Arthur C. Becker Jr.
Engineering in Andover, CT

License number
Louisiana EI.0003378
Issued Date
Jan 1, 1900
Category
Civil Engineer
Address
Address
750 Hop Riv Rd, Andover, CT 06232

Professional information

Arthur Becker Photo 1

Integrated System For Providing Aircraft Environmental Control

US Patent:
6817575, Nov 16, 2004
Filed:
Sep 20, 2002
Appl. No.:
10/251721
Inventors:
Jules Ricardo Munoz - South Windsor CT
Luca Bertuccioli - East Longmeadow MA
Michael K. Sahm - Avon CT
Jay Fletcher - Marlborough CT
Charles E. Lents - Amston CT
Steven E. Squier - Rockford IL
Richard Welch - Rockford IL
Arthur Curtis Becker - Andover CT
Assignee:
Hamilton Sundstrand Corporation - Windsor Locks CT
International Classification:
B64D 1308
US Classification:
2441185, 60 3907, 454 76
Abstract:
The present invention relates to an integrated enviromental control system for an aircraft. The system uses bleed air from a propulsion engine to drive an air turbine which provides power to at least one aircraft component such as an aircraft mounted accessory drive. The system uses the bleed air exiting the air turbine as an air source for the cabin and/or flight deck enviromental control system.


Arthur Becker Photo 2

Integrated Air Turbine Driven System For Providing Aircraft Environmental Control

US Patent:
6796527, Sep 28, 2004
Filed:
Sep 20, 2002
Appl. No.:
10/251720
Inventors:
Jules Ricardo Munoz - Vernon CT
Luca Bertuccioli - Enfield CT
Michael K. Sahm - Avon CT
Jay Fletcher - Marlborough CT
Charles E. Lents - Amston CT
Steve Squier - Rockford IL
Richard Welch - Rockford IL
Arthur Curtis Becker - Andover CT
Assignee:
Hamilton Sundstrand Corporation - Windsor Locks CT
International Classification:
B64D 1100
US Classification:
2441185, 244 58, 454 74, 454 76, 60 39142
Abstract:
The present invention relates to an integrated air turbine driving system for providing aircraft environmental control. The system has at least one air driven turbine for providing power to an aircraft mounted accessory drive and for providing heated air to an aircraft anti-ice system. The system further has a subsystem for supplying cooled pressurized air to a flight deck and/or cabin and to aircraft avionics. Still further, the subsystem provides cooling air to other aircraft components such as a generator and/or an aircraft mounted accessory drive.


Arthur Becker Photo 3

Vapor Compression Cycle Environmental Control System

US Patent:
6663044, Dec 16, 2003
Filed:
Sep 20, 2002
Appl. No.:
10/251719
Inventors:
Jules Ricardo Munoz - Vernon CT
Luca Bertuccioli - Enfield CT
Michael K. Sahm - Avon CT
Jay Fletcher - Marlborough CT
Charles E. Lents - Amston CT
Richard Welch - Rockford IL
Steve Squier - Rockford IL
Arthur Chris Becker - Andover CT
Assignee:
Hamilton Sundstrand Corporation - Windsor Locks CT
International Classification:
B64D 1100
US Classification:
2441185, 62172, 62 93, 62 87, 62402, 60 3907, 60366
Abstract:
The present invention relates to a vapor compression cycle environmental control system for use on aircraft. The system includes an environmental control subsystem which supplies pressurized ram air at a desired temperature to the aircrafts flight deck and/or cabin. The environmental control subsystem uses a vapor compression cycle subsystem to provide the ram air at the desired temperature. The system further includes an air turbine driven by engine bleed air to provide power to an aircraft mounted accessory drive and to provide heated air to an anti-ice system. The aircraft mounted accessory drive provides power to an air compressor which forms part of the environmental control subsystem and to a working fluid compressor which forms part of the vapor compression cycle subsystem.