Method for increasing heat transfer from combustors

Metal working – Method of mechanical manufacture – Impeller making

Reexamination Certificate

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Details

C029S889210, C029S889220, C029S890010, C029S527200, C029S527500

Reexamination Certificate

active

06842980

ABSTRACT:
A combustor for a gas turbine engine includes a deflector assembly that enhances heat transfer from the combustor and minimizes low cycle fatigue stresses induced within the combustor. The deflector assembly includes a plurality of deflectors secured to a spectacle plate. Each deflector has tapered edges and includes a plurality of cylindrical projections extending outward from the deflector to facilitate heat transfer. The projections include rounded edges and are arranged in a high density pattern. The deflector is coated with a thermal barrier coating and a bondcoat to minimize exposure to hot combustion gases or flame radiation.

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patent: 10068524 (1998-03-01), None

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