Aircraft engine annular combustor test facility
Tests under high temperature and high pressure conditions, including an annular combustor for aircraft jet engines
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| Department | Aviation Technology Directorate |
|---|---|
| Air supply units | Pre-stage compressor: two 720 kW units, one 1,140 kW unit, one 2,240 kW unit, one 930 kW unit Post-stage compressor: one 10,000 kW unit |
| Standalone operation test (test using post-stage compressor only) | Maximum pressure: 0.8 Mpa Maximum air temperature: 673 K Maximum air flow rate: 8.5 kg/s |
| Series operation test (test using two-stage operations, a pre-stage compressor and post-stage compressor) | Maximum pressure: 1.8 Mpa Air temperature: 753 K Maximum air flow rate: 18.5 kg/s |
| Year of completion | Repairs in FY 2006 (constructed in FY 1975) |
| Fees | Standalone operation test: 149,698 yen/hour (Current as of April 1, 2024) Series operation test: 481,808 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. |