György Jendrassik

György Jendrassik or George Jendrassik (1898 Budapest – 1954 London) was a Hungarian physicist and mechanical engineer.

Jendrassik completed his education at Budapest's József Technical University, then at the University of Berlin, where he attended lectures of the famous physicists Albert Einstein and Max Planck. In 1922, he obtained his diploma in mechanical engineering in Budapest. From 1927 onward, he worked at Ganz Rt, where he helped to develop diesel engines, of which the first few pieces were made with single and double cylinders. Later, the 4- and 6-cylinder four-stroke versions were developed, without compression and with mixing chamber.

Diesel Engines

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Jendrassik started working at Ganz and Company - Danubius Electricity, Machine, Waggon and Shipyard Ltd. He started his activities within the Study Department, which was the development and experimental department. His first work included the strength calculation and preparation of the load tests for the main girders of a new type of wagon for the Dutch coastal local railways. At this time, the main focus of the Study Department was the development of a medium-speed semi-diesel engine. This gave Jendrassik the opportunity to study the theoretical and practical problems of the diesel engine. Jendrassik's interest soon turned to the development of diesel engines. He developed a number of patents which laid the foundations for the development of small and medium-performance diesel engines for use in vehicles. After two years of development work, the Jm 130 single-cylinder engine was produced in 1927. It had a bore of 130 mm, a stroke of 160 mm, and produced 12 hp at 1000 rpm with a specific consumption of 210 grams. This was later developed into two-, four- and six-cylinder versions, which were stable, suitable for rail and marine propulsion, and which featured a combustion chamber in the front. In 1927, seeing the success of the diesel engines, Jendrassik developed the first patents and engines within the Study Department, and in the summer of 1927 the independent Jendrassik Engine Construction Department was established. This department continued to operate after Jendrassik's death until the end of 1958. The Ganz-Jendrassik engines were the start of the motorisation of the railways, but diesel engines were also used in shipping and road vehicles.

His patents and invetions were bought by several major engine manufacturers in Europe, including the Hispano-Suiza and the British Vickers, which were the leading engine manufacturers at the time. Jendrassik was fluent in German, French, English and Spanish, due to his frequent trips to the headquarters of large Western European engineering companies in the affairs of the Ganz company and in the case of the sale of his own patents. He set up a private office in 1934, where he and his colleagues designed a six-cylinder V-type diesel engine for Hispano-Suiza. He also maintained his own office alongside Ganz Rt.

In 1934, he married Johanna Schmall, the eldest daughter of Henrik Schmall, a qualified architect. The increasingly perfected Jendrassik engines became known all over the world and enhanced the reputation of Hungarian industry, the Ganz factory and not least György Jendrassik. In addition to his constant engine development activities, he was also involved in the realisation of gas turbines. In his private office, the thermodynamic calculations for the future gas turbine were carried out.

Turboprop

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Later on, Jendrassik worked on gas turbines and in order to speed up research, he established the Invention Development and Marketing Co. Ltd. in 1936. The next year he successfully ran a small experimental gas turbine engine of 100 hp.[1]

Jendrassik next began work on a larger turboprop engine, which would emerge as the CS-1 prototype, produced and tested in the Ganz works in Budapest. Of axial-flow design with 15-stage compressor and 7-stage turbine, it incorporated many modern features. With predicted output of 1,000 bhp at 13,500 rpm the Cs-1 stirred interest in the Hungarian aircraft industry with its potential to power a modern generation of high-performance aircraft, and construction was begun of a twin-engined fighter-bomber, the Varga RMI-1 X/H, to be powered by it. Its first bench run took place in 1940, making it the world's first turboprop engine to run. However, combustion problems were experienced which limited the output to around 400 bhp. Development was discontinued in 1941, when an agreement was reached to manufacture the Daimler-Benz DB 605 engine in Hungary.[1][2]

Jendrassik's became the factory's managing director from 1942 to 1945. In recognition of his scientific work, in 1943 he was elected as a corresponding member of the Hungarian Academy of Sciences.

In Exile

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After World War II, he was not able to continue developing gas turbines. As a successful entrepreneur, political distrust surrounded him in the new communist-dominated Hungary. Before the nationalization of large companies, the communist party of Mátyás Rákosi carried out a large-scale political campaign and disparaging propaganda activities against the rich industrialists and large entrepreneurs, and made the rich socially responsible for the poverty after the war. Jendrassik no longer felt safe in Hungary. After a spell in Argentina, he came to London in 1948 to become consultant and director to Metropolitan Railcars Ltd., controlled by Metropolitan Cammell and Metropolitan-Vickers. Since 1949, Jendrassik has also been an external consultant of Power Jets (Research and Development) Ltd., with which he worked with until his death, on the development of a pressure exchanger; this is a promising type of heat engine in which the compression and expansion of a gaseous medium is effected by direct action of the gases involved without the employment of mechanical parts such ad pistons or blades[3] The number of his inventions on record only in Hungary is 77. His last invention of great importance was the pressure-compensating device for jet engines at the Power Jets Ltd.

Patents in Hungary

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During his lifetime, he has been listed on 60 patent applications in Hungary:

Hungarian patent number Date of filing Department code Title of the patent
94510 09.09.1924 V/d/2 Internal combustion engine and method of operation thereof
94538 21.05.1926 V/d/2 Internal combustion engine with variable torque over a wide range
94953 30.09.1926 V/d/2 The fuel pump operating mechanism for internal combustion engines
95627 21.04.1927 V/d/2 Compressorless fuel injection internal combustion engine
98058 22.11.1927 V/e/1 Valve, mainly for fuel pumps or carburettors for thermal power engines
99445 25.06.1928 V/d/2 Device for operating a fuel pump
99555 22.05.1928 V/d/3 Sickle shaped working chamber, roller pump or motor
100249 12.03.1929 XXI/c Diffuser, mainly for centrifugal pumps and compressors
101099 22.03.1929 V/d/1 Radial flow gas turbine wheel, mainly for constant pressure gas turbines
102168 01.01.1930 V/d/2 Compressorless fuel injection internal combustion engine
102467 21.11.1929 V/d/2 Stroke governor for spring-loaded fuel pumps with buffer stroke
103750 03.07.1930 V/d/2 Flushing pump for internal combustion engines
103785 05.04.1930 V/d/2 Equipment for cooling pistons of internal combustion engines with lubricating oil
103968 06.05.1930 XXI/c Piston pump
104125 02.08.1930 V/d/2 Piston pump or engine
104590 10.07.1930 V/d/2 Equipment to facilitate starting of power engines
105614 19.02.19.19.19.31. V/e/2 Method and apparatus for storing energy of currents and returning the stored energy
105664 30.11.1928 V/d/2 Bypass bore or duct for partitions and baffles in the combustion chamber of internal combustion engines with a prechamber system
105928 07.02.1930 V/d/2 Fuel pump actuator
106412 16.10.1930 XXI/c Process and apparatus for the transfer of energy between fluid media
106453 30.05.1931 XXI/c Suction equipment for pumps, especially centrifugal pumps
108105 02.03.1932 V/e/1 Equipment for increasing the heat transfer of fluids flowing in tubes
108126 1932.04.05. V/d/2 Method for eliminating harmful pressure surges in the injection bodies of diesel engines without compressors
109447 10.01.1933 XVIII/a Cooling or heating surfaces for liquid or gaseous media
109728 08.04.1930 V/d/2 Two-stroke internal combustion engine
111353 11.11.1933 V/d/2 Method and apparatus for cooling main and crank pins of rotary shaft valves, especially of internal combustion engines
111446 23.09.1933 V/d/2 Bypass bore or duct for combustion chamber bulkheads and baffles of internal combustion engines with pre-chamber system
111648 14.01.1933 V/d/2 Equipment for fixing antechambers, air receivers, etc. in the cylinder heads of internal combustion engines
113629 22.03.1935. V/e/1 Gland plate
114505 01.04.1935 V/d Operating procedure and equipment for gas turbines
114689 15.06.1935 V/d/3 Drive rods, especially for high-speed engines
114740 09.04.1935 V/d/2 Operating procedure and equipment for internal combustion piston engines, mainly for vehicles
117387 10.06.1936 V/d/2 Equipment for the operational control of engines for motor vehicles
117559 09.07.1936 V/e/1 Piston ring pair in a common piston groove
119895 13.02.1937 V/d/2 Working procedure for gas turbines and gas turbine for carrying out the procedure
120477 31.05.1935 XXI/c Rotary aerodynamic compressor
120831 24.12.1937 V/d/1 Control method for gas turbines and gas turbine for use therewith
120860 26.06.1937 V/d/2 Equipment for gas turbines
121918 26.01.1938 V/d/2 Operating procedure for combustion turbines and turbine equipment for carrying out the procedure
121919 16.04.1938 V/d/2 Operating procedure and equipment for gas turbines
123678 12.07.1938 V/d/2 Process for a group of machines comprising in series and mechanically independent turbines and associated equipment
123679 14.07.1938 V/d/2 Procedure for the control of gas turbines and associated equipment
124290 11.04.1939 V/d/2 Operation procedure and equipment for gas turbines
126422 02.08.1939 V/d/2 Heat exchanger
128044 26.07.1940 V/d/2 Method and apparatus for gas turbine valves for changing the rotational sense of the machinery unit performing the useful work
128045 17.10.1940 XXI/c Process and apparatus for compressor plants for controlling the quantity of working fluid delivered
128611 28.08.1940 V/d/2 Support system for bearings for rotating machines with hot working fluid, mainly gas and steam turbines
130185 03.07.1941 V/e/1 Equipment for damping torsional vibrations
131263 20.12.1941 XVIII/b Dry quenching method and equipment
132904 26.02.1942 V/d/2 Procedure and apparatus for controlling the operation of gas turbines
133514 22.05.1942 II/h Heat exchanger
134340 26.11.1942 V/d/1 Caloric turbine, mainly gas turbine
134341 26.11.1942 V/d/1 Caloric turbine, mainly gas turbine
135274 16.04.1943 II/h Surface heat exchanger, mainly cooling
136421 13.07.1943 V/d/2 Process for the operation of rotating machines with blades of a periodic type according to a periodic operating process, and machine or mechanical apparatus for carrying out the process
136611 28.01.1943 II/h Heat exchanger with thermal storage
137368 21.06.1943 V/d/1 Process for the operation of rotary machines with paddle-cosmos in alternating flow direction and rotary machines for carrying out the process
138415 10.11.1942 V/d/2 Method and apparatus for the control of variable speed turbine gas turbine plants
139149 12.02.1946 XVIII/h Process and apparatus for cooling high temperature gaseous media

References

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  1. ^ a b Green, W. and Swanborough, G.; "Plane Facts", Air Enthusiast Vol. 1 No. 1 (1971), Page 53.
  2. ^ Gunston World, p.111
  3. ^ "Archived copy". Archived from the original on 2016-03-05. Retrieved 2012-02-24.{{cite web}}: CS1 maint: archived copy as title (link)