Rsrc
J-GLOBAL ID:201110025257933230   Research Resource code:5000002736 Update date:Dec. 15, 2003

Medium pressure high temperature combustion test facility

中圧高温燃焼試験装置
Owning Organization:
Contact: SUZUKI Kazuo
Resource classification: Experience equipment, Facilities, etc
Overview:
Medium pressure high temperature combustion test
facility Main purpose: To examine combustion state,
heat transfer, exhaust characteristics of a gas
turbine combustor, a conbustor element and a ring
combustotr for practical machine up to 1MPa.
(1) Medium pressure combustion test facility
Air source: 720kW motor driven multistage
centrifugal compressor 2
Testing part:
Inlet air pressure 0.11 - 1.0MPa
Inlet air temperature: 400 - 1,200K
Inlet air flow rate: 0.4 - 3.6kg/s
Fuel: Lamp oil, methane gas, hydrogen gas
Completion: Fiscal 1982
(2) Ring combustor tester
Air source: 10,000kW motor driven multistage
centrifugal compressor
Testing part:
Inlet air pressure: 0.11 - 0.7MPa
Inlet air temperature: 500 - 700K
Inlet air flow rate: 8kg/sec
Fuel: Lamp oil
Completion: Fiscal 1975
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.

Return to Previous Page