ES8100700A1 - Double turbine turboreactor engine. (Machine-translation by Google Translate, not legally binding) - Google Patents

Double turbine turboreactor engine. (Machine-translation by Google Translate, not legally binding)

Info

Publication number
ES8100700A1
ES8100700A1 ES489102A ES489102A ES8100700A1 ES 8100700 A1 ES8100700 A1 ES 8100700A1 ES 489102 A ES489102 A ES 489102A ES 489102 A ES489102 A ES 489102A ES 8100700 A1 ES8100700 A1 ES 8100700A1
Authority
ES
Spain
Prior art keywords
engine
translation
machine
legally binding
google translate
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired
Application number
ES489102A
Other languages
Spanish (es)
Other versions
ES489102A0 (en
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
VICENTE TRILLA RIERA
Original Assignee
VICENTE TRILLA RIERA
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by VICENTE TRILLA RIERA filed Critical VICENTE TRILLA RIERA
Priority to ES489102A priority Critical patent/ES8100700A1/en
Publication of ES489102A0 publication Critical patent/ES489102A0/en
Publication of ES8100700A1 publication Critical patent/ES8100700A1/en
Expired legal-status Critical Current

Links

Landscapes

  • Turbine Rotor Nozzle Sealing (AREA)

Abstract

Double turbine tuborreactor engine. Characterized to have two concentric turbines located in a concentrated way, one front to another, and possessing a series of intercaled pallet rollers concentrically oriented counterweight from each turbine, all of them provided in a manner that when producing an expansion of gases by the explosion of the fuel in the central part of the both both turbines will turn to the other way, causing a turn of the engine axis and improving the other, with its turn, the conditions of adequate pressure of the fuel for a greater thermodynamic performance. (Machine-translation by Google Translate, not legally binding)
ES489102A 1980-02-29 1980-02-29 Double turbine turboreactor engine. (Machine-translation by Google Translate, not legally binding) Expired ES8100700A1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
ES489102A ES8100700A1 (en) 1980-02-29 1980-02-29 Double turbine turboreactor engine. (Machine-translation by Google Translate, not legally binding)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
ES489102A ES8100700A1 (en) 1980-02-29 1980-02-29 Double turbine turboreactor engine. (Machine-translation by Google Translate, not legally binding)

Publications (2)

Publication Number Publication Date
ES489102A0 ES489102A0 (en) 1980-11-01
ES8100700A1 true ES8100700A1 (en) 1980-11-01

Family

ID=8479930

Family Applications (1)

Application Number Title Priority Date Filing Date
ES489102A Expired ES8100700A1 (en) 1980-02-29 1980-02-29 Double turbine turboreactor engine. (Machine-translation by Google Translate, not legally binding)

Country Status (1)

Country Link
ES (1) ES8100700A1 (en)

Also Published As

Publication number Publication date
ES489102A0 (en) 1980-11-01

Similar Documents

Publication Publication Date Title
CH514069A (en) Combustion chamber, especially for a gas turbine engine
CA1005242A (en) Combustor dome assembly for a gas turbine engine
AU420962B2 (en) Fuel control systems for duel fuel gas turbine engines
JPS5420203A (en) Combustion control equipment of engine
BE755567A (en) FIXED VANE STRUCTURE, FOR GAS TURBINE ENGINE AND ASSOCIATED TEMPERATURE ADJUSTMENT ARRANGEMENT
IT7824303A0 (en) IMPROVEMENTS MADE TO FUEL BURNERS FOR GAS TURBINE ENGINES.
DK138463B (en) Combustion chamber for a gas turbine.
JPS5289717A (en) Fuel injector for gas turbine engine
GB1547770A (en) Gas turbine engine fuel injectocorsvk
SE392748B (en) PUMP WITH VARIABLE DEPLACEMENT FOR A GAS TURBINE FUEL SYSTEM
NL7804765A (en) COMBUSTION ENGINE WITH TWO-STAGE TURBO PRESSURE FILLING.
JPS51127912A (en) Fuel injector for gas turbine engine
JPS5372926A (en) Internal combustion engine run-on protector
JPS52109018A (en) Radial-flow turbine
JPS5332239A (en) Speed regulator of centrifugal type for internal combustion engine
ES271553U (en) Perfected combustión chamber for a diesel engine for the use of combustibles such as ethanol or methanol. (Machine-translation by Google Translate, not legally binding)
JPS5329412A (en) Exhaust gas system equipment
JPS5431820A (en) Variable compression ratio type internal combustion engine
ES433850A1 (en) Improvements in explosion engines, with five times and double expansion. (Machine-translation by Google Translate, not legally binding)
JPS5394303A (en) Preparation of methane-rich gas
JPS53120014A (en) Turbo-supercharging engine
JPS5324917A (en) Fuel injector for diesel engine
JPS51111521A (en) Internal combustion engine with fuel property changer
JPS53143818A (en) Production of cylinder for two cycle engine
JPS5371711A (en) Turbo charger for internal combustion engine