Patents by Inventor Dominique P. Sautron
Dominique P. Sautron has filed for patents to protect the following inventions. This listing includes patent applications that are pending as well as patents that have already been granted by the United States Patent and Trademark Office (USPTO).
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Patent number: 11959499Abstract: An Environmental Control System (ECS) for an aircraft includes a ram air system having a ram inlet and a ram outlet. The ECS includes a cabin air compressor motor, a diverter valve, and a dedicated outlet. The cabin air compressor motor has a motor inlet passage and a motor outlet passage with the motor inlet passage being coupled to the ram inlet. The diverter valve includes a first diverter inlet, a first diverter outlet, and a second diverter outlet. The first diverter inlet is coupled to the motor outlet passage. The dedicated outlet is connected to the first diverter outlet in a flight mode of operation of the aircraft and the ram outlet is connected to the second diverter outlet in a ground mode of operation of the aircraft.Type: GrantFiled: October 5, 2021Date of Patent: April 16, 2024Assignee: HAMILTON SUNDSTRAND CORPORATIONInventors: Donald E. Army, Patrick McCord, Dominique P. Sautron, Thomas M. Zywiak
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Patent number: 11391299Abstract: An Environmental Control System (ECS) for an aircraft includes a ram air system having a ram inlet and a ram outlet. The ECS includes a cabin air compressor motor, a diverter valve, and a dedicated outlet. The cabin air compressor motor has a motor inlet passage and a motor outlet passage with the motor inlet passage being coupled to the ram inlet. The diverter valve includes a first diverter inlet, a first diverter outlet, and a second diverter outlet. The first diverter inlet is coupled to the motor outlet passage. The dedicated outlet is connected to the first diverter outlet in a flight mode of operation of the aircraft and the ram outlet is connected to the second diverter outlet in a ground mode of operation of the aircraft.Type: GrantFiled: October 11, 2018Date of Patent: July 19, 2022Assignee: HAMILTON SUNDSTRAND CORPORATIONInventors: Donald E. Army, Patrick McCord, Dominique P. Sautron, Thomas M. Zywiak
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Publication number: 20220025907Abstract: An Environmental Control System (ECS) for an aircraft includes a ram air system having a ram inlet and a ram outlet. The ECS includes a cabin air compressor motor, a diverter valve, and a dedicated outlet. The cabin air compressor motor has a motor inlet passage and a motor outlet passage with the motor inlet passage being coupled to the ram inlet. The diverter valve includes a first diverter inlet, a first diverter outlet, and a second diverter outlet. The first diverter inlet is coupled to the motor outlet passage. The dedicated outlet is connected to the first diverter outlet in a flight mode of operation of the aircraft and the ram outlet is connected to the second diverter outlet in a ground mode of operation of the aircraft.Type: ApplicationFiled: October 5, 2021Publication date: January 27, 2022Inventors: Donald E. Army, Patrick McCord, Dominique P. Sautron, Thomas M. Zywiak
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Patent number: 11156233Abstract: An Environmental Control System (ECS) for an aircraft includes a ram air system having a ram inlet and a ram outlet. The ECS includes a cabin air compressor motor, a diverter valve, and a dedicated outlet. The cabin air compressor motor has a motor inlet passage and a motor outlet passage with the motor inlet passage being coupled to the ram inlet. The diverter valve includes a first diverter inlet, a first diverter outlet, and a second diverter outlet. The first diverter inlet is coupled to the motor outlet passage. The dedicated outlet is connected to the first diverter outlet in a flight mode of operation of the aircraft and the ram outlet is connected to the second diverter outlet in a ground mode of operation of the aircraft.Type: GrantFiled: October 11, 2018Date of Patent: October 26, 2021Assignee: HAMILTON SUNDSTRAND CORPORATIONInventors: Donald E. Army, Patrick McCord, Dominique P. Sautron, Thomas M. Zywiak
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Publication number: 20190040877Abstract: An Environmental Control System (ECS) for an aircraft includes a ram air system having a ram inlet and a ram outlet. The ECS includes a cabin air compressor motor, a diverter valve, and a dedicated outlet. The cabin air compressor motor has a motor inlet passage and a motor outlet passage with the motor inlet passage being coupled to the ram inlet. The diverter valve includes a first diverter inlet, a first diverter outlet, and a second diverter outlet. The first diverter inlet is coupled to the motor outlet passage. The dedicated outlet is connected to the first diverter outlet in a flight mode of operation of the aircraft and the ram outlet is connected to the second diverter outlet in a ground mode of operation of the aircraft.Type: ApplicationFiled: October 11, 2018Publication date: February 7, 2019Inventors: Donald E. Army, Patrick McCord, Dominique P. Sautron, Thomas M. Zywiak
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Publication number: 20190040876Abstract: An Environmental Control System (ECS) for an aircraft includes a ram air system having a ram inlet and a ram outlet. The ECS includes a cabin air compressor motor, a diverter valve, and a dedicated outlet. The cabin air compressor motor has a motor inlet passage and a motor outlet passage with the motor inlet passage being coupled to the ram inlet. The diverter valve includes a first diverter inlet, a first diverter outlet, and a second diverter outlet. The first diverter inlet is coupled to the motor outlet passage. The dedicated outlet is connected to the first diverter outlet in a flight mode of operation of the aircraft and the ram outlet is connected to the second diverter outlet in a ground mode of operation of the aircraft.Type: ApplicationFiled: October 11, 2018Publication date: February 7, 2019Inventors: Donald E. Army, Patrick McCord, Dominique P. Sautron, Thomas M. Zywiak
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Patent number: 10184494Abstract: An Environmental Control System (ECS) for an aircraft includes a ram air system having a ram inlet and a ram outlet. The ECS includes a cabin air compressor motor, a diverter valve, and a dedicated outlet. The cabin air compressor motor has a motor inlet passage and a motor outlet passage with the motor inlet passage being coupled to the ram inlet. The diverter valve includes a first diverter inlet, a first diverter outlet, and a second diverter outlet. The first diverter inlet is coupled to the motor outlet passage. The dedicated outlet is connected to the first diverter outlet in a flight mode of operation of the aircraft and the ram outlet is connected to the second diverter outlet in a ground mode of operation of the aircraft.Type: GrantFiled: June 28, 2013Date of Patent: January 22, 2019Assignee: HAMILTON SUNDSTRAND CORPORATIONInventors: Donald E. Army, Patrick McCord, Dominique P. Sautron, Thomas M. Zywiak
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Publication number: 20150004011Abstract: An Environmental Control System (ECS) for an aircraft includes a ram air system having a ram inlet and a ram outlet. The ECS includes a cabin air compressor motor, a diverter valve, and a dedicated outlet. The cabin air compressor motor has a motor inlet passage and a motor outlet passage with the motor inlet passage being coupled to the ram inlet. The diverter valve includes a first diverter inlet, a first diverter outlet, and a second diverter outlet. The first diverter inlet is coupled to the motor outlet passage. The dedicated outlet is connected to the first diverter outlet in a flight mode of operation of the aircraft and the ram outlet is connected to the second diverter outlet in a ground mode of operation of the aircraft.Type: ApplicationFiled: June 28, 2013Publication date: January 1, 2015Inventors: Donald E. Army, Patrick McCord, Dominique P. Sautron, Thomas M. Zywiak
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Publication number: 20130345928Abstract: Disclosed is an aircraft environmental control system having interfaces to a first onboard power generation system, interfaces to a second onboard power generation system, and a controller. The controller is operable to distribute power from the first power generation system and the second power generation system to a plurality of aircraft environmental systems, and the controller is operable to switch a subset of the plurality of environmental systems from the first onboard power generation system to the second onboard power generation system.Type: ApplicationFiled: June 21, 2012Publication date: December 26, 2013Inventors: Dominique P. Sautron, Carol M. SaNogueira, Evelyn V. Kobialka