METHOD AND SYSTEM FOR SEALING AN ANNULUS

A method and system for a compartment baffle system (206) are provided. The compartment baffle system (206) includes a first baffle portion (302) extending along an axial length of a casing (32), the first baffle portion (302) extending radially outwardly from an outer surface (304) of the casing (3...

Ausführliche Beschreibung

Gespeichert in:

Bibliographische Detailangaben
Hauptverfasser:	GROSE, KYLE ANDREW, HEGEMAN, ARJAN JOHANNES, KEMP, ANDREW DAVID, PYLES, JOHN MICHAEL
Format:	Patent
Sprache:	eng ; fre
Schlagworte:	AIR INTAKES FOR JET-PROPULSION PLANTS BLASTING CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TOTRANSPORTATION COMBUSTION ENGINES CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS ENGINE PLANTS IN GENERAL 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 MACHINES OR ENGINES IN GENERAL MECHANICAL ENGINEERING NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES STEAM ENGINES TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINSTCLIMATE CHANGE WEAPONS
Online-Zugang:	Volltext bestellen
Tags:	Tag hinzufügen Keine Tags, Fügen Sie den ersten Tag hinzu!

Beschreibung
Zusammenfassung:	A method and system for a compartment baffle system (206) are provided. The compartment baffle system (206) includes a first baffle portion (302) extending along an axial length of a casing (32), the first baffle portion (302) extending radially outwardly from an outer surface (304) of the casing (32) and a second baffle portion (306) extending at least partially radially outwardly from the first baffle portion (302). The second baffle portion (306) further includes a radially inner edge (308) supported by the first baffle portion (302) and a radially outer edge (310) extending proximate an inner surface (312) of a radially outer cowl (30). The compartment baffle system (206) also includes a gap (314) extending between the radially outer edge (310) and the inner surface (312).