Hamilton Sundstrand Corporation

Collins Engine Nozzles, Inc.

Murtuza Lokhandwalla

Brandon Phillip Williams

Todd Haugsjaahabink

Jason Allen Ryon

Darryl A Colson

Charles E Reuter

Christopher McAuliffe

Jay W Kokas

Richard E Versailles

Craig M Beers

Russell P Rourke

Michael Ferrarotti

John D Monacchio

Haralambos Cordatos

Leo J Veilleux, Jr

Brent J Merritt

Mark R Gurvich

Harold W Hipsky

Clarence J Wytas

Brian R Shea

Lance R Bartosz

Andrew M Caldecutt

Jesse C Peters

Blair A Smith

Eric Surawski

Seth E Rosen

Eric Chrabascz

Dilip Prasad

Michael E Folsom

Paul Mackenzie Colson

John M Beck

Thomas J Ocken

Kevin M Rankin

Ronald M Struziak

Kevin D Gibbons

Joseph Samo

Patrick McCord

David A Dorman

William R Fiske

Paul E Hamel

Raffi O Mangoyan

Christopher Simpson

Kevin P Walsh

Jerry Logsdon

Thomas James Killen

Sebastian Zuraw

Ali Shakil

Anthony Santiago

Maciej Ostrowski

Luke Martin

Jaroslaw Rubalewski

Georgina Tucsa

Alan F Hunter

Rebecca R Stoner

Nathan Devore

Mark J Kelly

Kevin Gibbons

A system includes an injector having a scheduling valve assembly and a nozzle in fluid communication with the valve assembly. The scheduling valve assembly is configured for regulation of flow from an inlet of the injector to the nozzle. An electromagnetic device is operatively connected to a hydromechanical valve spool of the valve assembly to selectively adjust position of the valve spool in the valve assembly.

Force modification of passive valve spools for control of nozzles

A system includes an injector having a scheduling valve assembly and a nozzle in fluid communication with the valve assembly. The scheduling valve assembly is configured for regulation of flow from an inlet of the injector to the nozzle. The injector includes two fluid circuits between the inlet of the injector and two respective outlets of the nozzle for staged flow output from the nozzle. A first one of the two fluid circuits is a primary circuit, and a second one of the two fluid circuits is a secondary circuit. A solenoid valve is connected in fluid communication with the scheduling valve assembly, wherein the solenoid valve is configured to adjust position of a hydromechanical valve spool of the valve assembly.

Proportional force modification of passive spool for control of secondary nozzle circuits

A fuel injector for a turbine engine includes a fuel scheduling valve configured for regulation of fuel flow from a fuel inlet, in response to fuel pressure received at the fuel inlet. Primary, secondary and auxiliary fuel circuits receive fuel from the scheduling valve, and an electrically-controlled valve is provided in fluid communication with the auxiliary circuit, which electrically-controlled valve is adapted and configured to actively control fuel through the auxiliary circuit in response to a control signal. The auxiliary fuel circuit joins with the secondary fuel circuit for delivery to a fuel nozzle.

Proportional restriction of a secondary circuit of a fuel injector

A fuel injector for a turbine engine includes a fuel scheduling valve configured for regulation of fuel flow from a fuel inlet in response to fuel pressure received at the fuel inlet. Primary and secondary fuel circuits receive fuel from the scheduling valve, and an electrically-controlled valve is provided in fluid communication with the primary circuit, adapted and configured to actively control fuel through the primary circuit in response to a control signal.

Variable restriction of a fuel circuit of a fuel nozzle

A fuel injector for a turbine engine includes a fuel scheduling valve configured for regulation of fuel flow from a fuel inlet, in response to fuel pressure received at the fuel inlet. Primary, secondary and auxiliary fuel circuits receive fuel from the scheduling valve, and an electrically-controlled valve is provided in fluid communication with the auxiliary circuit, which electrically-controlled valve is adapted and configured to actively control fuel through the auxiliary circuit in response to a control signal.

Proportional restriction of fuel nozzle with an auxiliary circuit

A method of manufacturing a last chance screen for an aircraft engine includes forming an array of holes through a metal sheet with a wire electrode using electrical discharge machining. The array of holes comprises a plurality of holes. Each hole of the plurality of holes comprises a first end and a second end and is surrounded by a wall section such that the last chance screen is defined by the plurality of holes and the plurality of wall sections. The first and second end of each hole are widened by either applying a flow of an abrasive flow medium to the array of holes in two directions or using a conical sinker electrode on either side of the metal sheet. Shaping the first and second end of each hole results in an airfoil-shaped cross-section of each wall section.

Airfoil last chance screen utilizing EDM and AFM

A method of forming a degassing system includes the step of forming a bundle of hollow tube membrane members by wrapping hollow tube membrane members to form the bundle at a temperature above 100° F. (38° C.). Another method of forming a degassing system includes the step of the inserting bundle into an outer canister at a temperature above 100° F. (38° C.). A fuel supply system made by these methods is also disclosed.

Membrane bundle for fuel deoxygenation with enhanced durability

Force modification of passive spool for control of secondary nozzle circuits

A flow diverter of a coke catching element is provided. The flow diverter includes a body disposable in a flow field and defining an interior, an upstream end, which is defined relative to the flow field, and a downstream end, which is downstream from the upstream end. At least one of the upstream end and the downstream end is open to the interior and the other of the upstream end and the downstream end is closed. The interior diverges at the one of the upstream end and the downstream end that is open and converges at the other of the upstream end and the downstream end.

Coke catching screen

A system includes a plurality of injectors each having a respective main circuit configured to be connected in fluid communication with one manifold for supplying fuel to each injector in the plurality of injectors. Each injector in the plurality of injectors includes a respective hydromechanical scheduling valve member configured to regulate fuel flow from a respective inlet to a respective nozzle of each injector of the plurality of injectors as a function of pressure input from the manifold to the respective main circuits. A valve block is connected in fluid communication with a respective auxiliary circuit in each injector in the plurality of injectors. The auxiliary circuit is operatively connected to adjust position of the respective scheduling valve member for actuating force modification of the scheduling valve member. The valve block is configured to control all of the injectors in the plurality of injectors as a block.

Banked force modification for fuel nozzles

A fuel supply component with coking mitigation includes a housing having a main fuel inlet and a main fuel outlet. The main fuel inlet and outlet define a main fuel flow path therebetween. The housing includes a de-oxygenated fuel inlet in fluid communication with the main fuel flow path downstream from the main fuel inlet. The de-oxygenated fuel inlet is configured and adapted to supply de-oxygenated fuel to the main fuel flow path to mitigate insoluble fuel elements from diffusing and adhering to a wall of the housing.

Systems and methods for coking mitigation in fuel supply systems

A ventilation fan includes a shaft, a rotor, a motor housing, a bearing housing, and an air bearing. The shaft has a shaft body that extends between a first shaft end and a second shaft end. The shaft body defines a first port and a bore. The rotor is disposed about the shaft. The motor housing is disposed about the shaft and is axially spaced apart from the rotor. The bearing housing is disposed about the shaft. The air bearing is disposed proximate the second shaft end and is disposed between the bearing arm and the second shaft end.

Ventilation fan having a hybrid bearing system

Variable restriction of a secondary circuit of a fuel injector

Variable restriction of fuel nozzle with an auxiliary circuit

Growing community of inventors

South Windsor, CT, United States of America

Murtuza Lokhandwalla