Title:
HEAT EXCHANGER FOR AIRCRAFT ENGINE
Document Type and Number:
WIPO Patent Application WO/2016/063311
Kind Code:
A1
Abstract:
A heat exchanger is provided which can suppress deformation of heat dissipating fins due to an outside force. This heat exchanger (1) can be arranged along a curved surface of the aircraft engine. The heat exchanger (1) is provided with a main body (10), multiple heat dissipating fins (20), and lid members (50). The main body (10) comprises a back surface (3) which comprises an internal flow path for circulating a fluid and faces the curved surface, and a front surface (2) opposite of the back surface (3). The main body (10) is curved corresponding to the curved surface of the aircraft engine. The multiple heat dissipating fins (20) are arrayed on the front surface (2) of the main body and are exposed to the airflow. The lid members (50) are fixed to the top of the heat dissipating fins (20).
Inventors:
UEDA TATSUYA (JP)
Application Number:
PCT/JP2014/005334
Publication Date:
April 28, 2016
Filing Date:
October 21, 2014
Export Citation:
Assignee:
SUMITOMO PRECISION PROD CO (JP)
International Classes:
F28F1/32; F02C7/18; F28D1/03
Foreign References:
| JP5442916B1 | 2014-03-19 | |||
| JP2006023031A | 2006-01-26 | |||
| JPH1038276A | 1998-02-13 | |||
| JPS58132372U | 1983-09-06 |
Attorney, Agent or Firm:
ASCEND IP LAW FIRM (JP)
アセンド patent business corporation (JP)
アセンド patent business corporation (JP)
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