Accession Number : ADD009206

Title :   An Augmented Combustion Chamber Using Vorbix Principle with Core Stream Swirl.

Descriptive Note : Patent Application,


Personal Author(s) : Reilly,Richard S ; Hanloser,Kurt J

Report Date : 23 Oct 1981

Pagination or Media Count : 8

Abstract : The present invention relates to vortex burning and mixing (VORBIX) augmentors for aircraft engines, and more particularly to a VORBIX augmentor using core stream swirl. Accordingly, the present invention provides a VORBIX augmentor with core stream swirl. Means for swirling the core stream are situated upstream from the augmentor area to promote mixing of core and pilot flows. Such swirling means is provided by a redesigned turbine exit guide vane which produces an approximately 20 deg off axial swirl flow entering the augmentor area.

Descriptors :   *Patent applications, *Aircraft engines, *Engine fuel systems components, *Guide vanes, Swirler vanes, Augmentation, Vortices, Turbine parts, Combustion, Mixing, Fuels, Jet engine fuels, Inventions

Subject Categories : Jet and Gas Turbine Engines

Distribution Statement : APPROVED FOR PUBLIC RELEASE