Rsrc
J-GLOBAL ID:201110091870689671   Research Resource code:5000002737 Update date:Dec. 15, 2003

High pressure combustion test facility

高圧燃焼試験装置
Owning Organization:
Contact: SUZUKI Kazuo
Resource classification: Experience equipment, Facilities, etc
Overview:
High pressure combustion test facility
Main purpose: To examine combustion state, heat
transfer, exhaust characteristics of a gas turbine
combustor and a combustor element under high pressure.
Air source: 2 step booster by 720kW and 1,900kW
motor driven multistage centrifugal
compressors
Testing part:
Inlet air pressure 1 - 5MPa
Inlet air temperature: 400 - 730K
Inlet air flow rate: 4kg/s (max.)
Fuel: Lamp oil, methane gas
Completion: Fiscal 1982
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 organs are limited to a case approved
to be especially necessary for improvement of
aeronautical technology and space technology.

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