Invention Grant
- Patent Title: Aerodynamically active stiffening feature for gas turbine recuperator
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Application No.: US13804118Application Date: 2013-03-14
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Publication No.: US09724746B2Publication Date: 2017-08-08
- Inventor: Andreas Eleftheriou , Daniel Alecu , David Menheere
- Applicant: PRATT & WHITNEY CANADA CORP.
- Applicant Address: CA Longueuil
- Assignee: PRATT & WHITNEY CANADA CORP.
- Current Assignee: PRATT & WHITNEY CANADA CORP.
- Current Assignee Address: CA Longueuil
- Agency: Norton Rose Fulbright Canada LLP
- Main IPC: B21D53/04
- IPC: B21D53/04 ; F02K1/82 ; F02C7/08 ; F28F3/04 ; F28F13/06 ; B21D49/00 ; F28F13/02 ; F28D7/16 ; F28D9/00 ; F28D21/00

Abstract:
A recuperator disposed in the exhaust duct of a gas turbine engine includes a plurality of recuperator plates arranged in a spaced-apart relationship to define therebetween a plurality of interstices and fluid channels, the plurality of interstices adapted to direct therethrough at least one first stream received at a leading plate edge of the recuperator plates and the plurality of fluid channels adapted to direct therethrough at least one second stream to effect heat exchange between the at least one first stream and the at least one second stream. Each recuperator plate includes, formed at the leading plate edge thereof, a first concavity extending along the leading edge in a direction substantially parallel to a longitudinal axis of the plate. The first concavity extends transversely to a direction of the at least one first stream flowing over each recuperator plate.
Public/Granted literature
- US20140260178A1 AERODYNAMICALLY ACTIVE STIFFENING FEATURE FOR GAS TURBINE RECUPERATOR Public/Granted day:2014-09-18
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