Title:
HEAT MANAGEMENT SYSTEM FOR AIRCRAFT
Document Type and Number:
Japanese Patent JP2005207415
Kind Code:
A
Abstract:
To provide an effective lightweight heat management system for minimizing the number of air-to-liquid heat exchangers.
The heat management system using fuel as the base has a fuel stabilizing system for enabling fuel to exceed a conventional coking temperature. A high temperature component is arranged along a fuel flow passage so that the fuel functions as a heat absorbing source, because heat is transmitted from the high temperature component to the fuel even at higher operating temperatures. Optimal high temperature ester base oil reaches high temperatures allowing an oil loop to exceed the present oil temperature limit and heat to be efficiently exhausted to the fuel at the back of the fuel flow passage.
Inventors:
SABATINO DANIEL
SPADACCINI LOUIS J
KASLUSKY SCOTT
SPADACCINI LOUIS J
KASLUSKY SCOTT
Application Number:
JP2004359040A
Publication Date:
August 04, 2005
Filing Date:
December 10, 2004
Export Citation:
Assignee:
UNITED TECHNOLOGIES CORP
International Classes:
F02C7/22; B64D37/00; B64D37/32; B64D37/34; F02C7/06; F02C7/236; (IPC1-7): F02C7/22; F02C7/06; F02C7/236
Attorney, Agent or Firm:
Masatake Shiga
Takashi Watanabe
Yasuhiko Murayama
Shinya Mitsuhiro
Takashi Watanabe
Yasuhiko Murayama
Shinya Mitsuhiro