Rolls-royce Corporation

Western Michigan University

Richard-allan Scientific Company

Nathanael Cooper

Michael Nesteroff

Mark E Whitlock

Steven Mazur

Paul Melevage

Jonathan Acker

Keith Owen Whittlinger

Grace Aker

Jennifer H Freeland

Cassandra Cummings

Younes Khamliche

Parviz Merati

A gas turbine engine includes a fan, a compressor, a combustor, and a turbine. The compressor compresses gases entering the gas turbine engine. The combustor receives the compressed gases from the compressor and mixes fuel with the compressed gases. The turbine receives the hot, high pressure combustion products created by the combustor by igniting the fuel mixed with the compressed gases. The turbine extracts mechanical work from the hot, high pressure combustion products to drive the fan and compressor.

Turbine engine with centrifugal compressor having impeller backplate offtake

A compressor assembly for a gas turbine engine includes a shroud assembly, an outer case assembly, and a plurality of locating bolt assemblies. The shroud assembly extends circumferentially around the engine axis. The outer case assembly includes an outer case that extends circumferentially around the axis and a plurality of fasteners that couple the shroud assembly with the outer case. The plurality of locating bolt assemblies extend into the outer case and abut the shroud assembly at a predetermined axial location to axially locate the shroud assembly.

Adjustable position impeller shroud for centrifugal compressors

A compressor assembly for a gas turbine engine comprising an outer case, a shroud arranged circumferentially around the axis to direct compressed air through an impeller, and an actuator coupled with the outer case and the shroud to vary the position of the shroud axially relative to the outer case. The actuator includes a mount arm, an actuator body, and a travel stop. The mount arm is coupled with the outer case. The actuator body is coupled with the mount arm and the shroud to control axial movement of the shroud relative to the outer case. The travel stop is coupled to the mount arm and extends away from the mound arm and is configured to limit a forward most axial position of the shroud relative to the outer case.

Travel stop for a tip clearance control system

A compressor shroud assembly is disclosed comprising a dynamically moveable impeller shroud, a static compressor casing, an air piston mounted between said impeller shroud and said compressor casing, and a clearance control system. The air piston effects axial movement of said impeller shroud responsive to a supply of actuating air. The clearance control system regulates the pressure of actuating air in said air piston and comprises a supply conduit having a supply modulating valve and a discharge conduit having a blowoff check valve. The blowoff check valve is set to open at a predetermined differential pressure between pressure of the air piston and pressure of the supply of actuating air.

Clearance control system for a compressor shroud assembly

A centrifugal impeller shroud assembly has a dynamically moveable impeller shroud for encasing a rotatable centrifugal impeller and resolving misalignment between the impeller shroud and the rotatable centrifugal impeller. The assembly comprises a static casing, an impeller shroud, a shroud arm, and a thermal member. The shroud arm is coupled between the casing and the impeller shroud. The thermal member is coupled to the impeller shroud and has a coefficient of thermal expansion (CTE) lower than the CTE of the shroud. The shroud arm comprises a flexible portion configured to flex responsive to a differential pressure across the shroud arm.

Passive clearance control for a centrifugal impeller shroud

A tissue cassette includes a body having a first floor and a first perimeter wall encircling and extending from the first floor so that the first floor and first perimeter wall at least partially bound a body cavity, the first floor having a plurality of spaced apart openings extending therethrough. A mold has a second floor and a second perimeter wall encircling and extending from the second floor so that the second floor and second perimeter wall at least partially bound a mold cavity, the second floor having at least one micropore extending therethrough, the at least one micropore having a maximum diameter less than 0.040 inches. A hinge couples the body to the mold so that the body and mold can move between a closed position wherein the first floor overlies the second floor so as to form a tissue compartment therebetween and an open position.

Growing community of inventors

Avon, IN, United States of America

Nathanael Cooper