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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Bibliographische Detailangaben
Hauptverfasser:	SHERER TOMAS, SOLNTSEV ALEKSANDR, KHEESH MIKHAEHL
Format:	Patent
Sprache:	eng ; rus
Schlagworte:	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
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Beschreibung
Zusammenfassung:	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.