YAsUMoTo et al., 1964 - Google Patents

Experimental Investigation of Recessed Wall Flameholder

YAsUMoTo et al., 1964

View PDF
Document ID
414009042072508671
Author
YAsUMoTo T
NEGISHI K
NISHIOKA K
Publication year
Publication venue
Bulletin of JSME

External Links

Snippet

Flameholders are of great importance in the design of ramjet combustors. It was already confirmed by LH Huellmantel et al. that recessed wall flameholders had the advantages of smaller pressure drop and wider range of flame stabilization compared with bluff body …
Continue reading at www.jstage.jst.go.jp (PDF) (other versions)

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING ENGINES OR PUMPS
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23RGENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/02Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration
    • F23R3/16Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration with devices inside the flame tube or the combustion chamber to influence the air or gas flow
    • F23R3/18Flame stabilising means, e.g. flame holders for after-burners of jet-propulsion plants
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING ENGINES OR PUMPS
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23RGENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/28Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING ENGINES OR PUMPS
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23CCOMBUSTION APPARATUS USING FLUENT FUEL
    • F23C6/00Combustion apparatus characterised by the combination of two or more combustion chambers or combustion zones, e.g. for staged combustion
    • F23C6/04Combustion apparatus characterised by the combination of two or more combustion chambers or combustion zones, e.g. for staged combustion in series connection
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING ENGINES OR PUMPS
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23CCOMBUSTION APPARATUS USING FLUENT FUEL
    • F23C7/00Combustion apparatus characterised by arrangements for air supply
    • F23C7/02Disposition of air supply not passing through burner
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING ENGINES OR PUMPS
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23CCOMBUSTION APPARATUS USING FLUENT FUEL
    • F23C2900/00Special features of, or arrangements for combustion apparatus using fluid fuels or solid fuels suspended in air; Combustion processes therefor

Similar Documents

Publication Publication Date Title
Schulte Fuel regression and flame stabilization studies of solid-fuel ramjets
Zhang et al. Investigation of flame establishment and stabilization mechanism in a kerosene fueled supersonic combustor equipped with a thin strut
Roquemore et al. Vortex combustor concept for gas turbine engines
Rasmussen et al. Visualization of flameholding mechanisms in a supersonic combustor using PLIF
RU2358194C1 (en) Solid fuel burner
Ghoniem et al. Stability and emissions control using air injection and H2 addition in premixed combustion
Jin et al. Experimental investigations on flow field and combustion characteristics of a model trapped vortex combustor
Takeno et al. An experimental study on the stability of jet diffusion flame
Zhang et al. Combustion and emissions characteristics of dual-channel double-vortex combustion for gas turbine engines
An et al. Flame stabilization enhancement in a strut-based supersonic combustor by shock wave generators
US3067582A (en) Method and apparatus for burning fuel at shear interface between coaxial streams of fuel and air
Pan et al. Experimental investigation of combustion mechanisms of kerosene-fueled scramjet engines with double-cavity flameholders
Genova et al. Exploration of a Reacting Jet-in-Crossflow in a High-Pressure Axial Stage Combustor
Liu et al. Experimental investigation of single jet and dual jet injection in a supersonic combustor
Chen et al. Experimental study on combustion and flow resistance characteristics of an afterburner with air-cooled bluff-body flameholder
Zhao et al. Experimental study on the effect of injection schemes on fuel spray and combustion characteristics in a compact combustor
Al-Naffakh et al. Burner rim geometry effect on flame stability
YAsUMoTo et al. Experimental Investigation of Recessed Wall Flameholder
Shimokuri et al. Flame propagation in a vortex flow within small-diameter tubes
Zhu et al. Experimental study of combustion efficiency and outlet temperature distribution characteristics of a combined evaporative flameholder
Elbaz et al. Mixing and flame structure study of inverse swirl diffusion flames
Shi et al. Investigation on auto-ignition and chemical energy release characteristics of pilot hydrogen in supersonic combustion flow
Bruno et al. The trapped vortex combustor: an advanced combustion technology for aerospace and gas turbine applications
Gilbert et al. Enhancing flow migration and reducing emissions in full annular ultra compact combustor
Fuhrmann et al. Investigations on multi-stage supersonic combustion in a model combustor