The patent badge is an abbreviated version of the USPTO patent document. The patent badge does contain a link to the full patent document.

The patent badge is an abbreviated version of the USPTO patent document. The patent badge covers the following: Patent number, Date patent was issued, Date patent was filed, Title of the patent, Applicant, Inventor, Assignee, Attorney firm, Primary examiner, Assistant examiner, CPCs, and Abstract. The patent badge does contain a link to the full patent document (in Adobe Acrobat format, aka pdf). To download or print any patent click here.

Date of Patent:
Apr. 21, 2015

Filed:

Jul. 27, 2012
Applicants:

James P. Bangerter, Manchester, CT (US);

Dennis J. Duhamel, Oakdale, CT (US);

Robert M. Sonntag, Bolton, CT (US);

Reza Rezvani, Manchester, CT (US);

Inventors:

James P. Bangerter, Manchester, CT (US);

Dennis J. Duhamel, Oakdale, CT (US);

Robert M. Sonntag, Bolton, CT (US);

Reza Rezvani, Manchester, CT (US);

Assignee:

United Technologies Corporation, Hartford, CT (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F02C 1/00 (2006.01); F02G 3/00 (2006.01); F01D 9/02 (2006.01); F23R 3/00 (2006.01); F23R 3/06 (2006.01); F23R 3/50 (2006.01);
U.S. Cl.
CPC ...
F01D 9/023 (2013.01); F05D 2260/202 (2013.01); F23R 3/002 (2013.01); F23R 3/06 (2013.01); F23R 3/50 (2013.01); F23R 2900/00012 (2013.01); F23R 2900/03041 (2013.01); F23R 2900/03042 (2013.01); F23R 2900/03044 (2013.01);
Abstract

A turbine engine assembly includes a combustor and a stator vane arrangement having a plurality of stator vanes. The combustor includes a combustor wall that extends axially from a combustor bulkhead to a distal combustor wall end, which is located adjacent to the stator vane arrangement. The combustor wall includes a support shell with a plurality of impingement apertures, and a heat shield with a plurality of effusion apertures. The combustor wall end includes a plurality of circumferentially extending film cooled regions. At least one of the film cooled regions is circumferentially aligned with one of the stator vanes and includes a cooling aperture.


Find Patent Forward Citations

Bangerter, James. (2015). Turbine engine combustor and stator vane assembly (U.S. Patent No. 9010122). U.S. Patent and Trademark Office. https://idiyas.com/patent/badge/9010122

Data source: USPTO (United States Patent and Trademark Office) public patent records. Weekly synchronization. How IDiyas builds this profile

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