AIR DUCT TO FEED OUTSIDE AIR INTO AIRCRAFT

FIELD: aircraft engineering. ^ SUBSTANCE: air duct (10) has first air inlet (12) and main air channel (16) running from said fist air inlet along airflow. Air duct (10) incorporates second air inlet (24) independent of said first air inlet (12). Proposed method consists in using above described air...

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Hauptverfasser: SHERER TOMAS, SOLNTSEV ALEKSANDR, KHEESH MIKHAEHL
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SOLNTSEV ALEKSANDR
KHEESH MIKHAEHL
description FIELD: aircraft engineering. ^ SUBSTANCE: air duct (10) has first air inlet (12) and main air channel (16) running from said fist air inlet along airflow. Air duct (10) incorporates second air inlet (24) independent of said first air inlet (12). Proposed method consists in using above described air duct. ^ EFFECT: higher safety, simplified design. ^ 7 cl, 3 dwg Изобретение относится к оборудованию воздушного судна. Воздуховод (10) для подачи наружного воздуха в воздушное судно снабжен первым воздушным впускным отверстием (12) и основным воздушным каналом (16), проходящим по ходу потока от первого воздушного впускного отверстия (12). Воздуховод (10) снабжен вторым воздушным впускным отверстием (24), которое выполнено независимым от первого воздушного впускного отверстия (12). Способ характеризуется использованием воздуховода. Изобретения направлены на повышение надежности снабжения бортовых систем воздушного судна наружным воздухом при упрощении конструкции. 2 н. и 5 з.п. ф-лы, 3 ил.
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Air duct (10) incorporates second air inlet (24) independent of said first air inlet (12). Proposed method consists in using above described air duct. ^ EFFECT: higher safety, simplified design. ^ 7 cl, 3 dwg Изобретение относится к оборудованию воздушного судна. Воздуховод (10) для подачи наружного воздуха в воздушное судно снабжен первым воздушным впускным отверстием (12) и основным воздушным каналом (16), проходящим по ходу потока от первого воздушного впускного отверстия (12). Воздуховод (10) снабжен вторым воздушным впускным отверстием (24), которое выполнено независимым от первого воздушного впускного отверстия (12). Способ характеризуется использованием воздуховода. Изобретения направлены на повышение надежности снабжения бортовых систем воздушного судна наружным воздухом при упрощении конструкции. 2 н. и 5 з.п. ф-лы, 3 ил.</abstract><oa>free_for_read</oa></addata></record>
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subjects AIR INTAKES FOR JET-PROPULSION PLANTS
AIRCRAFT
ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT
AVIATION
BLASTING
CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TOTRANSPORTATION
COMBUSTION ENGINES
CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
COSMONAUTICS
EQUIPMENT FOR FITTING IN OR TO AIRCRAFT
FLYING SUITS
GAS-TURBINE PLANTS
GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC
GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS
HEATING
HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
LIGHTING
MECHANICAL ENGINEERING
PARACHUTES
PERFORMING OPERATIONS
TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
TECHNICAL SUBJECTS COVERED BY FORMER USPC
TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINSTCLIMATE CHANGE
TRANSPORTING
WEAPONS
title AIR DUCT TO FEED OUTSIDE AIR INTO AIRCRAFT
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