[go: up one dir, main page]

Cambier, 2002 - Google Patents

Mhd power generation from a pulse detonation rocket engine

Cambier, 2002

Document ID
11169967937863567624
Author
Cambier J
Publication year
Publication venue
33rd Plasmadynamics and Lasers Conference

External Links

Snippet

This paper summarizes a preliminary investigation [1] of the potential for power generation from coupling a Pulse Detonation Rocket Engine (PDRE) with a MHD generator. The PDRE configuration is similar to a rocket engine, except that the operation is pulsed, and the …
Continue reading at arc.aiaa.org (other versions)

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING ENGINES OR PUMPS
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02KJET-PROPULSION PLANTS
    • F02K7/00Plants 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
    • F02K7/02Plants 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
    • F02K7/06Plants 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 with combustion chambers having valves
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING ENGINES OR PUMPS
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02KJET-PROPULSION PLANTS
    • F02K9/00Rocket- engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
    • F02K9/42Rocket- engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using liquid or gaseous propellants
    • F02K9/44Feeding propellants
    • F02K9/46Feeding propellants using pumps
    • F02K9/48Feeding propellants using pumps driven by a gas turbine fed by propellant combustion gases or fed by vaporized propellants or other gases
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING ENGINES OR PUMPS
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02KJET-PROPULSION PLANTS
    • F02K9/00Rocket- engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
    • F02K9/42Rocket- engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using liquid or gaseous propellants
    • F02K9/60Constructional parts; Details

Similar Documents

Publication Publication Date Title
Wu et al. System performance and thermodynamic cycle analysis of airbreathing pulse detonation engines
Bratkovich et al. An introduction to pulse detonation rocket engines (PDREs)
Talei et al. Sound generation by laminar premixed flame annihilation
Kailasanath et al. Performance estimates of pulsed detonation engines
Gray et al. Thermodynamic evaluation of pulse detonation combustion for gas turbine power cycles
Wintenberger Application of steady and unsteady detonation waves to propulsion
Cooper et al. The effect of nozzles and extensions on detonation tube performance
Nielsen Hydrodynamic calculations of surface response in the presence of laser‐supported detonation waves
Cambier Mhd power generation from a pulse detonation rocket engine
Geng et al. Combined numerical and experimental investigation of a hobby-scale pulsejet
Paulson et al. Ideal Thermodynamic performance results for rotating detonation rocket engine thrust chambers using CEA
Ross et al. Flow acceleration in an RDRE with gradual chamber constriction
Alavilli et al. Ignition-transient modeling for solid propellant rocket motors
Zhang et al. Numerical studies of multi-cycle detonation induced by shock focusing
Eidelman et al. Pulsed detonation engine: Key issues
Allgood et al. Effects of exit geometry on the performance of a pulse detonation engine
Bauer et al. Design and test of a resonance ignition system for green in-orbit propulsion systems
Zuniga Investigation of Detonation Theory and the Continuously Rotating Detonation Engine
Kailasanath et al. On factors controlling the performance of pulsed detonation engines
Knowlen et al. Ram accelerator performance modeling
He et al. Reactive flow phenomena in pulse detonation engines
Godil et al. Numerical simulation of ignition transient in solid rocket motor: a revisit
Bellini Ideal cycle analysis of a regenerative pulse detonation engine for power production
Kassoy et al. Thermomechanical Response of Reactive Gas to Rapid Transient, Spatially Distributed Energy Addition: An Asymptotic Formulation
Cambier et al. The pulse detonation rocket induced MHD ejector (PDRIME) concept