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36th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit | 2000

High Performance Combustor Cloth Seals

Mahmut Faruk Aksit; Bharat S. Bagepalli; Sami Aslam

Design of combustor seals poses a real challenge to designers who seek to achieve extended service life. In gas turbines with can-annular combustion systems, the combustor seals are used to seal the gap between the cans (transition duct) and the first stage nozzles. Combination of concentrated contact loads caused by thermal distortions and combustor dynamics limit the part service life. The introduction of flexible cloth seals has demonstrated the promise to extend the service life by 50% or more. However, to provide more air for combustion, and to satisfy decreasing NOx emissions limits, leakage reduction beyond existing levels is also required in addition to extending the service life. This paper describes the new combustor cloth seals designed to minimize leakage while extending the service life. Flexibility introduced by composite cloth assembly extends seal life by reducing contact load severity. Uniform slot contact minimizes leakage. To achieve maximum part life with minimum leakage rate, seal design has been optimized using statistical analysis tools. The systematic life improvement started with optimization of the metallic cloth. Once the process capability has been defined, the best vendor, weave and orientation were identified. Critical design areas have been identified through field inspections of prototypes. To minimize cloth wear in transition duct aft frame slots, seal slot engagements have been optimized using the tolerances on design parameters. The parameter values were assumed to be normally distributed within the tolerance bands. Inner-outer and side seal junctions have been redesigned to reduce contact load severity. Two separate Design of Experiments (DOE) series were conducted to develop load distribution transfer functions for both in-plane and out-of-plane cases representing the observed offset between neighboring * Copyright


Archive | 1998

Turbine spline seal and turbine assembly containing such spline seal

Bharat S. Bagepalli; Sami Aslam; Leslie Boyd Bedell; Mahmut Faruk Aksit


Archive | 2000

Fracture resistant support structure for a hula seal in a turbine combustor and related method

Maz Sutcu; Bernard Arthur Couture; Sami Aslam


Archive | 2000

Methods for robotically inspecting gas turbine combustion components

Kenneth John Hatley; Richard Michael Hatley; Sean Michael Mcdonnel; Michael John Bousquet; Thomas Arthur Wagner; Sami Aslam; Kathleen Lynne Bentzel


Archive | 2001

Method for inspecting and recording machine component condition data

Sami Aslam; Donald E. Woodmansee


Archive | 2001

Low leakage flexible cloth seals for turbine combustors

Mahmut Faruk Aksit; Jeffrey Arthur Benoit; Sami Aslam; Robert Bland; Bharat Sampathkumaran Bagepalli


Archive | 2002

Flexible cloth seal for turbine combustors

Mahmut Faruk Aksit; Sami Aslam; Bharat S. Bagepalli; Robert Bland; Jeffrey Arthur Ebnoit


Archive | 1999

Turbine seal and turbine assembly containing such spline seal

Mahmut Faruk Aksit; Sami Aslam; Bharat S. Bagepalli; Leslie Boyd Bedell


Archive | 2014

Method of robotically inspecting in situ an impingement sleeve of a gas turbine cannular combustion component

Kenneth John Hatley; Richard Michael Hatley; Michael John Bousquet; Sean Michael Mcdonnell; Thomas Arthur Wagner; Sami Aslam; Kathleen Lynne Bentzel


Archive | 2001

Fracture resistant support structure for hula seal in turbine combustion device and related method

Sami Aslam; Bernard Arthur Couture; Maz Sutcu; サミ・アスラム; バーナード・アーサー・コーター,ジュニア; マズ・スチュ

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