Invention Grant
- Patent Title: System for temperature and actuation control and method of controlling fluid temperatures in an aircraft
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Application No.: US14651583Application Date: 2013-11-26
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Publication No.: US09656762B2Publication Date: 2017-05-23
- Inventor: Deepak Manohar Kamath , Mehdi Milani Baladi , Sergei A. Jerebets , Robert Lawrence Mayer , Scott Chandler Morton , Alejandro Yatzail Perez Valadez
- Applicant: General Electric Company
- Applicant Address: US NY Schenectady
- Assignee: General Electric Company
- Current Assignee: General Electric Company
- Current Assignee Address: US NY Schenectady
- Agent Pamela A. Kachur
- International Application: PCT/US2013/071786 WO 20131126
- International Announcement: WO2014/105328 WO 20140703
- Main IPC: B64D37/30
- IPC: B64D37/30 ; B64D37/34 ; F02C3/22 ; F02C7/22 ; F02C7/224 ; F02C9/40
Abstract:
A system for fluid temperature control and actuation control for an aircraft engine fueled by dual fuels. The system includes a first fuel system having a first fuel tank fluidly coupled to the engine, a second fuel system having a second fuel tank fluidly coupled to the engine, with the second fuel being different from the first fuel and having a different temperature than the first fuel, a fuel distribution unit (FDU) fluidly coupled to the first fuel tank of the first fuel system, and a fuel-to-fuel cooler (FFC) configured to transfer heat between the first fuel in the first fuel system and the second fuel in the second fuel system.
Public/Granted literature
- US20150321767A1 SYSTEM FOR TEMPERATURE AND ACTUATION CONTROL AND METHOD OF CONTROLLING FLUID TEMPERATURES IN AN AIRCRAFT Public/Granted day:2015-11-12
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