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BREVET 2.319.019 (A1) (76 21811). - 16 JUILLET 1976. PERFECTIONNEMENTS AUX TURBOREACTEURS A SOUFFLANTE.sdPatent

LA BATAILLE DES REACTEURS A DOUBLE FLUX DE 15 TONNES DE POUSSEEWOOD D; MAURICE P.1981; INTERAVIA; ISSN 0376-9402; CHE; DA. 1981; VOL. 36; NO 6; PP. 561-563Article

LE JT9D DE PRATT & WHITNEY APRES SA CURE DE RAJEUNISSEMENTREK B.1982; INTERAVIA; ISSN 0376-9402; CHE; DA. 1982; VOL. 37; NO 2; PP. 178-180Article

IMPROVED COMPONENTS FOR ENGINE FUEL SAVINGSANTL RJ; MCAULEY JE.1980; SAE TRANS.; ISSN 0096-736X; USA; DA. 1980; VOL. 89; NO 3; PP. 3382-3396; BIBL. 11 REF.Article

BUSINESS AIRCRAFT TURBOFAN TECHNOLOGY PROGRESS IN THE 1970'S, CHALLENGES IN THE 1980'SWALLACE FB.1980; SAE TRANS.; ISSN 0096-736X; USA; DA. 1980; NO 2; PP. 2114-2123; BIBL. 6 REF.Article

SULL' APPLICAZIONE DEL METODO DEI RESIDUI PER LA PREVISIONE DELLE CARATTERISTICHE OPERATIVE TURBOFAN FUNZIOANTI IN CONDIZIONI DI FUORI-PROGETTO. = UTILISATION DE LA METHODE DES VARIABLES PERTURBEES POUR L'EVALUATION DES PERFORMANCES D'UN TURBOREACTEUR DOUBLE FLUX EN COURS DE VOLAMBROSIO B; FEOLA M.1976; TERMOTECNICA; ITAL.; DA. 1976; VOL. 30; NO 12; PP. 642-650; ABS. ANGL.; BIBL. 14 REF.Article

DESIGN AND PERFORMANCE OF THE PROPULSION SYSTEM FOR THE QUIET SHORT-HAUL RESEARCH AIRCRAFTSHOVLIN MD; SKAVDAHL H; HARKONEN DL et al.1980; J. AIRCR.; ISSN 0021-8669; USA; DA. 1980; VOL. 17; NO 12; PP. 843-850; BIBL. 6 REF.Article

TECHNOLOGY OF THE ROLLS-ROYCE RB211 ENGINECOPLIN JF.1979; AIRCR. ENGNG; GBR; DA. 1979; VOL. 51; NO 12; PP. 8-11Article

SCHWEIZERISCHE STRAHLFLUGZEUGE UND STRAHLTRIEBWERKE. TEIL 6/7. = AVIONS A REACTION ET PROPULSEURS A REACTION DE CONSTRUCTION SUISSE. VI ET VIIBRIDEL G.1977; SCHWEIZ. BAUZTG; SCHWEIZ; DA. 1977; VOL. 95; NO 32; PP. 541-545; BIBL. 12 REF.Article

DEVELOPMENT OF A NEW CLASS OF ENGINE. THE SMALL TURBOFAN.WILLS TK; WISE EP.1976; IN: PROPUL. CONF. 12; PALO ALTO, CALIF.; 1976; NEW YORK; AM. AERONAUT. ASTRONAUT.; DA. 1976; VOL. 618; PP. 1-16; BIBL. 2 REF.Conference Paper

BREVET 2.337.258 (A1) (76 19695). - 29 JUIN 1976. EQUIPEMENT INVERSEUR DE POUSSEE POUR MOTEURS A DOUBLE FLUX.sdPatent

MAINTENANCE DES GROS MOTEURS D'AVIONS DE LIGNE. L'EXEMPLE DU GENERAL ELECTRIC CF6-80A DE L'A310SEIDL D.1983; INTERAVIA; ISSN 0376-9402; CHE; DA. 1983; NO 4; PP. 305-308Article

SMALL FAN-JET ENGINESSPEER IE.1978; SOC. EXPER. TEST PILOTS, TECH. REV.; USA; DA. 1978 PUBL. 1979; PP. 43-51Article

BREVET 2.300.899 (A1) (76 04076). - 13 FEVRIER 1976. PRISE D'AIR D'APPOINT REGLABLE POUR CANAL D'EJECTION DE TURBOREACTEUR.sdPatent

BREVET 2.327.411 (A1) (76 30514). - 11 OCTOBRE 1976. PERFECTIONNEMENTS AUX INVERSEURS DE POUSSEE POUR TURBOREACTEURS A SOUFFLANTE CANALISEE.sdPatent

BREVET 2.347.539 (A1) (77 10090). - 4 AVRIL 1977. REVETEMENT ACOUSTIQUE POUR CONDUIT DE SOUFFLANTE CANALISEE DE TURBOREACTEUR.sdPatent

ROLLS-ROYCE RB 211-535 POWER PLANTPICKERELL DJ.1983; J. AIRCR.; ISSN 0021-8669; USA; DA. 1983; VOL. 20; NO 1; PP. 15-20Article

INFRARED EMISSIONS FROM TURBOFANS WITH HIGH ASPECT RATIO NOZZLESDECHER R.1981; J. AIRCR.; ISSN 0021-8669; USA; DA. 1981; VOL. 18; NO 12; PP. 1025-1031; BIBL. 12 REF.Article

THERMAL EXPANSION ACCOMODATION IN A JET ENGINE FRAMESCHNEIDER MH.1981; J. ENG. POWER; ISSN 0022-0825; USA; DA. 1981; VOL. 103; NO 4; PP. 776-780Article

REVERSE THRUST PERFORMANCE OF THE QCSEE VARIABLE PITCH TURBOFAN ENGINE (QUIET, CLEAN, SHORT-HANL EXPERIMENTAL ENGINE)SAMANICH NE; REEMSNYDER DC; BLOOMER HE et al.1980; SAE TRANS.; ISSN 0096-736X; USA; DA. 1980; VOL. 89; NO 4; PP. 3623-3650; BIBL. 15 REF.Article

INLET AND DUCT FOR THE QSRA BOUNDARY-LAYER CONTROL SYSTEMGUNNARSON DW; MCARDLE JC.1979; J. AIRCR.; USA; DA. 1979; VOL. 16; NO 5; PP. 303-308; BIBL. 4 REF.Article

BREVET 2.349.740 (A1) (77 12605). - 26 AVRIL 1977. BERCEAU DE TURBOREACTEUR A DOUBLE FLUX A PORTES DE CONTOURNEMENT DE STATORS.sdPatent

COMPACT DIFFUSERS FOR CENTRIFUGAL COMPRESSORSBLAIR LW; RUSSO CJ.1982; J. AIR AIRCR.; ISSN 0021-8669; USA; DA. 1982; VOL. 19; NO 1; PP. 46-51; BIBL. 3 REF.Article

REVERSE THRUST PERFORMANCE OF A VARIABLE-PITCH FAN ENGINE AT FORWARD VELOCITYREEMSNYDER DC; SAGERSER DA.1979; J. AIRCR.; USA; DA. 1979; VOL. 16; NO 12; PP. 848-855; BIBL. 9 REF.Article

GE LM500 GAS TURBINE1978; SHIPBUILDG MAR. ENGNG INTERNATION.; GBR; DA. 1978; VOL. 101; NO 1222; PP. 467-469; (2 P.)Article

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