Invention Grant
- Patent Title: Heat exchange module for a turbine engine
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Application No.: US16360329Application Date: 2019-03-21
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Publication No.: US11149644B2Publication Date: 2021-10-19
- Inventor: Frederick M. Schwarz , John T. Schmitz
- Applicant: Raytheon Technologies Corporation
- Applicant Address: US CT Farmington
- Assignee: Raytheon Technologies Corporation
- Current Assignee: Raytheon Technologies Corporation
- Current Assignee Address: US CT Farmington
- Agency: Getz Balich LLC
- Main IPC: F02C7/18
- IPC: F02C7/18 ; B64D33/12 ; F02C7/12 ; F02K3/077 ; B64D33/10 ; F01D25/14 ; B64D33/08 ; F01D25/08 ; F02C7/14 ; F02C7/32 ; F02K3/105 ; F02K3/115 ; B64D33/02 ; F28D21/00

Abstract:
A heat exchange module is provided for a turbine engine. The heat exchange module includes a duct and a plurality of heat exchangers. The duct includes a flowpath defined radially between a plurality of concentric duct walls. The flowpath extends along an axial centerline through the duct between a first duct end and a second duct end. The heat exchangers are located within the flowpath, and arranged circumferentially around the centerline.
Public/Granted literature
- US20190218973A1 HEAT EXCHANGE MODULE FOR A TURBINE ENGINE Public/Granted day:2019-07-18
Information query
IPC分类: