TURBOFAN ENGINE COUPLED WITH THRUST REVERSAL UNIT, WITH FAIRING MOUNTED IN GAS FLOW CHANNEL

aircraft engine manufacture. SUBSTANCE: engine has inner structure that forms primary shroud for engine and outer structure that holds thrust reversal unit both not coupled at bottom part of these structures. Inner and outer structures form gas flow discharge channel or annular channel. Airfoil-sect...

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Bibliographische Detailangaben
Hauptverfasser:	RUJER PASKAL' ZHERAR, GONIDEK PATRIK, VOSHEL' GI BERNAR
Format:	Patent
Sprache:	eng
Schlagworte:	AIRCRAFT ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT AVIATION BLASTING CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TOTRANSPORTATION COMBUSTION ENGINES COSMONAUTICS EQUIPMENT FOR FITTING IN OR TO AIRCRAFT FLYING SUITS 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 JET-PROPULSION PLANTS LIGHTING MECHANICAL ENGINEERING PARACHUTES PERFORMING OPERATIONS 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:	aircraft engine manufacture. SUBSTANCE: engine has inner structure that forms primary shroud for engine and outer structure that holds thrust reversal unit both not coupled at bottom part of these structures. Inner and outer structures form gas flow discharge channel or annular channel. Airfoil-section fairing is mounted in annular channel of thrust reversal unit at rear-in-flow side of bracket to form supporting structure for external wall of channel downstream of engine fan. EFFECT: improved aerodynamic flow in nacelle. 9 cl, 10 dwg