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:
Dec. 21, 1993

Filed:

Jul. 09, 1992
Applicant:
Inventors:

Andrew Shepherd, Fairfield, OH (US);

Richard W Albrecht, Fairfield, OH (US);

Robert J Corsmeier, Cincinnati, OH (US);

Assignee:

General Electric Company, Cincinnati, OH (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F01D / ;
U.S. Cl.
CPC ...
41520920 ; 415189 ; 4152093 ;
Abstract

In a gas turbine engine having an annular casing with a stationary support structure, a high pressure turbine, and an annular high pressure turbine nozzle having at least one stage which includes a plurality of circumferentially aligned nozzle segments and which is disposed in the annular casing between a combustor and the high pressure turbine, a nozzle support arrangement is provided for mounting each nozzle segment to the stationary support structure. The arrangement includes a single mounting pin mounted on and extending from an annular nozzle support flange on the casing support structure and a hole defined in an oval shape in the one end portion of an inner band flange for receiving the mounting pin in an interference fitting relation. The oval-shaped hole has a greater height than width such that a tight tangential fit of the pin with the hole is provided along the width of the hole and a loose fit of the pin with the hole is provided along the height of the hole so as to ensure negligible variation of the tangential location of the nozzle segments relative to one another and to the support structure, while allowing free axial rocking of the nozzle segment on the inner band without bending the pin nor the support flange.


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