Bypass jet engine comprising a thrust reverser

The engine has a thrust reverser (18) e.g. door type thrust reverser, including a deviation unit (20) to divert a part of a gas stream (12) near or downstream of a rear end (11) of a nacelle (10) in a thrust reverse position, such that the diverted gas stream contacting a gas stream (14) reduces spe...

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Bibliographische Detailangaben
Hauptverfasser:	Fert, Jérémy, Emprin, Yves, Wesolowski, Jean-Pierre
Format:	Patent
Sprache:	eng ; fre ; ger
Schlagworte:	BLASTING CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TOTRANSPORTATION COMBUSTION ENGINES 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 TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINSTCLIMATE CHANGE WEAPONS
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Beschreibung
Zusammenfassung:	The engine has a thrust reverser (18) e.g. door type thrust reverser, including a deviation unit (20) to divert a part of a gas stream (12) near or downstream of a rear end (11) of a nacelle (10) in a thrust reverse position, such that the diverted gas stream contacting a gas stream (14) reduces speed of ejection towards a back of the stream (14) and generates a thrust reverse effect in the reverse position. The deviation unit is radially fixed inside a section (45) of an ejector shroud (44) at level of the rear end of the nacelle in the reverse position.