Английская Википедия:Hans von Ohain

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Hans Joachim Pabst von Ohain (14 December 1911Шаблон:Spaced ndash13 March 1998) was a German physicist, engineer, and the designer of the first turbojet engine to power an aircraft.[1] Together with Frank Whittle he has been described as the co-inventor of the turbojet engine however, the historical timelines show that von Ohain was still a university student when in January 1930, Whittle filed his first patent for a turbojet engine and Whittle successfully ran his first engine in April 1937, some 6 months before von Ohain. Additionally, prior to designing engine and filing his own patent in 1935, von Ohain had read and critiqued Whittle's patents.[2][3][4][5][6][7][8] Von Ohain stated in his biography, that "My interest in jet propulsion began in the fall of 1933 when I was in my seventh semester at Göttingen University. I didn't know that many people before me had the same thought.".[9] Unlike Whittle von Ohain had the significant advantage of being supported by an aircraft manufacturer, Heinkel who funded his work.

When in 1935 von Ohain designed his overall engine layout, he based it for compactness on a centrifugal impeller (centrifugal or radial compressor) and a radial inflow turbine.[10]

Ultimately this configuration had too many shortcomings to be to be put into production, however aided by the enormous resources of the Heinkel Aircraft Company, a developed version was sufficient to power the He-178, and on 27 August 1939, von Ohain entered history, as the designer of the world's first gas turbine to power an aircraft.

Von Ohain stayed with centrifugal designs, contributing his research to Heinkel's other projects, such as the combined centrifugal/axial HeS8 and 011 [11] but ultimately, none of his designs were put into production and other competing German designers at Junkers and BMW, following the axial design layout, saw their engines in production, although they never solved some of the basic power and durability problems. Von Ohain nevertheless started the world's first jet engine industry in his homeland of Germany with many prototypes and series productions built till 1945.

Von Ohain, having entered turbojet design some time later than Whittle, began working on his first turbojet engine designs during the same period that Whittle was building his WU engine in Britain. Their turbojet designs have been said by some, to be an example of simultaneous invention.[12] However, von Ohain explains in his biography, that in 1935, while his own patent was being prepared,(and before he had begun construction of an engine) his lawyer gave him a copy of Whittle's patent which he read and critiqued. As a result, he was forced to modify his own application, so as not to infringe on Whittle's design.[13]

The core of Ohain's first jet engine, the Heinkel HeS 1, which he described as his "hydrogen test engine" was run "in March or early April" according to Ohain (although Ernst Heinkel's diaries record it as September 1937).[14]

[15] Work on the hydrogen test engine continued but the engine required modifications to cure overtemperature problems and to fit a fuel system to enable it to run self-contained on liquid fuel which was achieved in September 1937.[16][17] With the heavy backing of Heinkel, Ohain's jet engine was the first to power an aircraft, the Heinkel He 178 aircraft in 1939, which was followed by Whittle's engine within the Gloster E.28/39 in 1941.[18] Turbojet powered fighter aircraft from both Germany and Britain entered operational use virtually simultaneously in July, 1944, the Me 262 on July 26 and the Gloster Meteor on July 27 of 1944,Шаблон:Sfn[19]Шаблон:Sfn[20] so the Me 262 was the first operational fighter jet and saw flight combat with hundreds of machines, while the few dozen Meteors saw limited action.

After the war the two men met, became friends and received the Charles Stark Draper Prize for Engineering "for their independent development of the turbojet engine."[21][22]

Early life and jet development

Born in Dessau, Germany,[23] Ohain earned a PhD in physics in 1933, with his thesis on an optical microphone to record sound directly to film, at the University of Göttingen,[24] then one of the major centers for aeronautical research, having attended lectures by Ludwig Prandtl.[25] In 1933, while still a student, he conceived what he called "an engine that did not require a propeller".[23]

After receiving his second degree in Physics and Aerodynamics[24] in 1935, Ohain became the junior assistant of Robert Wichard Pohl, then director of the Physical Institute of the university. In 1936, while working for Pohl, Ohain registered a patent on his version of a jet engine, Process and Apparatus for Producing Airstreams for Propelling Airplanes.[26] Unlike Frank Whittle's Power Jets WU design with its axial flow turbine, Ohain used a radial in-flow turbine to go with a centrifugal compressor, placing them back-to-back with an annular combustion space wrapped around the rotor.

While working at the university, Ohain used to take his sports car to be serviced at a local garage, Bartles and Becker. There he met an automotive mechanic, Max Hahn, and eventually arranged for him to build a demonstration model of his engine for Шаблон:Reichsmark. The completed model was larger in diameter than Whittle's fully working engine of 1937, although much shorter. Ohain took the model to the university for testing but ran into problems with combustion of the petrol fuel, which took place mostly after the turbine, sending flames shooting out from the exhaust duct. The lack of combustion before the turbine contributed to the engine being unable to run without the assistance of the electric motor which subsequently overheated.

Файл:Hans von Ohain test engine engine-with Max Hahn.jpg
Mechanic Max Hahn and the major components of Hans von Ohain's test engine

According to von Ohain, "My interest in jet engines began in about 1933. I found that the elegance of flying was spoiled by the enormous vibrations and noise from the piston engine/propeller combination. I came to the conclusion that a constant work process, i.e. constant compression, combustion, expansion, would have great advantages. Thus I chose a quite simple engine, a radial compressor with a radial turbine."

However, the model he and Max Hahn built and tested in the courtyard of the Institute showed the combustion chamber needed further development. As a consequence, Pohl and von Ohain decided to approach Heinkel as someone who "doesn't back away from new ideas".[27]

Heinkel

In February 1936, Pohl wrote to Ernst Heinkel, telling him about Ohain's design and its possibilities. Heinkel arranged a meeting between his engineers and Ohain, during which he argued that the current "garage engine" would never work, but that the concept upon which it was based was sound. The engineers were convinced, and in April Ohain and Hahn began working for Heinkel[28] at the Marienehe airfield outside Rostock, in Warnemuende.

Working with Engineer Gundermann and Hahn in Special Development, von Ohain states: "Under pressure of aiming to bring a combustion chamber of unknown endurance to flight readiness, I came upon the idea of separating the turbine problem from the combustion chamber problem by using hydrogen fuel. As a physicist, I knew of course that the diffusion and combustion speed of gaseous hydrogen was substantially greater than that of petrol."[27]

A study of the model's airflow resulted in several improvements over a two-month period. Encouraged by these findings, Ohain produced a new prototype that would run on hydrogen gas supplied by an external pressurised source. The resulting Heinkel-Strahltriebwerk 1 (HeS 1), German for Heinkel Jet Engine 1, was built by hand-picking some of the best machinists in the company, much to the chagrin of the shop-floor supervisors. Hahn, meanwhile, worked on the combustion problem, an area in which he had some experience.

The engine was extremely simple, made largely of sheet metal. Construction, by the blacksmith in his village, started late in the summer of 1936 and was completed in March 1937. Two weeks later the engine was running on hydrogen, but the high temperature exhaust led to considerable "burning" of the metal. The tests were otherwise successful, and in September the combustor was replaced and the engine was run on gasoline for the first time. Running on gasoline caused the combustor to clog up. Although the engine was never intended to be a flight-quality design, it proved beyond a doubt that the basic concept was workable, and Ohain had at last caught up with Whittle. With vastly more funding and industry support, Ohain would soon overtake Whittle and forge ahead.

Unaware of Whittle?

Шаблон:Original research section It has often been claimed that Ohain was unaware of Whittle's work. [29]While in a very strict sense this may be true (in that he was unaware of Whittle's experiments at Lutterworth where the RAF engineer ran the world's first jet engine on the 12th of April 1937), nevertheless Ohain had been given a copy of Whittle's patents by his lawyer, while his own patent application being prepared and before he had begun construction of an engine.

In his biography, Ohain frankly critiqued Whittle's design:[30]

"When I saw Whittle's patent I was almost convinced that it had something to do with boundary layer suction combinations. It had a two-flow, dual entrance flow radial flow compressor that looked monstrous from an engine point of view. Its flow reversal looked to us to be an undesirable thing, but it turned out that it wasn't so bad after although it gave some minor instability problems ... Our patent claims had to be narrowed in comparison to Whittle's because Whittle showed certain things." He then somewhat understandably justified their knowledge of Whittle's work by saying: "We felt that it looked like a patent of an idea ... We thought that it was not seriously being worked on."

Developing the engine

In February 1937, the turbine section was running on a test stand. According to von Ohain, "We were now working on a machine capable of powering an aircraft, the forerunner of the He-S3B. I had intended to put the combustion chamber between the compressor and the turbine, as we had done with the hydrogen unit, but Hahn suggested putting it ahead of them, which was an excellent idea." The He-S3 turbine was test flown by Erich Warsitz and Walter Künzel in a Heinkel He 118, providing additional throttled thrust to the conventional engine.[27]Шаблон:Rp

While work on the HeS 1 continued, the Pohl-Ohain team had already moved on to the design of a flight-quality engine, the HeS 3. The major differences were the use of machined compressor and turbine stages, replacing the bent and folded sheet metal, and a re-arrangement of the layout to reduce the cross-sectional area of the engine by placing the annular combustor in an extended gap between the compressor and turbine. The original turbine was too small to work efficiently.

In the beginning of 1939, the He-S3A was fitted into the He 178 airframe for a standing display at Roggentin on 3 July 1939. Yet this turbine was still not powerful enough for flight. According to von Ohain, "We experimented with various combinations to modify the compressor diffuser and turbine nozzle vanes to increase thrust sufficiently to qualify the aircraft for the first flight demonstration. We found that a small diffuser behind the engine with a collar and splitter to divert flows functioned better than a high speed flow through the entire tube. The final result of the changes was the He-S3B."[27]Шаблон:Rp

Файл:NASM-A19810039000cp05.jpg
Hans von Ohain's Centrifugal compressor /Radial inflow turbine HeS3B

A new design, the HeS 3b was proposed,[28] which lengthened the combustor by placing the forward part of it in front of the compressor outer rim. While not as small as the original HeS 3 design, the 3b was nevertheless fairly compact. The 3b first ran in July 1939 (some references say in May), and was air-tested under the Heinkel He 118 dive bomber prototype. The original 3b engine soon burned out, but a second one was nearing completion at about the same time as a new test airframe, the Heinkel He 178, which first flew on 27 August 1939, the first jet-powered aircraft to fly by test pilot Erich Warsitz. Heinkel had applied, May 31, 1939, for a patent: US2256198 Espacenet - Original document, an 'Aircraft power plant', inventor Max Hahn. First application for this patent in Germany was May, 1938.

Файл:Heinkel He 178 050602-F-1234P-002.jpg
Heinkel He 178 050602-F-1234P-002
Файл:Hans von Ohain and Ernst Heinkel celebrate the first jet flight.jpg
Hans von Ohain leads a toast after the successful flight of the Heinkel He 178. Ernst Heinkel raises his glass on the left side of the image.

Work started immediately on larger versions, first the HeS 6 which was simply a larger HeS 3b, and then on a new design known as the HeS 8 which once again re-arranged the overall layout. The compressor and turbine were connected with a large-diameter drum long-enough to fit an annular combustion chamber between them. It was intended to install the engine on the Heinkel He 280 fighter, but the airframe development progressed much more smoothly than the engine, and had to be used in gliding tests while work on the engine continued. A flight-quality HeS 8 was installed in late March 1941, followed by the first flight on 2 April. Three days later the aircraft was demonstrated for a party of Nazi and RLM officials, all of whom were impressed. Full development funds soon followed.

By this point there were a number of turbojet developments taking place in Germany. Heinkel was so impressed by the concept that he arranged the transfer to the project of Adolph Müller from Junkers, who was developing an axial compressor-powered design, renamed as the Heinkel HeS 30. Müller left Junkers after they purchased the Junkers Motoren company, who had their own project under way, which by this time was known as the Junkers Jumo 004. Meanwhile, BMW was making good progress with its own design, the BMW 003.

By early 1942 the HeS 8, officially the 109-001 (HeS 001), was still not progressing well. Meanwhile, Müller's HeS 30, officially the 109-006 (HeS 006), was developing much more quickly. Both engines were still some time from being ready for production, however, while the 003 and 004 appeared to be ready to go. In early 1942 the director of jet development at the RLM, Helmut Schelp, refused further funding for both designs, and ordered Heinkel to work on a new "pet project" of his own, eventually becoming the Heinkel HeS 011. Although this was the first of Schelp's "Class II" engines to start working well, production had still not started when the war ended. Work continued on the HeS 8 for some time, but it was eventually abandoned in the spring of 1943.

Ultimate outcome

Part of the challenge for von Ohain was his approach to designing a practical turbojet that could be developed. His primary design comprised a centrifugal compressor with a radial inflow turbine, a design that proved to be impractical and as a result, despite much effort, was never put into production.

By comparison, Whittle's centrifugal flow engines, in both straight-through and reverse flow configuration (developed further by Rolls Royce), powered all Allied World War Ii jets and the majority of immediate post-war fighters. They were built under licence in numerous countries including Australia, France and the US and were copied by the Russians and Chinese to power the MiG-15 and MiG-17. Whittle's basic reverse flow design remains the most common gas turbine configuration in production today with over 80,000 built in the form of the Allison (RR) 250/300 and Pratt & Whitney PT6 series of engines.[31][32][33]

However, in his invention of HE S011, von Ohain introduced a standard concept which combined axial and radial designs for most business jets today, along with turboprops and helicopters.[34]

Post-World War II

In 1947, Ohain was brought to the United States by Operation Paperclip and went to work for the United States Air Force at Wright-Patterson Air Force Base.[23] In 1956 he was made the Director of the Air Force Aeronautical Research Laboratory and by 1975 he was the Chief Scientist of the Aero Propulsion Laboratory there.[23]

During his work at Wright-Patterson, Ohain continued his own personal work on various topics. In the early 1960s he did a fair amount of work on the design of gas core reactor rockets which would retain the nuclear fuel while allowing the working mass to be used as exhaust. The engineering needed for this role was also used for a variety of other "down to earth" purposes, including centrifuges and pumps. Ohain would later use the basic mass-flow techniques of these designs to create a fascinating jet engine with no moving parts,[35] in which the airflow through the engine created a stable vortex that acted as the compressor and turbine.

This interest in mass-flow led Ohain to research magnetohydrodynamics (MHD) for power generation,[36] noting that the hot gases from a coal-fired plant could be used to extract power from their speed when exiting the combustion chamber, remaining hot enough to then power a conventional steam turbine. Thus an MHD generator could extract further power from the coal, and lead to greater efficiencies. Unfortunately this design has proven difficult to build due to a lack of proper materials, namely high-temperature non-magnetic materials that are also able to withstand the chemically active exhaust. Ohain also investigated other power related concepts.[37]

He also invented[38] the idea of the "jet wing", in which air from the compressor of a jet engine is bled off to large "augmented" vents in the wings to provide lift for VTOL aircraft. A small amount of high-pressure air is blown into a venturi, which in turn sucks a much larger volume of air along with it, thus leading to "thrust augmentation". The concept was used in the Rockwell XFV-12 experimental aircraft, although the market interest in VTOL aircraft was short-lived. He participated in several other patents.[39]

Ohain was the influence in shifting the mind of Paul Bevilaqua, one of his students at WP-AFB, from math to engineering,[40] which later enabled Bevilaqua to invent the Rolls-Royce LiftSystem for the JSF F35B STOVL: "in school I learned how to move the pieces, and Hans taught me how to play chess".[41] Ohain also showed Bevilaqua "what those TS-diagrams actually mean".[42]

Ohain retired from Wright-Patterson in 1979 and took up an associate professor position teaching propulsion and thermodynamics at the nearby University of Dayton,[28] spending winter sessions from 1981 to 1983 teaching the same subjects at the University of Florida. Ohain continued at the University of Dayton until 1992, when concerns about his health prompted a move with his wife, Hanny, to Melbourne, Florida.[43]

Awards

During his career, Ohain won many engineering and management awards, including (among others) the American Institute of Aeronautics and Astronautics (AIAA) Goddard Astronautics Award, the United States Air Force Exceptional Civilian Service Award, Systems Command Award for Exceptional Civilian Service, the Eugene M. Zuckert Management Award, the Air Force Special Achievement Award, and just before he retired, the Citation of Honor. In 1984–85, Ohain served as the Charles A. Lindbergh Chair in Aerospace History, a competitive senior fellowship at the National Air and Space Museum.[44] In 1991 Ohain and Whittle were jointly awarded the Charles Stark Draper Prize for their work on turbojet engines. Ohain was elected a member of the U.S. National Academy of Engineering (NAE).[23]

Ohain was awarded the Ludwig-Prandtl-Ring from the Deutsche Gesellschaft für Luft- und Raumfahrt (German Society for Aeronautics and Astronautics) for "outstanding contribution in the field of aerospace engineering" in 1992.[45]

In 1982, Ohain was inducted into the International Air & Space Hall of Fame at the San Diego Air & Space Museum.[46]

In 1990, Ohain was inducted into the National Aviation Hall of Fame.[47]

Death

Ohain died in Melbourne, Florida, in 1998, aged 86.[48] He was survived by his wife and four children.[49] One of his sons, Christopher von Ohain, joined USMC. Christopher’s son, Hans Christopher von Ohain, also joined USMC, was killed during a car accident in 2022.[50]

See also

References

Шаблон:Reflist

Sources

External links

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  1. ↑ Шаблон:Cite web
  2. ↑ Golley,John-Genesis of the Jet Airlife Publishing 1995 p 86
  3. ↑ Margaret Conner, Hans von Ohain: Elegance in Flight (Reston, Virginia: American Institute for Aeronautics and Astronautics, Inc., 2001), page 31
  4. ↑ Шаблон:Cite web
  5. ↑ Шаблон:Citation
  6. ↑ Шаблон:Cite web
  7. ↑ Шаблон:Cite web
  8. ↑ Шаблон:Cite web
  9. ↑ Margaret Conner, Hans von Ohain: Elegance in Flight (Reston, Virginia: American Institute for Aeronautics and Astronautics, Inc., 2001), page 31
  10. ↑ Margaret Conner, Hans von Ohain: Elegance in Flight (Reston, Virginia: American Institute for Aeronautics and Astronautics, Inc., 2001), page 131-133
  11. ↑ Margaret Conner, Hans von Ohain: Elegance in Flight (Reston, Virginia: American Institute for Aeronautics and Astronautics, Inc., 2001), page 124-131
  12. ↑ Шаблон:Cite web
  13. ↑ Conner, Margaret (2001). hans von Ohain – Elegance in Flight. American Institute for Aeronautics and Astronautics, Inc. ISBN 1563475200.
  14. ↑ Margaret Conner, Hans von Ohain: Elegance in Flight (Reston, Virginia: American Institute for Aeronautics and Astronautics, Inc., 2001), page 62
  15. ↑ Шаблон:Cite web
  16. ↑ Шаблон:Cite web
  17. ↑ Margaret Conner, Hans von Ohain: Elegance in Flight (Reston, Virginia: American Institute for Aeronautics and Astronautics, Inc., 2001), page 63
  18. ↑ Koehler 1999, p. 173.
  19. ↑ Шаблон:Cite book
  20. ↑ Шаблон:Cite web
  21. ↑ Klooster 2009, p. 459.
  22. ↑ Шаблон:Cite web
  23. ↑ 23,0 23,1 23,2 23,3 23,4 Шаблон:Cite web
  24. ↑ 24,0 24,1 Шаблон:Cite web
  25. ↑ Constant, Edward. "Genesis N + 1: The origins of the Turbo-Jet revolution" Шаблон:ISBN Retrieved: 1 August 2010.
  26. ↑ On 10 November 1935, Ohain filed patent 317/38 for a turbojet engine. See: Margaret Conner, Hans von Ohain: Elegance in Flight (Reston, Virginia: American Institute for Aeronautics and Astronautics, Inc., 2001), page 34. Copies of some pages from this patent appear (with English translations) on pages 125 and 126.
  27. ↑ 27,0 27,1 27,2 27,3 Шаблон:Cite book
  28. ↑ 28,0 28,1 28,2 Шаблон:Cite web
  29. ↑ https://www.bartleby.com/essay/The-Jet-Engine-The-Inventions-Of-The-PJTK5MMMF6
  30. ↑ Шаблон:Cite book
  31. ↑ Шаблон:Cite web
  32. ↑ Шаблон:Cite web
  33. ↑ Шаблон:Cite news
  34. ↑ Шаблон:Cite web
  35. ↑ Hans von Ohain et al. Hot gas flow generator with no moving parts Шаблон:Webarchive United States Patent 4689950, 1 September 1987, and 4756154 Шаблон:Webarchive, 12 July 1988. Retrieved: 23 September 2010.
  36. ↑ Sears, William R. Memorial Tributes (copy) page 237 National Academy of Engineering, 2002; Шаблон:ISBN, Шаблон:ISBN Retrieved: 23 September 2010.
  37. ↑ Hans von Ohain et al. Two component electro-fluid-dynamic power generator employing contact ionization United States Patent 3465180, 2 September 1969; retrieved 23 September 2010.
  38. ↑ "Jet pump or Thrust augmentor", United States Patent 3525474, 25august1970
  39. ↑ List of patents by Hans von Ohain Шаблон:Webarchive; retrieved December 2009.
  40. ↑ Bevilaqua interview Шаблон:Webarchive, retrieved from Engineering newspaper December 2009.
  41. ↑ LM Video Шаблон:Webarchive, retrieved from Engineering newspaper December 2009. Link also at http://www.lockheedmartin.com/how/stories/f35_player.htmlШаблон:Dead link
  42. ↑ Karen Auguston Field, The man with the fan Шаблон:Webarchive, Design News, 22 February 2004; retrieved January 2010.
  43. ↑ Margaret Conner, Hans von Ohain: Elegance in Flight (Reston, Virginia: American Institute for Aeronautics and Astronautics, Inc., 2001), pages 232-240
  44. ↑ Шаблон:Cite book
  45. ↑ Шаблон:Cite web
  46. ↑ Sprekelmeyer, Linda, editor. These We Honor: The International Aerospace Hall of Fame. Donning Co. Publishers, 2006. Шаблон:ISBN.
  47. ↑ Шаблон:Cite web
  48. ↑ Шаблон:Cite web
  49. ↑ Шаблон:Cite news
  50. ↑ Шаблон:Cite web
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