William M Winn

US Patent:

42731836, Jun 16, 1981

Filed:

Jul 31, 1979

Appl. No.:

6/062592

Inventors:

Frank E. Altoz - Catonsville MD
William H. Winn - Linthicum MD

Assignee:

The United States of America as represented by the Secretary of the Air
Force - Washington DC

International Classification:

F28F 2700

US Classification:

165 32

Abstract:

A unidirectional heat transfer device for use between an electronic assembly on an aircraft and the skin and/or pod on the aircraft. The device includes a thermal decoupler mechanism which operates to disengage a retractable interface heat transfer surface when the skin on the aircraft reaches a predetermined elevated temperature caused by the high speed of the aircraft. In the decoupled mode, the heat from the electronic equipment passes to a phase change material heat absorber to provide a limited capability cooling function during extended high speed aircraft operation.

US Patent:

20170275537, Sep 28, 2017

Filed:

Mar 23, 2016

Appl. No.:

15/078754

Inventors:

- Centennial CO, US
Timothy J. Bradley - Centennial CO, US
William H. Winn - Centennial CO, US
David E. Anderson - Billings MT, US
Pritam Mazumder - Centennial CO, US

International Classification:

C10G 53/02

Abstract:

The present inventions are related to oil and gas recovery, and in particular to enhanced oil and gas separation during oil and gas recovery.