Trailing edge cooling using angled impingement on surface enhanced with cast chevron arrangements

Title: Trailing edge cooling using angled impingement on surface enhanced with cast chevron arrangements

Abstract

A gas turbine engine component, including: a pressure side (12) having an interior surface (34); a suction side (14) having an interior surface (36); a trailing edge portion (30); and a plurality of suction side and pressure side impingement orifices (24) disposed in the trailing edge portion (30). Each suction side impingement orifice is configured to direct an impingement jet (48) at an acute angle (52) onto a target area (60) that encompasses a tip (140) of a chevron (122) within a chevron arrangement (120) formed in the suction side interior surface. Each pressure side impingement orifice is configured to direct an impingement jet at an acute angle onto an elongated target area that encompasses a tip of a chevron within a chevron arrangement formed in the pressure side interior surface.

Inventors:: Lee, Ching-Pang; Heneveld, Benjamin E.; Brown, Glenn E.; Klinger, Jill

Issue Date:: 2015-05-26

Research Org.:: Siemens Aktiengesellschaft, Munchen, DE (United States)

Sponsoring Org.:: USDOE

OSTI Identifier:: 1182596

Patent Number(s):: 9,039,371

Application Number:: 14/068,070

Assignee:: Siemens Aktiengesellschaft (Munchen, DE) DOESC

DOE Contract Number:: SC0001359

Resource Type:: Patent

Country of Publication:: United States

Language:: English

Subject:: 33 ADVANCED PROPULSION SYSTEMS; 17 WIND ENERGY

Citation Formats


                    Lee, Ching-Pang, Heneveld, Benjamin E., Brown, Glenn E., and Klinger, Jill. Trailing edge cooling using angled impingement on surface enhanced with cast chevron arrangements.  United States: N. p., 2015. 
        Web.

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                    Lee, Ching-Pang, Heneveld, Benjamin E., Brown, Glenn E., & Klinger, Jill. Trailing edge cooling using angled impingement on surface enhanced with cast chevron arrangements.  United States.

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                    Lee, Ching-Pang, Heneveld, Benjamin E., Brown, Glenn E., and Klinger, Jill. Tue .  
        "Trailing edge cooling using angled impingement on surface enhanced with cast chevron arrangements".  United States.  https://www.osti.gov/servlets/purl/1182596.

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@article{osti_1182596,

  title        = {Trailing edge cooling using angled impingement on surface enhanced with cast chevron arrangements},

  author       = {Lee, Ching-Pang and Heneveld, Benjamin E. and Brown, Glenn E. and Klinger, Jill},

  abstractNote = {A gas turbine engine component, including: a pressure side (12) having an interior surface (34); a suction side (14) having an interior surface (36); a trailing edge portion (30); and a plurality of suction side and pressure side impingement orifices (24) disposed in the trailing edge portion (30). Each suction side impingement orifice is configured to direct an impingement jet (48) at an acute angle (52) onto a target area (60) that encompasses a tip (140) of a chevron (122) within a chevron arrangement (120) formed in the suction side interior surface. Each pressure side impingement orifice is configured to direct an impingement jet at an acute angle onto an elongated target area that encompasses a tip of a chevron within a chevron arrangement formed in the pressure side interior surface.},

  doi          = {},

  journal      = {},
number       = ,

  volume       = ,

  place        = {United States},

  year         = {2015},

  month        = {5}

}

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Works referenced in this record:

Designing a Turbine Blade Cooling System Using a Generalised Regression Genetic Algorithm
journal, January 2003

Roy, R.; Tiwari, A.; Corbett, J.
CIRP Annals, Vol. 52, Issue 1, p. 415-418
DOI: 10.1016/S0007-8506(07)60614-3

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Title: Trailing edge cooling using angled impingement on surface enhanced with cast chevron arrangements

Abstract

Citation Formats

Designing a Turbine Blade Cooling System Using a Generalised Regression Genetic Algorithm journal, January 2003

Designing a Turbine Blade Cooling System Using a Generalised Regression Genetic Algorithm
journal, January 2003