Simon J Pickford, Age 56South Glastonbury, CT
Simon Pickford Phones & Addresses
South Glastonbury, CT
454 Hope Valley Rd, Amston, CT 06231
62 Loveland St, Middletown, CT 06457
Clinton, CT
Hebron, CT
East Hartford, CT
Mentions for Simon J Pickford
Publications & IP owners
Us Patents
Turbomachine Thermal Management
US Patent:
2013025, Oct 3, 2013
Filed:
Apr 2, 2012
Appl. No.:
13/437265
Inventors:
Gabriel L. Suciu - Glastonbury CT, US
Simon Pickford - Amston CT, US
William K. Ackermann - East Hartford CT, US
Nathan Snape - Tolland CT, US
Harold W. Hipsky - Willington CT, US
Simon Pickford - Amston CT, US
William K. Ackermann - East Hartford CT, US
Nathan Snape - Tolland CT, US
Harold W. Hipsky - Willington CT, US
International Classification:
F01D 25/00
F01D 25/08
F01D 25/08
US Classification:
416 1, 416245 R
Abstract:
An example turbomachine assembly includes, among other things, a nose cone of a turbomachine. The nose cone provides an aperture that communicates air to an interior of the nose cone.
Gas Turbine Engine Oil Tank With Integrated Packaging Configuration
US Patent:
2014001, Jan 9, 2014
Filed:
Jul 5, 2012
Appl. No.:
13/541935
Inventors:
Nathan Snape - Tolland CT, US
Gabriel L. Suciu - Glastonbury CT, US
Simon Pickford - Amston CT, US
Gabriel L. Suciu - Glastonbury CT, US
Simon Pickford - Amston CT, US
International Classification:
F01D 25/12
F01D 1/02
F01D 25/18
F01D 1/02
F01D 25/18
US Classification:
415177
Abstract:
A gas turbine engine includes a fan case radially outwardly of a core compartment. A compressor section is located within an engine core compartment and includes a front mount flange and an aft mount flange. An oil tank is mounted to at least one of the fan case or the front and aft mount flanges. The oil tank has a cooling structure integrated into an outer surface such that the oil tank is subjected to cooling air flow from a plurality of air sources.
Turbomachine Thermal Management
US Patent:
2013025, Oct 3, 2013
Filed:
Apr 2, 2012
Appl. No.:
13/437375
Inventors:
Gabriel L. Suciu - Glastonbury CT, US
Simon Pickford - Amston CT, US
William K. Ackermann - East Hartford CT, US
Nathan Snape - Tolland CT, US
Simon Pickford - Amston CT, US
William K. Ackermann - East Hartford CT, US
Nathan Snape - Tolland CT, US
International Classification:
F01D 1/00
US Classification:
415 1, 415117
Abstract:
An example turbomachine assembly includes, among other things, a nose cone of a turbomachine, and a pump that is selectively driven by a motor or a shaft to communicate air to an interior of the nose cone. The pump shaft is driven by a dedicated geared architecture.
Turbomachine Thermal Management
US Patent:
2013025, Oct 3, 2013
Filed:
Apr 2, 2012
Appl. No.:
13/437296
Inventors:
Gabriel L. Suciu - Glastonbury CT, US
Simon Pickford - Amston CT, US
William K. Ackermann - East Hartford CT, US
Nathan Snape - Tolland CT, US
Simon Pickford - Amston CT, US
William K. Ackermann - East Hartford CT, US
Nathan Snape - Tolland CT, US
International Classification:
F01D 1/00
US Classification:
415 1, 415117
Abstract:
An example turbomachine assembly includes, among other things, a nose cone of a turbomachine, and a pump at least partially within an interior of the nose cone. The pump is selectively rotated by a motor to communicate air to the interior.
Geared Architecture Turbofan Engine Thermal Management System And Method
US Patent:
2019021, Jul 18, 2019
Filed:
Mar 22, 2019
Appl. No.:
16/362028
Inventors:
- Farmington CT, US
Simon Pickford - South Glastonbury CT, US
Simon Pickford - South Glastonbury CT, US
Assignee:
United Technologies Corporation - Farmington CT
International Classification:
F01D 25/12
F01D 17/10
F01D 5/02
F01D 15/12
F02K 3/115
F02K 3/06
F02C 7/14
F01D 17/10
F01D 5/02
F01D 15/12
F02K 3/115
F02K 3/06
F02C 7/14
Abstract:
A method of sizing a heat exchanger for a geared architecture gas turbine engine includes sizing a minimum frontal area of at least one heat exchanger located in communication with a fan bypass airflow such that a ratio of waste heat area to horsepower generation characteristic area is between 1.6 to 8.75.
Turbomachine Thermal Management
US Patent:
2018030, Oct 25, 2018
Filed:
Jun 25, 2018
Appl. No.:
16/017110
Inventors:
- Farmington CT, US
Simon Pickford - South Glastonbury CT, US
William K. Ackermann - East Hartford CT, US
Nathan Snape - Tolland CT, US
Simon Pickford - South Glastonbury CT, US
William K. Ackermann - East Hartford CT, US
Nathan Snape - Tolland CT, US
International Classification:
F01D 9/06
F01D 9/02
F01D 5/02
F01D 1/02
F02C 7/047
F02C 7/32
F02C 7/18
F01D 25/12
F02C 7/04
F01D 9/02
F01D 5/02
F01D 1/02
F02C 7/047
F02C 7/32
F02C 7/18
F01D 25/12
F02C 7/04
Abstract:
An example turbomachine assembly includes, among other things, a nose cone of a turbomachine, and a pump at least partially within an interior of the nose cone. The pump is selectively rotated by a motor to communicate air to the interior.
Gas Turbine Engine Oil Tank With Integrated Packaging Configuration
US Patent:
2018019, Jul 12, 2018
Filed:
Mar 7, 2018
Appl. No.:
15/914519
Inventors:
- Farmington CT, US
Gabriel L. Suciu - Glastonbury CT, US
Simon Pickford - Amston CT, US
Gabriel L. Suciu - Glastonbury CT, US
Simon Pickford - Amston CT, US
International Classification:
F01D 25/18
F02C 7/32
F02C 7/14
F02C 7/06
F01D 25/12
B64D 29/08
F02C 7/32
F02C 7/14
F02C 7/06
F01D 25/12
B64D 29/08
Abstract:
A gas turbine engine includes a fan case radially outwardly of a core compartment. A compressor section is located within an engine core compartment and includes a front mount flange and an aft mount flange. An oil tank is mounted to at least one of the fan case or the front and aft mount flanges. The oil tank has a cooling structure integrated into an outer surface such that the oil tank is subjected to cooling air flow from a plurality of air sources.
Diffuser Mounted Fuel-Air Heat Exchanger
US Patent:
2017016, Jun 15, 2017
Filed:
Dec 9, 2015
Appl. No.:
14/963545
Inventors:
- Farmington CT, US
Steven J. Laporte - Coventry CT, US
Stephen K. Kramer - Cromwell CT, US
Simon Pickford - South Glastonbury CT, US
Steven J. Laporte - Coventry CT, US
Stephen K. Kramer - Cromwell CT, US
Simon Pickford - South Glastonbury CT, US
International Classification:
F02C 7/18
Abstract:
A thermal energy exchange system for cooling air of a gas turbine engine includes a heat exchanger located at a diffuser of the gas turbine engine. The diffuser is positioned axially between a compressor and a combustor of the gas turbine engine. A fuel source is operably connected to the heat exchanger to direct a flow of fuel through the heat exchanger via a fuel pipe and toward a fuel nozzle of the combustor. An airflow inlet directs a cooling airflow through the heat exchanger to reduce an airflow temperature via thermal energy exchange between the cooling airflow and the flow of fuel. An airflow outlet directs the cooling airflow from the heat exchanger toward one or more of components of the turbine to cool the one or more components.
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