YAsUMoTo et al., 1964 - Google Patents
Experimental Investigation of Recessed Wall FlameholderYAsUMoTo 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 …
- 238000009114 investigational therapy 0 title description 7
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING ENGINES OR PUMPS
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
- F23R3/00—Continuous combustion chambers using liquid or gaseous fuel
- F23R3/02—Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration
- F23R3/16—Continuous 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
- F23R3/18—Flame stabilising means, e.g. flame holders for after-burners of jet-propulsion plants
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING ENGINES OR PUMPS
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
- F23R3/00—Continuous combustion chambers using liquid or gaseous fuel
- F23R3/28—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING ENGINES OR PUMPS
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23C—COMBUSTION APPARATUS USING FLUENT FUEL
- F23C6/00—Combustion apparatus characterised by the combination of two or more combustion chambers or combustion zones, e.g. for staged combustion
- F23C6/04—Combustion apparatus characterised by the combination of two or more combustion chambers or combustion zones, e.g. for staged combustion in series connection
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING ENGINES OR PUMPS
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23C—COMBUSTION APPARATUS USING FLUENT FUEL
- F23C7/00—Combustion apparatus characterised by arrangements for air supply
- F23C7/02—Disposition of air supply not passing through burner
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING ENGINES OR PUMPS
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23C—COMBUSTION APPARATUS USING FLUENT FUEL
- F23C2900/00—Special 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 |