Rsrc
J-GLOBAL ID:201110004858632710   Research Resource code:5000002735 Update date:Dec. 15, 2003

Atmospheric pressure combustion test facility

常圧燃焼試験設備
Owning Organization:
Contact: SUZUKI Kazuo
Resource classification: Experience equipment, Facilities, etc
Overview:
Atmospheric pressure combustion test facility
Main purpose: To execute an atmosphere open combustion
test of a gas turbine combustor and a combustor element.
(1) Atmospheric combustion test facility 1
Testing part:
Inlet air temperature: 300 - 600K
Inlet air flow rate: 0.8kg/sec maximum
Fuel: Lamp oil
Completion: Fiscal 1990
(2) Atmospheric combustion test facility 2
Testing part:
Inlet air temperature: 450 - 1,200K
Inlet air flow rate: 0.03 - 0.1kg/sec maximum
Fuel: Lamp oil
Completion: Fiscal 1990
(3) Atmospheric combustion test facility 3
Testing part:
Inlet air temperature: 400 - 700K
Inlet air flow rate: 1.0kg/sec maximum
Fuel: Lamp oil, methane gas, hydrogen gas
Completion: Fiscal 1983
User environment and conditions:
It is required not to disturb execution of research work by this Laboratory.
User procedures and method:
[Procedure for Use]
Refer in detail to Business Squad, Planning Room.
[Charge for Use]
According to the calculation standard of acceptance
research expenses appointed by the Science and
Technology Agency
[Restriction for use]
Uses by a person not belonging to national
administration are limited to a case approved to
be especially necessary for improvement of
aeronautical technology and space technology.

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