Inlet system having dual inlets

A method and apparatus for supplying air to a precooler (1417). Air flow is created through a fan duct in an engine system. A first portion of the air flow is directed into a first inlet (1428) of an inlet system (1416) to feed a first half of the precooler (1417). A second portion of the air flow i...

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Bibliographic Details
Main Authors Willie, Robert H, Tretow, Paul R
Format Patent
LanguageEnglish
French
German
Published 29.08.2018
Subjects
AIR INTAKES FOR JET-PROPULSION PLANTS
AIRCRAFT
ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT
AVIATION
BLASTING
COMBUSTION ENGINES
CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
COSMONAUTICS
EQUIPMENT FOR FITTING IN OR TO AIRCRAFT
FLYING SUITS
GAS-TURBINE PLANTS
HEATING
HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
LIGHTING
MECHANICAL ENGINEERING
PARACHUTES
PERFORMING OPERATIONS
TRANSPORTING
WEAPONS
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Summary:A method and apparatus for supplying air to a precooler (1417). Air flow is created through a fan duct in an engine system. A first portion of the air flow is directed into a first inlet (1428) of an inlet system (1416) to feed a first half of the precooler (1417). A second portion of the air flow is directed through the fan duct into a second inlet (1441) of the inlet system to feed a second half of the precooler (1417).
Bibliography:Application Number: EP20140183062