Testing gas turbine combustors and other equipment under high pressure conditions
Research mainly of combustion performance, exhaust characteristics, and cooling performance
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| Department | Aviation Technology Directorate |
|---|---|
| Air supply units | Two 720 kW units; motor driven multi-stage centrifugal compressor |
| Sample section | Inlet air pressure: 0.11 to 1 Mpa Inlet air temperature: 400 to 1,200 K Inlet airflow volume: 0.4 to 3.6 kg/s |
| Year of completion | FY 1982 |
| Fees | 49,455 yen/hour (Current as of April 1, 2024) *The usage fee above includes the general management fee. *The usage fee above does not include technical fees and consumption tax. These fees will be charged separately. *The usage fee above does not include required support fees, such as for operations. These fees will be charged separately depending mainly on the test details. *The usage fee is calculated each fiscal year. In addition, prices may be revised without notice midway through the fiscal year. Inquire using the form below for details. |
