EDWARD TODD HAGAMAN
Pilots at Marbella Ln, Tolland, CT

License number
Connecticut A2240596
Issued Date
Oct 2016
Expiration Date
Oct 2018
Category
Airmen
Type
Authorized Aircraft Instructor
Address
Address
96 Marbella Ln, Tolland, CT 06084

Professional information

Edward Hagaman Photo 1

Hybrid Engine Accessory Power System

US Patent:
2009027, Oct 29, 2009
Filed:
Mar 30, 2009
Appl. No.:
12/413617
Inventors:
Timothy M. Morris - San Diego CA, US
Wayne R. Spock - Canton CT, US
Peter Gerard Smith - Wallingford CT, US
Matthew J. Schryver - Wethersfield CT, US
Ronald S. Walther - Granby CT, US
Robert L. Gukeisen - Middletown CT, US
Edward T. Hagaman - Tolland CT, US
Assignee:
United Technologies Corporation - Hartford CT
International Classification:
G06F 19/00
US Classification:
701100
Abstract:
A system for generating accessory power from a gas turbine engine is provided by the present invention. The system includes an electronic control device for monitoring at least one parameter which provides information about an incipient change in power demand, a control valve operated by the control device for supplying bleed air from the engine during a transient state in response to the at least one monitored parameter, and a pneumatically operated device for receiving the bleed air and for generating power to operate equipment onboard an aircraft. The pneumatically operated device may be an air turbine or a pneumatically integrated generator.


Edward Hagaman Photo 2

Hybrid Engine Accessory Power System

US Patent:
2005010, May 19, 2005
Filed:
Oct 27, 2003
Appl. No.:
10/694645
Inventors:
Timothy Morris - San Diego CA, US
Wayne Spock - Canton CT, US
Peter Smith - Wallingford CT, US
Matthew Schryver - Wethersfield CT, US
Ronald Walther - Granby CT, US
Robert Gukeisen - Middletown CT, US
Edward Hagaman - Tolland CT, US
International Classification:
B64D041/00
US Classification:
244058000
Abstract:
A system for generating accessory power from a gas turbine engine is provided by the present invention. The system includes an electronic control device for monitoring at least one parameter which provides information about an incipient change in power demand, a control valve operated by the control device for supplying bleed air from the engine during a transient state in response to the at least one monitored parameter, and a pneumatically operated device for receiving the bleed air and for generating power to operate equipment onboard an aircraft. The pneumatically operated device may be an air turbine or a pneumatically integrated generator.