Turbo rocket with real carnot cycle

Details Turbo rocket with real carnot cycle Turbo rocket with real carnot cycle

F - Mech Eng,Light,Heat,Weapons

02

K

F02K 3/02 (2006.01) F01D 5/18 (2006.01) F02K 9/52 (2006.01) F02K 9/64 (2006.01) F02K 9/94 (2006.01)

Patent

CA 2526591

Engine embodiments primarily designed for aircraft propulsion and power generation incorporating the Carnot cycle for efficient combustion with typical embodiments including air compressors having one or more stages with isothermal compression and including combustion and expansion chambers having in part isothermal expansion before final adiabatic expansion.

Cette invention concerne des modes de réalisation d'un moteur principalement conçu pour la propulsion et la production d'énergie dans des aéronefs en incorporant le cycle de Carnot pour une combustion efficace au moyen de modes de réalisation typiques contenant des compresseurs d'air présentant un ou plusieurs étages avec compression isotherme et contenant des chambres de combustion et d'expansion soumises partiellement à une expansion isotherme avant l'expansion adiabatique finale.

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