Invention Grant
- Patent Title: Gas turbine engine heat exchanger
- Patent Title (中): 燃气涡轮发动机热交换器
-
Application No.: US13336378Application Date: 2011-12-23
-
Publication No.: US09410482B2Publication Date: 2016-08-09
- Inventor: Michael Stephen Krautheim , Carlos Soto-Gonzalez
- Applicant: Michael Stephen Krautheim , Carlos Soto-Gonzalez
- Applicant Address: US IN Indianapolis
- Assignee: Rolls-Royce North American Technologies, Inc.
- Current Assignee: Rolls-Royce North American Technologies, Inc.
- Current Assignee Address: US IN Indianapolis
- Agency: Fishman Stewart PLLC
- Main IPC: F02C7/052
- IPC: F02C7/052 ; F02K3/06 ; F02K3/115 ; F02C7/141

Abstract:
A gas turbine engine having a heat exchanger is disclosed. In one form the gas turbine engine includes a particle separator that can be used to separate particles or foreign objects and create a dirty flow and a clean flow. A blower can be used to discharge the particles or foreign objects from the separator. The heat exchanger includes a relatively warm flow path from a downstream region of a compressor and a relatively cool flow path from an upstream region of the compressor. The relatively cool flow path is merged with the dirty flow. In another embodiment, the gas turbine engine is a turbofan and the relatively cool flow path is merged with a bypass flow. In one embodiment of the engine the relatively warm flow path, after having exchanged heat with the relatively cool flow path is delivered to a working component without passing through a turbomachinery component.
Public/Granted literature
- US20120159961A1 GAS TURBINE ENGINE HEAT EXCHANGER Public/Granted day:2012-06-28
Information query
IPC分类: