Title:
HEAT EXCHANGER FOR AIRCRAFT ENGINE
Document Type and Number:
WIPO Patent Application WO/2014/207784
Kind Code:
A1
Abstract:
A heat exchanger for an aircraft engine is provided with a main body constructed of a first member and a second member, each in the form of a plate, superposed and joined in a thickness-wise direction, and defining therein a fluid channel for allowing a fluid to be cooled to flow therethrough, and a corrugated fin plate disposed in the fluid channel. The main body is curved so as to extend along a curved surface on which the heat exchanger is to be mounted, and a plurality of heat radiating fins are erected on the outer surface of the first member and/or the second member.
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Inventors:
UEDA TATSUYA (JP)
Application Number:
PCT/JP2013/004011
Publication Date:
December 31, 2014
Filing Date:
June 26, 2013
Export Citation:
Assignee:
SUMITOMO PRECISION PROD CO (JP)
International Classes:
F02C7/18
Foreign References:
| JPH0544927A | 1993-02-23 | |||
| JP2008144752A | 2008-06-26 | |||
| JP2007127119A | 2007-05-24 | |||
| JPH08505682A | 1996-06-18 | |||
| JPH0749041A | 1995-02-21 | |||
| JPH08338633A | 1996-12-24 | |||
| JPH03267618A | 1991-11-28 | |||
| JP2011089435A | 2011-05-06 | |||
| JP2011163344A | 2011-08-25 | |||
| JPH04116315A | 1992-04-16 | |||
| JP2008144752A | 2008-06-26 |
Other References:
See also references of EP 2843213A4
Attorney, Agent or Firm:
MAEDA & PARTNERS (JP)
Patent business corporation MAEDA PATENT OFFICE (JP)
Patent business corporation MAEDA PATENT OFFICE (JP)
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