[go: up one dir, main page]

Bellini et al., 2010 - Google Patents

Exergy analysis of a hybrid pulse detonation power device

Bellini et al., 2010

View PDF
Document ID
1481535644678418858
Author
Bellini R
Lu F
Publication year
Publication venue
Journal of Propulsion and Power

External Links

Snippet

TRADITIONAL gas cycles, such as the Otto, Diesel, and Brayton cycles [1], are based on the deflagrative mode of combustion for adding energy to the working fluid. A paradigm shift from deflagration-based cycles can be achieved by using detonations to develop thrust or …
Continue reading at www.academia.edu (PDF) (other versions)

Classifications

    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/60—Efficient propulsion technologies
    • Y02T50/67—Relevant aircraft propulsion technologies
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T10/00—Road transport of goods or passengers
    • Y02T10/10—Internal combustion engine [ICE] based vehicles
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING ENGINES OR PUMPS
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C3/00—Gas-turbine plants characterised by the use of combustion products as the working fluid
    • 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
    • F02K7/10—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 characterised by having ram-action compression, i.e. aero-thermo-dynamic-ducts or ram-jet engines
    • F02K7/16—Composite ram-jet/turbo-jet engines
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING ENGINES OR PUMPS
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C6/00—Plural gas-turbine plants; Combinations of gas-turbine plants with other apparatus; Adaptations of gas- turbine plants for special use
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING ENGINES OR PUMPS
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING ENGINES OR PUMPS
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01C—ROTARY-PISTON OR OSCILLATING-PISTON MACHINES OR ENGINES
    • F01C11/00—Combinations of two or more machines or engines, each being of rotary-piston or oscillating-piston type
    • F01C11/002—Combinations of two or more machines or engines, each being of rotary-piston or oscillating-piston type of similar working principle

Similar Documents

Publication Publication Date Title
Akbari et al. A review of wave rotor technology and its applications
Smart How much compression should a scramjet inlet do?
US11773777B2 (en) Zero-emission jet engine employing a dual-fuel mix of ammonia and hydrogen using a wave
US7367194B2 (en) Pulse detonation engine system for driving turbine
Bobusch et al. Shockless explosion combustion: An innovative way of efficient constant volume combustion in gas turbines
Akbari et al. Performance enhancement of microturbine engines topped with wave rotors
Kent field Thermodynamics of airbreathing pulse-detonation engines
US5058826A (en) Scramjet engine having a low pressure combustion cycle
Bellini et al. Exergy analysis of a hybrid pulse detonation power device
Kent field Fundamentals of idealized airbreathing pulse-detonation engines
Xisto et al. Analytical model for the performance estimation of pre-cooled pulse detonation turbofan engines
Goldmeer et al. System-level performance estimation of a pulse detonation based hybrid engine
Naitoh et al. Fugine cycle theory: predicting high efficiency of the supermultijet-convergence engine working from startup to hypersonic scram mode
Akbari et al. Numerical simulation and design of a combustion wave rotor for deflagrative and detonative propagation
Şöhret A comprehensive approach to understanding irreversibility in a turbojet
Chen et al. Effects of excess oxidizer coefficient on RBCC engine performance in ejector mode: A theoretical investigation
Rähse et al. Gas dynamic simulation of shockless explosion combustion for gas turbine power cycles
Dean Recent developments in approaches to pulsed detonation propulsion
Akbari et al. Investigation of Ammonia-Hydrogen Mixture as a Green Fuel for Jet Engines Using a Wave Reformer
Rose et al. Potential applications of wave machinery to energy and chemical processes
Dean A review of PDE development for propulsion applications
Akbari et al. The use of wave machinery for power generation and production of hydrogen as gas turbine fuel
Bonanos et al. Dual-mode combustion experiments with an integrated aeroramp-injector/plasma-torch igniter
Nalim et al. Internal combustion wave rotors for gas turbine engine enhancement
Akbari et al. Analysis of flow processes in detonative wave rotors and pulse detonation engines