Sinibaldi et al., 2005 - Google Patents
Investigation of transient plasma ignition for pulse detonation enginesSinibaldi et al., 2005
View PDF- Document ID
- 5842423047382671697
- Author
- Sinibaldi J
- Rodriguez J
- Channel B
- Brophy C
- Wang F
- Cathey C
- Gundersen M
- Publication year
- Publication venue
- 41st AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit
External Links
Snippet
Results show that TPI system is more effective than conventional spark ignition systems. The TPI system shows near 20% improvements to DDT distances and up-to 2.5 reduction factor in DDT times. In addition, at high flow rates, where the flames normally extinguish when …
- 238000005474 detonation 0 title abstract description 57
Classifications
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING ENGINES OR PUMPS
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02K—JET-PROPULSION PLANTS
- F02K9/00—Rocket- engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
- F02K9/42—Rocket- engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using liquid or gaseous propellants
- F02K9/60—Constructional parts; Details
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING ENGINES OR PUMPS
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02K—JET-PROPULSION PLANTS
- F02K7/00—Plants in which the working fluid is used in a jet only, i.e. the plants not having a turbine or other engine driving a compressor or a ducted fan; Control thereof
- F02K7/02—Plants in which the working fluid is used in a jet only, i.e. the plants not having a turbine or other engine driving a compressor or a ducted fan; Control thereof the jet being intermittent, i.e. pulse-jet
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