HAIL SCREEN IN THE INLET OF A CONDUIT TO A HEAT EXHANGER OF AN AIRCRAFT ENGINE

Aspects of the disclosure are directed to a screen (122) configured for use in association with a cooler (106) of an aircraft, the screen (122) comprising: a first portion (332) arranged as a grid and located in a line-of-sight of the cooler (106) with respect to a fluid inlet (102), and a second po...

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Bibliographische Detailangaben
Hauptverfasser:	SNYDER, Ryan K, HEIMS, Eric J
Format:	Patent
Sprache:	eng ; fre ; ger
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 JET-PROPULSION PLANTS LIGHTING MECHANICAL ENGINEERING PERFORMING OPERATIONS PHYSICAL OR CHEMICAL PROCESSES OR APPARATUS IN GENERAL SEPARATION TRANSPORTING WEAPONS
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Beschreibung
Zusammenfassung:	Aspects of the disclosure are directed to a screen (122) configured for use in association with a cooler (106) of an aircraft, the screen (122) comprising: a first portion (332) arranged as a grid and located in a line-of-sight of the cooler (106) with respect to a fluid inlet (102), and a second portion (334) located out of the line-of-sight of the cooler (106) with respect to the fluid inlet (102), wherein the second portion (334) is grid-free.