an aircraft 100 . Accordingly, explosion of the first fuel tank 15 can be prevented, and the fuel consumption of an engine 1 can be improved in the descent phase.

First claim

What is claimed is:

1. A nitrogen enriched air supply system which supplies nitrogen enriched air that is enriched with nitrogen to a fuel tank of an aircraft, the system comprising:
a nitrogen enrichment unit that produces the nitrogen enriched air upon supply of bleed air from a flight engine of the aircraft;
a flow regulation unit that controls a supply of the nitrogen enriched air to the fuel tank;
a residual fuel detector that detects an amount of liquid fuel remaining in the fuel tank during a flight of the aircraft; and
a control unit that controls the supply in the flow regulation unit and acquires information regarding the amount of residual liquid fuel detected by the residual fuel detector,
wherein the control unit controls a supply flow rate Fs of the nitrogen enriched air which is supplied to the fuel tank so as to gradually increase in at least a part of a descent phase of the aircraft, the supply flow rate Fs being dependent upon the amount of residual liquid fuel remaining in the fuel tank.

2. The nitrogen enriched air supply system according to claim 1 , wherein the system further includes an altimeter that detects an altitude of the aircraft during a flight, the control unit acquires information regarding the altitude detected by the altimeter, and controls the supply flow rate Fs not to be increased, when the detected altitude reaches a reference value or a value lower than the reference value in the descent phase of the aircraft.

3. The nitrogen enriched air supply system according to claim 1 , wherein
an oxygen concentration in the nitrogen enriched air gradually increases, in at least the part of the descent phase of the aircraft.

4. The nitrogen enriched air supply system according to claim 1 , wherein
a nitrogen concentration in the nitrogen enriched air gradually decreases, in at least the part of the descent phase of the aircraft.

5. An aircraft comprising the nitrogen enriched air supply system according to claim 1 .

6. The nitrogen enriched air supply according to claim 1 , wherein the nitrogen enrichment unit comprises a polymer membrane that decreases a concentration of nitrogen contained in the nitrogen enriched air supplied to the fuel tank in the descent phase of the aircraft and increases a concentration of oxygen contained in the nitrogen enriched air supplied to the fuel tank in the descent phase of the aircraft.

7. The nitrogen enriched air supply according to claim 1 , further comprising:
a temperature instrument that detects a temperature of an internal space of the fuel tank,
wherein the control unit acquires information regarding the temperature detected by the temperature instrument, the supply flow rate Fs being dependent upon the temperature.

Assignees

• Mitsubishi Aircraft Corp

Inventors

• Fukuda Koki

Classifications

• B01D2053/224

  with hollow fibres · CPC title

• B01D2258/06

  Polluted air · CPC title

• B64D37/32 Primary

  Safety measures not otherwise provided for, e.g. preventing explosive conditions · CPC title

• B01D2259/4575

  in aeroplanes or space ships · CPC title

• G05D7/0635

  by action on throttling means (G05D7/0688, G05D7/0694 take precedence) · CPC title