HEAT EXCHANGER

A primary heat exchanger for use in an environmental control system of an aircraft is provided having a rectangular core. The core includes a plurality of alternately stacked first fluid layers and second fluid layers. The core has a length to width ratio of about 4.88 and a width to height ratio of...

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Bibliographische Detailangaben
1. Verfasser:	VAN LIEU PIETER
Format:	Patent
Sprache:	eng
Schlagworte:	BLASTING DETAILS OF HEAT-EXCHANGE AND HEAT-TRANSFER APPARATUS, OFGENERAL APPLICATION HEAT EXCHANGE IN GENERAL HEAT-EXCHANGE APPARATUS, NOT PROVIDED FOR IN ANOTHER SUBCLASS,IN WHICH THE HEAT-EXCHANGE MEDIA DO NOT COME INTO DIRECT CONTACT HEATING LIGHTING MECHANICAL ENGINEERING WEAPONS
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Beschreibung
Zusammenfassung:	A primary heat exchanger for use in an environmental control system of an aircraft is provided having a rectangular core. The core includes a plurality of alternately stacked first fluid layers and second fluid layers. The core has a length to width ratio of about 4.88 and a width to height ratio of about 2.37. A first header is positioned adjacent a first surface of the core and a second header is positioned adjacent a second opposite surface of the core. The first header and the second header form a portion of a flow path for a first fluid. An inlet flange is positioned adjacent a third surface of the core. An outlet flange is positioned adjacent a fourth, opposite surface of the core to form a portion of a flow path for a second fluid.