United Technologies Corporation

B/e Aerospace, Inc.

Hamilton Sundstrand Corporation

Brian M Welch

John P Wesson

Thomas Gregory Tillman

Charles C Coffin

Haralambos Cordatos

Brian St Rock

Jonathan Rheaume

Matthew Robert Pearson

Joseph J Sangiovanni

Louis J Spadaccini

Foster Philip Lamm

Catherine Thibaud

Zidu Ma

He Huang

Michael Paul Humbert

Catalin G Fotache

Alexander Chen

Michael A Fortin

Lou Chiappetta

James A Wilkinson

Mathieu Le Cam

Michael Fortin

Alexander G Chen

A personal aircraft seat air treatment system may include an air blower, a ventilation output component installed within a passenger compartment, and a treatment component fluidically coupled to the air blower and the ventilation output component. The air blower may be configured to receive cabin air from a cabin air ventilation system installed in an aircraft cabin. The ventilation output component may be configured to provide treated air to a breathing area of a passenger proximate to an aircraft seat installed in the passenger compartment. The treatment component may be fluidically coupled to the air blower and the ventilation output component. The treatment component may be configured to receive the cabin air from the air blower and treat the cabin air to generate the treated air.

Personal aircraft seat air treatment system

A fuel system for an energy conversion device includes a multiple of non-metallic fuel plates, gaskets, oxygen permeable membranes, porous substrate plates, and vacuum frame plates. Intricate 3-dimension fuel channel structures such as laminar flow impingement elements within the fuel channel dramatically enhance oxygen diffusivity in the FSU. The fuel plates are manufactured from a relatively soft non-metallic material. The non-metallic fuel plates and gasket arrangement provide an effective sealing interface between the fuel plate and oxygen permeable membrane, since compression may be applied to the plates without damaging the relatively delicate oxygen permeable membrane.

Fuel deoxygenation system with non-metallic fuel plate assembly

A fuel stabilization system includes a first deoxygenator and a second deoxygenator both for removing dissolved oxygen from a hydrocarbon fuel. The first and second deoxygenators are arranged in parallel or series to sequentially remove a portion of dissolved oxygen from the hydrocarbon fuel. The arrangement of several deoxygenators for a single fuel stream improves removal of dissolved oxygen and provides for scalability of the fuel system to meet application specific demands. The arrangement also provides for the preservation of partial system functionality in the event of the failure of one of the deoxygenator modules.

Modular fuel stabilization system

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West Hartford, CT, United States of America

Brian M Welch