Mark A Gee

US Patent:

6607854, Aug 19, 2003

Filed:

Nov 13, 2000

Appl. No.:

09/712621

Inventors:

Tim Rehg - Rancho Palos Verdes CA
Mark Gee - South Pasadena CA
Terence P. Emerson - Hermosa Beach CA
Joe Ferrall - Simi Valley CA
Pavel Sokolov - Redondo Beach CA

Assignee:

Honeywell International Inc. - Morristown NJ

International Classification:

H01M 804

US Classification:

429 13, 429 17, 429 20, 429 26

Abstract:

A fuel cell system comprises a compressor and a fuel processor downstream of the compressor. A fuel cell stack is in communication with the fuel processor and compressor. A combustor is downstream of the fuel cell stack. First and second turbines are downstream of the fuel processor and in parallel flow communication with one another. A distribution valve is in communication with the first and second turbines. The first and second turbines are mechanically engaged to the compressor. A bypass valve is intermediate the compressor and the second turbine, with the bypass valve enabling a compressed gas from the compressor to bypass the fuel processor.

US Patent:

7565731, Jul 28, 2009

Filed:

Aug 1, 2005

Appl. No.:

11/194288

Inventors:

Carol A. Oximberg - Los Angeles CA, US
Richard W. Fraser - Orange CA, US
Wei-Shing Chaing - Diamond Bar CA, US
Mark Gee - South Pasadena CA, US

Assignee:

Honeywell International Inc. - Morristown NJ

International Classification:

H02K 15/03
H02K 1/27
H02K 1/28

US Classification:

29598, 29607, 31015612, 31015622

Abstract:

A method for manufacturing a rotor assembly. The method includes providing a stub shaft having a first part and a second part, providing a magnet between the first part and the second part, and compressing the magnet between the first part and the second part using a connecting device. The method also includes drilling a hole through the first part and the magnet, cooling an inner shaft, and inserting the inner shaft into the hole.

US Patent:

7988426, Aug 2, 2011

Filed:

Jan 10, 2005

Appl. No.:

11/032418

Inventors:

David G. Elpern - Los Angeles CA, US
Niall McCabe - Torrance CA, US
Mark Gee - South Pasadena CA, US

Assignee:

Honeywell International Inc. - Morristown NJ

International Classification:

F03B 11/06
F01D 25/16

US Classification:

417 53, 417407, 415112, 415229, 416174

Abstract:

A compressor ported shroud takes compressed air from the shroud of the compressor before it is completely compressed and delivers it to foil bearings. The compressed air has a lower pressure and temperature than compressed outlet air. The lower temperature of the air means that less air needs to be bled off from the compressor to cool the foil bearings. This increases the overall system efficiency due to the reduced mass flow requirements of the lower temperature air. By taking the air at a lower pressure, less work is lost compressing the bearing cooling air.

US Patent:

20130266417, Oct 10, 2013

Filed:

Apr 4, 2012

Appl. No.:

13/439663

Inventors:

MARK GEE - SOUTH PASADENA CA, US
MARSHALL SAVILLE - TORRANCE CA, US
KEITH ALAN HURLEY - GARDEN GROVE CA, US

Assignee:

HONEYWELL INTERNATIONAL INC. - MORRISTOWN NJ

International Classification:

F01D 5/08

US Classification:

415 1, 415180

Abstract:

A turbomachine having gas cooled bearings may include an axially-oriented, cooling-gas passageway interconnecting first and second bearing chambers. The passageway may include grooves formed at an interface between an aerodynamic component of the turbomachine (e.g., a wheel or impeller) and a portion of a shaft assembly of the turbomachine.

US Patent:

20150090119, Apr 2, 2015

Filed:

Oct 1, 2013

Appl. No.:

14/042936

Inventors:

- Morristown NJ, US
Dennis M. Morita - Rancho Palos Verdes CA, US
Mark Gee - South Pasadena CA, US

Assignee:

HONEYWELL INTERNATIONAL INC. - Morristown NJ

International Classification:

B64D 13/06
B03C 3/66
B03C 3/38

US Classification:

95 57, 96 15, 96 80, 96 76

Abstract:

An Environmental Control System may use an electronic air treatment system to control humidity in an aircraft. The electronic air treatment system may use an electronic charging system and a separation system. A turbine rotor may drive a power generating stage to provide high voltage power to the electronic charging system. The charging stage may charge airflow passing through to repel liquid particles away from the airflow. Liquid droplets may be collected and centrifugally flung toward a periphery of the separation system. The liquid particles may be collected outside of the airflow, which may be allowed to pass through the separation system and out to a destination in the aircraft without the collected liquid.