General Electric Company

Hill-rom Services, Inc.

Cold Jet, Inc.

Other

Ross Michael Leon

Robert Petrosenko

Mayur Yermaneni

Eric Richard Larson

Dennis G O'Keefe

Timothy J Ikeler

Matthew J Sampson

Clifford L Spiro

Thomas Frank Fric

David Perveiler

David R Linger

Malcolm Kenneth MacLean

Mike Rivir

An air pulse generator provides a high frequency chest wall oscillation therapy to a patient wearing an inflatable garment. The air pulse generator includes a blower and a valve coupled to the blower and coupled to the inflatable garment. The valve is movable to apply an oscillating pressure to the inflatable garment. The valve may be a rotary valve or a solenoid valve.

High frequency chest wall oscillation system having valve controlled pulses

A method of assembling a gas turbine engine is provided. The method includes providing at least one heat exchanger assembly including a heat exchanger and a mixer extending downstream from the heat exchanger. The mixer includes a plurality of windows formed therein. The method also includes coupling the at least one heat exchanger assembly within a bypass duct of the engine such that the at least one heat exchanger assembly is coupled to at least one of an outer engine casing and an inner engine casing of the turbine engine.

Methods and apparatus for mixing fluid in turbine engines

A HFCWO system includes an air pulse generator having a blower inlet in communication with a blower and an air port in communication with an inflatable garment. The air pulse generator includes a housing and an air pulse assembly coupled to the housing. The air pulse assembly has at least one diaphragm, at least one driver operable to move the at least one diaphragm and at least one spring arranged to bias the at least one diaphragm away from a portion of the housing.

Efficient high frequency chest wall oscillation system

A blast nozzle formed of a non-conductive material includes electrically conductive paths embedded therein to keep the build up of static electricity below an undesirable level. Stainless steel rods extend the length of the blast nozzle, providing a continuous electrical path.

Non-metallic particle blasting nozzle with static field dissipation

A thrust balanced turn base for changing the direction of a fluid flow containing entrained abrasive media is provided. The turn base includes an elongated member having an inlet for the fluid flow with the entrained abrasive media. The turn base further includes a first internal passageway that extends in a downstream direction from the inlet. The first passageway includes a first throat, a converging portion between the inlet and the throat, a diverging portion extending downstream from the throat, an additional converging portion downstream from the diverging portion, a turning portion downstream from the additional converging portion that converges to a second throat and that leads to a nozzle that conducts the fluid flow containing the entrained abrasive media in an angled direction relative to the long axis of the turn base. The turn base also includes a second internal passageway that is in fluid communication with the first internal passageway at an aperture in the first internal passageway located between the inlet and the first throat. The second internal passageway includes a first portion that extends from the aperture and a second gentlely diverging portion that extends from the first portion and that terminates abruptly in a second nozzle that is oriented at about 90.degree. to the long axis of the turn base. The first portion of the second passageway is configured to divert a portion of substantially abrasive media-free fluid flow from the first internal passageway. The second nozzle is oriented and sized so that the thrust of the entrained abrasive media flow from the first nozzle is substantially counter balanced by the thrust of the abrasive media-free flow from the second nozzle.

Thrust balanced turn base for the nozzle assembly of an abrasive media

Insect debris is removed from or prevented from adhering to insect impingement areas of an aircraft, particularly on an inlet cowl of an engine, by heating the area to 180.degree.-500.degree. C. An apparatus comprising a means to bring hot air from the aircraft engine to a plenum contiguous to the insect impingement area provides for the heating of the insect impingement areas to the required temperatures. The plenum can include at least one tube with a plurality of holes contained in a cavity within the inlet cowl. It can also include an envelope with a plurality of holes on its surface contained in a cavity within the inlet cowl.

Aircraft anti-insect system

An ultralight helicopter has a pair of counter-rotating rotor assemblies which in combination yield zero net angular momentum when rotating at equal speeds. A single motor drives both rotors through a counter-rotating bevel gear set coupled to a pair of concentrically nested output shafts. In an alternative embodiment, the motor is coupled to the rotors through a hydraulic drive system which includes a hydraulic pump and at least one hydraulic motor driving each of the rotor assemblies. The pilot is advantageously suspended in a 'hang-glider' type harness from a single hang point positioned proximate the center of lift of the helicopter. A control bar is fixedly mounted to the frame and is grasped by the pilot suspended in the harness. The pilot maneuvers the helicopter in both the pitch and roll directions by manipulating the control bar. The pilot shifts his own center of gravity relative to the center of gravity of the helicopter while grasping the control bar to thereby maneuver the helicopter.

Ultralight helicopter and control system

A jet engine fan nacelle which maintains attached flow during engine windmilling. The nacelle includes a cylindrical airfoil body having an inner surface. A plurality of vortex generators are positioned on the inner surface between the nacelle body's leading edge and its throat within ninety degrees of rotation from the crown line hilite about the nacelle's longitudinal axis. The vortex generators energize the airflow to maintain an attached flow around the leading edge and along the outer surface of the nacelle's body without separating from the outer surface which would produce an undesirable increase in drag.

Growing community of inventors

Cincinnati, OH, United States of America

Ross Michael Leon