Cooling circuit for enhancing turbine performance
A cooling circuit, turbine technology, used in turbine/propulsion cooling, engine cooling, mechanical equipment, etc.
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[0022] Referring to Figure 1, the system uses seals 12, such as brush seals, adjustable seals, etc., to prevent excessive airflow from the compressor discharge and secondary (bypass) cooled cooling air system to compensate for Overall required purge airflow and cooling of critical components. The adjustable seal may be one that retracts during engine transients to minimize wear or damage to the seal, or the adjustable seal may be one that is adjusted in use to suit the performance of the seal. degradation.
[0023] Before sealing all critical components and the existing honeycomb, a seal 12 is placed upstream or adjacent to the inlet of the HPP circuit. As mentioned, the seal can be a traditional brush seal, an adjustable seal with an actuation system, etc.
[0024] The intake duct 14 or intake duct 14 is positioned to receive compressor discharge. Preferably, the circuit comprises two intake ducts 14 or ducts 14 of approximately 3" diameter.
[0025] In intake duct 14 the...
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