SURFACE COOLER AND METHOD OF FORMING

The invention relates to a surface cooler and a method of forming. Specifically, a surface cooler is configured to be fluidly coupled to an aircraft fan housing and has a first surface configured to face a peripheral wall of the aircraft fan housing and a second surface opposite the first surface, a...

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Bibliographische Detailangaben
1. Verfasser:	LUSCHEK BERNARD ALBERT
Format:	Patent
Sprache:	chi ; eng
Schlagworte:	AIR INTAKES FOR JET-PROPULSION PLANTS BLASTING COMBUSTION ENGINES CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS GAS-TURBINE PLANTS HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS LIGHTING MECHANICAL ENGINEERING WEAPONS
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Beschreibung
Zusammenfassung:	The invention relates to a surface cooler and a method of forming. Specifically, a surface cooler is configured to be fluidly coupled to an aircraft fan housing and has a first surface configured to face a peripheral wall of the aircraft fan housing and a second surface opposite the first surface, a set of fluid channels inside a body, and a set of fins positioned on at least a portion of the second surface of the body. 本发明涉及表面冷却器和形成的方法。具体地，一种表面冷却器构造成用以流体地联接至航空器风扇壳体并且具有构造成用以面对航空器风扇壳体的周壁的第一表面和与第一表面相对的第二表面，在本体的内部的一组流体通道，以及定位在本体的第二表面的至少一部分上的一组翅片。