INTEGRATED THERMAL MANAGEMENT SYSTEM AND ENVIRONMENTAL CONTROL SYSTEM FOR A GAS TURBINE ENGINE
First Claim
Patent Images
1. A gas turbine engine comprising:
- a spool;
a first pump driven by said spool;
an air-oil cooler downstream of said first pump;
a second pump driven by said spool; and
an air-air precooler downstream of said second pump, said air-air precooler downstream of said air-oil cooler.
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Accused Products
Abstract
A gas turbine engine includes a first and second pump driven by a spool. An Air-Oil Cooler downstream of the first pump. An air-air precooler is downstream of the second pump, the air-air precooler downstream of the Air-Oil Cooler.
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Citations
20 Claims
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1. A gas turbine engine comprising:
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a spool; a first pump driven by said spool; an air-oil cooler downstream of said first pump; a second pump driven by said spool; and an air-air precooler downstream of said second pump, said air-air precooler downstream of said air-oil cooler. - View Dependent Claims (2, 3, 4, 5, 6, 7, 8, 9, 20)
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10. A gas turbine engine comprising:
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a spool; a constant speed transmission driven by said spool; a first pump driven by said constant speed transmission; an air-oil cooler downstream of said first pump; and an air-air precooler downstream of said an air-oil cooler. - View Dependent Claims (11, 12, 13, 14, 15)
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16. A gas turbine engine comprising:
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a low spool along an engine axis; a high spool along said engine axis; a first pump driven by said low spool; an air-oil cooler downstream of said first pump; an accessory gearbox driven by said high spool. - View Dependent Claims (17, 18, 19)
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Specification