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5 comparativelysmallratioofgearormayevenbeomitted in certain cases, in connection with gas turbines with a moderate rotational speed. FIG. 7 shows a variant of FIG. 6 with respect to the torus-shapeofthehydrodynamictorqueconverter. Here, the torque converter is also provided with a reaction member S1 with adjustable blades, and possibly with a further reaction member S2. Furthermore, a so-called brake free wheel F isprovided. 6 thesameandtheturbineshaft. Hereby,a?attere?i ciency curve for said turbine ismade possible. Obviously, the invention is not limited to the embodi ments shown but may be varied within the scope of the illustrated principles and the annexed claim. What I claim is: A gasturbinepowerplanthavinganoutputshaftand comprising a single gas turbine member having a power output shaft, a combustion chamber member adapted to 3,138,923 By the adjustable reaction member S1 being located 10 produce motive ?uid for driving said turbine member, a compressor member driven by said power output shaft of said turbine member and delivering combustion air to said combustion chamber member, and a hydrodynamic torqueconverterhavingapump member, aturbinemem between the pump P and the turbine T, an effective engine brake may be obtained here by reversing the direction of rotation of the ?owing medium in front of the turbine, thefreewheelthenpossiblypermittingofbeingomitted. Furthermore, there is a possibility by the embodiment 15 ber and a reaction member arranged in a closed liquid shown to provide a reverse gear in the actual hydro dynamic torque converter, and consequently the mechan ical reverse gear may possibly be omitted in certain cases. ?owcircuit,saidconverterpumpmemberbeingconnected to said gas turbine power output shaft and said converter turbine member being connected to said output ‘shaft of the plant, said reaction member including blading which FIG. 8 shows a further variant with respect to the hy drodynamictorqueconverter,thereactionmemberShav 20 isadjustableintoapositiontoreversethetorqueacting ing been located between the turbine T1 and the pump P (countedinthedirectionofflow). Inthisembodiment, a special reverse gear is required. FIG. 9 shows a further embodiment, wherein the re action member S is placed between spherical and con centricalsurfaces,thecentrelineofthepinsofthepivoted blades then coinciding with the radius of said concentric spheres. Saidarrangementmakesitpossibletoplacethe turbine at the greatest possible radius with the pump lo cated at the smallest possible radius, While an otherwise 30 suitable arrangement of the circuitous path of the hydro dynamic torque converter is obtained. FIGS. 10 and 11 show alternative embodiments as far as the compressor turbine is concerned, the ?rst or the second turbine step being provided with a free wheel F, 35 possibly in combination with a reduction gear between on said converter turbine member. References Cited in the ?le of this patent UNITED STATES PATENTS 1,199,361 2,314,370 2,327,647 2,336,052 2,631,427 2,651,492 2,667,744 2,932,940 495,469‘ Fottinger ______________ Sept. 26, 1916 Ball ________________ __ Mar. 23, 1943 Jandasek ______________ Aug. 24, 1943 Anderson et a1. ________.._ Dec. 7, 1943 Rainbow ______________ Mar. 17, 1953 Feilden ________________ Sept. 8, 1953 Butler _________________ Feb. 2, 1954 Edsall et al. ____________ Apr. 19, 1960 FOREIGN PATENTS Great Britain ____________ Feb. 8, 1937PDF Image | KRONOGARD AUTOMOTIVE GAS TURBINE POWER PLANT
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