Transition duct for gas turbine engine

Details Transition duct for gas turbine engine Transition duct for gas turbine engine

2006-10-13

2010-10-12

Cuff, Michael (Department: 3741)

Power plants

Combustion products used as motive fluid

Combustion products generator

Reexamination Certificate

active

07810334

ABSTRACT:
A transition duct having an inlet opening and an outlet opening and a body portion extending between the inlet and outlet openings at respective inlet and outlet ends. The inlet opening defines a generally circular cross-section for the body portion and has a geometric center, and the outlet opening defines a generally rectangular arc-like cross-section. The body portion has an internal profile substantially in accordance with coordinate values X, Y and Z at an angle θ, as set forth in Table 1, where each of the X, Y and Z coordinate values are taken at a sweep angle θ passing through the section origin and measured from a first plane defined by the inlet end and increasing toward a second plane defined by the outlet end.

REFERENCES:
patent: 6644032 (2003-11-01), Jorgensen et al.

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