US 6,334,298 B1 · Gas turbine combustor having dome-to-liner joint

Abstract

A joint for joining a dome plate to a combustor liner includes a first flange formed on the dome plate and a second flange formed on the liner. A mounting ring having a groove formed therein is provided such that the first flange is disposed in the groove and the second flange engages the mounting ring. A retainer is secured to the mounting ring and engages the second flange.

Claims0

Dependent claims

Claims aren’t available for this document.

Facts

Application

09/616,258Filed 14 Jul 2000

Granted

1 Jan 2002

Term ends

Not estimatedThe source records don’t support an estimate.

Classification4 codes

F23R 3/283
Characterised by the fuel supply: attaching or cooling of fuel injecting means including supports for fuel injectors, stems, or lances
F23R 3/58
Characterised by the arrangement or form of the flame tubes or combustion chambers: cyclone or vortex type combustion chambers
F23R 3/60
Characterised by the arrangement or form of the flame tubes or combustion chambers: support structures; Attaching or mounting means
F23R
Generating combustion products of high pressure or high velocity

Gas turbine combustor having dome-to-liner joint

Life of this patent

Abstract

Claims0

Gas turbine combustor having dome-to-liner joint

Life of this patent

Abstract

Claims0