- Frank Whittle
name = Frank Whittle
image_size = 300px
birth_date = birth date|1907|6|1|df=y
birth_place = Earlsdon,
death_date = death date and age|1996|8|9|1907|6|1|df=y
Columbia, Maryland. United States
nationality = English
known_for = Development of the
education = Peterhouse,
University of Cambridge
Royal Air Force
occupation = RAF officer
title = Sir
spouse = Dorothy Lee (1930–1976)
children = 2 sons
Air CommodoreSir Frank Whittle, OM, KBE, FRS, Hon FRAeS(1 June 1907 – 9 August 1996) was an English Royal Air Force(RAF) officer. Sharing credit with Germany's Dr. Hans von Ohainfor independently inventing the jet engine, he is hailed as a father of jet propulsion.cite video
people = Frank Whittle
title = Whittle – the Jet Pioneer
url = http://www.thehistorychannel.co.uk/site/tv_guide/full_details/Technology/programme_2819.php
format = History Channel broadcast & DVD
publisher = The History Channel (TV broadcast) & Quantal films (extended DVD of broadcast)
accessdate = 2007-10-05]
From an early age Whittle demonstrated an aptitude for engineering and an interest in flying. Determined to be a pilot, he overcame his physical limitations to be accepted into the RAF where his abilities earned him a place on the officer training course at Cranwell. He excelled in his studies and became an accomplished pilot. While writing his thesis there he formulated the fundamental concepts that led to the creation of the jet engine, taking out a patent on his design in 1930. His performance on an officers' engineering course bought him a place on a further course at the
University of Cambridgewhere he graduated with a First.
Air Ministrysupport, he and two retired RAF servicemen formed Power JetsLtd to build his engine with assistance from the firm of British Thomson-Houston. Despite limited funding, a prototype was created which first ran in 1937. Official interest was forthcoming following this success with contracts being placed to develop further engines, but the continuing stress seriously affected Whittle's health, eventually resulting in a nervous breakdown in 1940. In 1944 when Power Jets was nationalised he again suffered a nervous breakdown, and resigned from the board in 1946.
In 1948 Whittle retired from the RAF and received a knighthood. He joined BOAC as a technical advisor before working as an engineering specialist in one of Shell Oil's subsidiaries followed by a position with Bristol Aero Engines. After emigrating to the U.S. in 1976 he accepted the position of NAVAIR Research Professor at the
United States Naval Academyfrom 1977–1979. In August 1996, Whittle died of lung cancer at his home in Columbia, Maryland.
Whittle was born in a
terraced housein Earlsdon, Coventry, Englandon 1 June 1907, the eldest son of Moses and Sara Alice Whittle. [http://www.raf.mod.uk/history_old/whittle1.html Whittle's biography on the RAF history website p. 1] Retrieved: 18 July 2008] When he was nine years old, the family moved to the nearby town of Royal Leamington Spa where his father, a highly inventive practical engineer and mechanic,Details from the Sir Frank Whittle Jet Heritage Centre display at the Midland Air Museum] purchased the Leamington Valve and Piston Ring Company which comprised a few lathes and other tools, and a single-cylinder gas engine on which Whittle became an expert." [http://www2.eng.cam.ac.uk/~bcb/whittle/telgraph.htm Sir Frank Whittle] ", The Daily Telegraph, Obituaries, August 10, 1996] Whittle developed a rebellious and adventurous streak together with an early interest in aviation.
After two years attending Milverton School, Whittle won a scholarship to a secondary school which in due course became Leamington College, but when his father's business faltered there was not enough money to keep him there. He quickly developed practical engineering skills while helping in his father's workshop, and being an enthusiastic reader spent much of his spare time in the Leamington reference library, reading about astronomy, engineering, turbines, and the theory of flight. At the age of 15, determined to be a pilot, Whittle applied to join the RAF.
Entering the RAF
In January 1923, having passed the RAF entrance examination, Whittle reported to
RAF Haltonas an aircraft apprentice. He lasted only two days: just five feet tall and with a small chest measurement, he failed the medical. He then put himself through a vigorous training program and special diet devised by a physical training instructor at Halton to build up his physique, only to fail again six months later when he was told that he could not be given a second chance, despite having added three inches to his height and chest. Undeterred, he applied again under an assumed name and presented himself as a candidate at the RAF Cranwellapprentice school instead. This time he passed the physical, and in September that year, 364365 Boy Whittle, F started his three-year training as an aircraft mechanic at the No. 4 Apprentices Wing, No. 1 School of Technical Training.
Whittle hated the strict discipline, and convinced there was no hope of ever becoming a pilot, at one time seriously considered deserting. However, throughout his early days as an aircraft apprentice, first at the
Royal Air Force College Cranwell, and latterly at RAF Halton, he maintained his interest in the Model Aircraft Society where he built replicas. The quality of these attracted the eye of his commanding officer, who felt that Whittle was also a mathematical genius. He was so impressed that in 1926 he recommended Whittle for officer training at Cranwell, a rarity for a " commoner" in what was still a very class-based military structure.
For Whittle, this was the chance of a lifetime, not only to enter the officer corps but also because the training included flying lessons on the
Avro 504. While at Cranwell he lodged in a bungalow at Dorrington. Being an ex-apprentice amongst a majority of ex-public schoolboys, life as an officer cadet wasn't easy for him, but he nevertheless excelled in the courses and went solo in 1927 after only 13.5 hours instruction, quickly progressing to the Bristol Fighterand gaining a reputation for daredevil low flying and aerobatics.
A requirement of the course was that each student had to produce a thesis for graduation: Whittle decided to write his on potential aircraft design developments, notably flight at high altitudes and speeds over 500 mph (800 km/h). In "Future Developments in Aircraft Design" he showed that incremental improvements in existing propeller engines were unlikely to make such flight routine. Instead he described what is today referred to as a
motorjet; a motor using a conventional piston engineto provide compressed air to a combustion chamber whose exhaust was used directly for thrust – essentially an afterburnerattached to a propeller engine. The idea was not new and had been talked about for some time in the industry, but Whittle's aim was to demonstrate that at increased altitudes the lower outside air pressure would increase the design's efficiency. For long-range flight, using an Atlantic-crossing mailplane as his example, the engine would spend most of its time at high altitude and thus could outperform a conventional powerplant.
Of the few apprentices accepted, only about one percent normally completed the course, and Whittle graduated in 1928 at the age of 21. He ranked second in his class in academics, won the Andy Fellowes Memorial Prize for Aeronautical Sciences for his thesis, and was described as an "exceptional to above average" pilot. However, his flight logbook also showed numerous red ink warnings about showboating and overconfidence, and because of dangerous flying in an
Armstrong Whitworth Siskinhe was disqualified from the end of term flying contest.
Development of the jet engine
Whittle continued working on the motorjet principle after his thesis work but eventually abandoned it when further calculations showed it would weigh as much as a conventional engine of the same thrust. Pondering the problem he thought: "Why not substitute a turbine for the piston engine?" Instead of using a piston engine to provide the compressed air for the burner, a turbine could be used to extract some power from the exhaust and drive a similar compressor to those used for
superchargers. The remaining exhaust thrust would power the aircraft. [" [http://www.warbirdforum.com/whittle.htm Gentlemen, I give you the Whittle engine] "]
On 27 August 1928 Pilot Officer Whittle joined No. 111 Squadron, Hornchurch, flying Siskin IIIs. Continuing his reputation for low flying and aerobatics, one public complaint almost led to him being court-martialled. [http://www.raf.mod.uk/history_old/whittle2.html Whittle's biography on the RAF history website p. 2] Retrieved: 18 July 2008] Within a year he was posted to
Central Flying School, Wittering, for a flying instructor's course. He became a popular and gifted instructor, and was selected as one of the entrants in a competition to select a team to perform the "crazy flying" routine in the 1930 Royal Air Force Air Display at RAF Hendon. He destroyed two aircraft in accidents during rehearsals but remained unscathed on both occasions. After the second incident an enraged Flight Lieutenant Harold W Raeburn said furiously, "Why don't you take all my bloody aeroplanes, make a heap of them in the middle of the aerodrome and set fire to them – it's quicker!"
Whittle showed his engine concept around the base where it attracted the attention of Flying Officer Pat Johnson, formerly a patent examiner. Johnson, in turn, took the concept to the commanding officer of the base. This set into motion a chain of events that almost led to the engine being produced much sooner than actually occurred.
Earlier, in July 1926, A. A. Griffith published a paper on compressors and turbines, which he had been studying at the
Royal Aircraft Establishment(RAE). He showed that such designs up to this point had been flying "stalled", and that by giving the compressor blades an aerofoil-shaped cross-section their efficiency could be dramatically improved. The paper went on to describe how the increased efficiency of these sorts of compressors and turbines would allow a jet engine to be produced, although he felt the idea was impractical, and instead suggested using the power as a turboprop. At the time most superchargers used a centrifugal compressor, so there was limited interest in the paper.
Encouraged by his Commanding Officer, in late 1929 Whittle sent his concept to the
Air Ministryto see if it would be of any interest to them. With little knowledge of the topic they turned to the only other person who had written on the subject and passed the paper on to Griffith. Griffith appears to have been convinced that Whittle's "simple" design could never achieve the sorts of efficiencies needed for a practical engine. After pointing out an error in one of Whittle's calculations, he went on to comment that the centrifugal design would be too large for aircraft use and that using the jet directly for power would be rather inefficient. The RAF returned comment to Whittle, referring to the design as being "impracticable".
Pat Johnson remained convinced of the validity of the idea, and had Whittle patent the idea in January 1930. Since the RAF was not interested in the concept they did not declare it secret, meaning that Whittle was able to retain the rights to the idea which would have otherwise been their property. Johnson arranged a meeting with
British Thomson-Houston(BTH) whose chief turbine engineer seemed to agree with the basic idea. However, BTH did not want to spend the ₤60,000 it would cost to develop it and this potential brush with early success went no further.
In Coventry, on 24 May 1930, Whittle married his fiancée, Dorothy Mary Lee, with whom he would later have two sons, David and Ian. Then, in 1931, he was posted to the
Marine Aircraft Experimental Establishmentat Felixstoweas an armament officer and test pilot of seaplanes where he continued to publicize his idea. This posting came as a surprise as he had never previously flown a seaplane, but he nevertheless increased his reputation as a pilot by flying some 20 different types of floatplanes, flying boats and amphibians. Every officer with a permanent commission was expected to take a specialist course, and as a result Whittle attended the Officers’ Engineering Course at RAF Henlow, Bedfordshirein 1932. He obtained an aggregate of 98% in all subjects in his exams, completing the course in 18 months instead of the more normal two years.
His performance in the course was so exceptional, that in 1934 he was permitted to take a two-year engineering course as a member of Peterhouse, a college of Cambridge University, graduating in 1936 with a First in the Mechanical Sciences Tripos.
Still at Cambridge, Whittle could ill afford the £5 renewal free for his jet engine patent when it became due in January 1935, and because the Air Ministry refused to pay it the patent was allowed to lapse. Shortly after, in May, he received mail from Rolf Dudley-Williams, who had been with him at Cranwell in the '20s and Felixstowe in 1930. Williams proposed a meeting with Whittle, himself and another now-retired RAF serviceman,
James Collingwood Tinling. The two proposed a partnership that allowed them to act on Whittle's behalf to gather public financing so that development could go ahead.
The agreement soon bore fruit, and in September 1935 the pair introduced Whittle to two investment bankers at O T Falk & Partners, Sir Maurice Bonham-Carter and Lancelot Law Whyte. The firm had an interest in developing speculative projects that conventional banks would not touch. Whyte was impressed by the 28-year-old Whittle and his design when they met on 11 September, 1935:
cquote2|quotetext= The impression he made was overwhelming, I have never been so quickly convinced, or so happy to find one's highest standards met... This was genius, not talent. Whittle expressed his idea with superb conciseness: 'Reciprocating engines are exhausted. They have hundreds of parts jerking to and fro, and they cannot be made more powerful without becoming too complicated. The engine of the future must produce 2,000 hp with one moving part: a spinning turbine and compressor.' |personquoted= Lancelot Law Whyte|quotesource= Lee Payne, " [http://www.afa.org/magazine/jan1982/0182race.html The Great Jet Engine Race... And How We Lost] ", Air Force Magazine, Vol. 65, No. 1 (January 1982)]
Falk & Partners financed an independent engineering review that was favourable, [Nahum 2004, p. 28.] and with that the jet engine was finally on its way to becoming a reality.
On 27 January 1936, the principals signed the "Four Party Agreement", creating "
Power JetsLtd." The parties were O.T. Falk, the Air Ministry, Whittle and together, Williams and Tinling. Falk was represented on the board of Power Jets by Whyte as Chairman, and Bonham-Carter as a director. [Nahum 2004, pp. 34–35.] Whittle, Williams and Tinling retained a 49% share of the company in exchange for Falk and Partners putting in £2,000 with the option of a further £18,000 within 18 months. [http://www.frankwhittle.co.uk/content.php?act=viewDoc&docId=6&docFatherId=1&level=sub POWER JETS A brief biography] , "The Sir Frank Whittle Commemorative Trust"] As Whittle was still a full-time RAF officer and currently at Cambridge, he was given the title "Honorary Chief Engineer and Technical Consultant". Needing special permission to work outside the RAF, he was placed on the Special Duty List and allowed to work on the design as long as it was for no more than six hours a week. [Nahum 2004, p. 35.]
The Air Ministry still saw no value in the effort, and having no production facilities of its own, Power jets entered into an agreement with steam turbine specialists British Thomson-Houston to build an experimental engine facility at a BTH factory in
Rugby, Warwickshire. [Nahum 2004, p. 53.] Work progressed quickly, and by the end of the year the prototype detail design was finalised and parts for it were well on their way to being completed, all within the original £2,000 budget.
Earlier, in January when the company formed,
Henry Tizard, the rector of Imperial College Londonand chairman of the Aeronautical Research Committee(ARC), had prompted the Air Ministry's Director of Scientific Research to ask for a write-up of the design. The report was once again passed on to Griffith for comment, which was not received back until March 1937 by which point Whittle's design was well along. Griffith had already started construction of his own turbine engine design, and perhaps to avoid tainting his own efforts, he returned a somewhat more positive review. However, he remained highly critical of some features, notably the use of jet thrust. The Engine Sub-Committee of ARC studied Griffith's report, and decided to fund his effort instead.
Given this astonishing display of official disinterest, Falk and Partners gave notice that they could not provide funding beyond £5,000. Nevertheless the team pressed ahead, and the W.U. (Whittle Unit) engine ran successfully on 12 April, 1937. Tizard pronounced it "streets ahead" of any other advanced engine he had seen, and managed to interest the
Air Ministryenough to fund development with a contract for £5,000 to develop a flyable version.Nahum 2004, pp. 37–38.] However, it was a year before the funds were made available, greatly delaying development.
In July, when Whittle's stay at Cambridge was over, he was released to work full-time on the engine. On July 8th Falk gave the company an emergency loan of £250, and on the 15th they agreed to find £4,000 to £14,000 in additional funding. The money never arrived, and entering into default, Falk's shares were returned to Williams, Tinling and Whittle on November 1. Nevertheless, Falk arranged another loan of £3,000, and work continued.
Testing continued with the W.U., which showed an alarming tendency to race out of control. Due to the dangerous nature of the work being carried out, development was largely moved from Rugby to BTH's semi-disused Ladywood foundry at nearby
Lutterworthin Leicestershirein 1938 where there was a successful run of the W.U. in March that year. BTH had decided to put in £2,500 of their own in January, and in March 1938 the Air Ministry funds finally arrived. This proved to be a mixed blessing – the company was now subject to the Official Secrets Act, which made it extremely difficult to gather more private equity.
These delays and the lack of funding slowed the project. In Germany,
Hans von Ohainhad started work on a prototype in 1935, and had by this point passed the prototype stage and was building the first flyable design, the Heinkel HeS 3. There is little reason to believe that Whittle's efforts would not have been at the same level or more advanced had the Air Ministry taken a greater interest in the design. When war broke out in September 1939, Power Jets had a payroll of only 10 and Griffith's operations at the RAE and Metropolitan Vickerswere similarly small.
The stress of the continual on-again-off-again development and problems with the engine took a serious toll on Whittle.He suffered from stress-related ailments such as
eczemaand heart palpitations, while his weight dropped to nine stone (126 lb / 57 kg). In order to keep to his 16-hour workdays, he sniffed Benzedrineduring the day and then took tranquilizers and sleeping pills at night to offset the effects and allow him to sleep. Over this period he became irritable and developed an "explosive" temper. [Nahum 2004, pp. 79–80, 89.]
By June 1939 Power Jets could barely afford to keep the lights on when yet another visit was made by Air Ministry personnel. This time Whittle was able to run the W.U. at high power for 20 minutes without any difficulty. One of the members of the team was the Director of Scientific Research,
David Randall Pye, who walked out of the demonstration utterly convinced of the importance of the project. The Ministry agreed to buy the W.U. and then loan it back to them, injecting cash, and placed an order for a flyable version of the engine.
Whittle had already studied the problem of turning the massive W.U. into a flyable design, and with the new contract work started in earnest on the "Whittle Supercharger Type W.1". It featured a reverse-flow design; compressed air from the outer rim of the compressor was fed into the burners and ignited, then piped back towards the front of the engine, reversing again, then finally into the turbine area. This design allowed the flame cans to be folded in length, reducing the length of the engine, and the length of the drive shaft connecting the compressor and turbine, thus reducing weight.
In January 1940, the Ministry placed a contract with the
Gloster Aircraft Companyfor a simple aircraft specifically to flight-test the W.1, the Gloster E.28/39. They also placed a second engine contract, this time for a larger design that developed into the otherwise similar W.2. In February work started on a third design, the W.1A, which was the size of the W.1 but used the W.2's mechanical layout. The W.1A allowed them to flight test the W.2's basic mechanical design in the E.28/39. Power Jets also spent some time in May 1940 drawing up the W.2Y, a similar design with a "straight-through" airflow that resulted in a longer engine and (more critically) driveshaft but having a somewhat simpler layout. To reduce the weight of the driveshaft as much as possible, the W.2Y used a large cylindrical shaft almost as large as the turbine disk, "necked down" at either end where it connected to the turbine and compressor.
In April the Air Ministry issued contracts for W.2 production lines with a capacity of up to 3,000 engines a month in 1942, asking BTH, Vauxhall and the
Rover Companyto join. However, the contract was eventually taken up by Rover only. [Nahum 2004, p. 61.]
Meanwhile work continued with the W.U., which eventually went through nine rebuilds in an attempt to solve the combustion problems that caused the engines to race and surge. On October 9 the W.U. ran once again, this time equipped with Lubbock ("Shell" type) atomizing burners which solved the racing problems, [Developed by Isaac Lubbock of the Shell combustion laboratories in Fulham. Nahum 2004, pp. 80–81.] but surging continued.
By this point it was clear that Gloster's first airframe would be ready long before Rover could deliver an engine. Unwilling to wait, Whittle cobbled together an engine from spare parts, creating the W.1X ("X" standing for experimental) which ran for the first time on 14 December, 1940. On December 10 Whittle suffered a nervous breakdown, and left work for a month. [Nahum 2004, p. 89.] This engine powered the E.28/39 for taxi testing on April 7, 1941 near the factory in Gloucester, where it took to the air for two or three short hops of several hundred yards at about six feet from the ground.
The "full" W.1 of 850
lbf(3.8 kN) thrust ran on 12 April 1941, and on May 15 the W.1-powered E.28/39 took off from Cranwell at 7:40 pm, flying for 17 minutes and reaching a maximum speed of around 340 mph (545 km/h). At the end of the flight, Pat Johnson, who had encouraged Whittle for so long said to him, "Frank, it flies." Whittle replied, "Well, that's what it was bloody well designed to do, wasn't it?" [ [http://www.businessweek.com/magazine/content/04_18/b3881044_mz072.htm Frank Whittle: A Daredevil Who Built Jets] , BusinessWeek]
Within days the aircraft was reaching 370 mph (600 km/h) at 25,000 feet (7,600 m), exceeding the performance of the contemporary Spitfires. Success of the design was now evident; the first example of what was a purely experimental and entirely new engine design was already outperforming one of the best piston engines in the world, an engine that had five years of development and production behind it, and decades of basic engineering. Nearly every engine company in Britain then started their own crash efforts to catch up with Power Jets.
In 1941 Rover set up a new laboratory for Whittle's team along with a production line at their disused
Barnoldswickfactory, but by late 1941 it was obvious that the arrangement between Power Jets and Rover was not working. Whittle was frustrated by Rover's inability to deliver production-quality parts, as well as with their attitude of engineering superiority, and became increasingly outspoken about the problems. Rover decided to secretly set up a parallel effort with their own engineers at Waterloo Mill, Clitheroe. Here Adrian Lombardstarted work developing the W.2B into their own production quality design, dispensing with Whittle's "reverse-flow" burners and developing a longer but simpler "straight-through" engine instead. This was encouraged by the Air Ministry, who gave Whittle's design the name B.23, and Rover's became the B.26.
Work on all of the designs continued over the winter of 1941–42. The first W.1A was completed soon after, and on 2 March 1942, the second E.28/39 reached 430 mph (690 km/h) at 15,000 feet (4,600 m) on this engine. The next month work on an improved W.2B started under the new name, W2/500. In April Whittle learned of Rover's parallel effort, creating discontentment and causing a major crisis in the program. Work continued however, and in September the first W2/500 ran for the first time, generating its full design thrust of 1,750 lbf (7.8 kN) the same day. Work started on a further improvement, the W2/700.
Earlier, in 1940,
Stanley Hookerof Rolls-Royce had met with Whittle and later introduced him to their current CEO, Ernest Hives. Hooker led the supercharger division at Rolls-Royce, which was naturally suited to jet engine work. Hives agreed to supply key parts to help the project and it was Rolls engineers who helped solve the surging problems seen in the early engines. In early 1942 Whittle contracted Rolls for six engines, known as the WR.1, identical to the existing W.1.
The problems between Rover and Power Jets became a "public secret" and late in 1942 Spencer Wilkes of Rover met with Hives and Hooker at the "Swan and Royal" pub near the Barnoldswick factory. They decided to trade the jet factory at Barnoldswick for Rolls' tank engine factory in Nottingham, sealing the deal with a handshake. The official handover took place on 1 January 1943, although the W.2B contract had already been signed over in December. Rolls closed Rover's secret parallel plant at
Clitheroesoon after, however, they continued the development of the W.2B/26 that had begun there.
Testing and production ramp-up was immediately accelerated. In December 1942 Rover had tested the W.2B for a total of 37 hours, but within the next month Rolls-Royce tested it for 390 hours. The W.2B passed its first 100-hour test at full performance of 1,600 lbf (7.1 kN) on 7 May 1943. The prototype Meteor airframe was already complete and took to the air on 12 June 1943. Production versions of the engine started rolling off the line in October, first known as the W.2B/23, then the RB.23 (for Rolls-Barnoldswick) and eventually became known as the
Rolls-Royce Welland. Barnoldswick was too small for full-scale production and turned back into a pure research facility under Hooker's direction, while a new factory was set up in Newcastle-under-Lyme. The W.2B/26, as the Rolls-Royce Derwent, opened the new line and soon replaced the Welland, allowing the production lines at Barnoldswick to shut down in late 1944.
Despite lengthy delays in their own program, the
Luftwaffebeat the British efforts into the air by nine months. A lack of experience and supply of high-temperature steel alloys meant the German designs were always at risk of overheating and damaging their turbines. The Junkers Jumo 004, designed by Dr. Anselm Franz, would typically last only 10–25 hours (longer with an experienced pilot) before burning out, and sometimes exploded on their first startup. Whittle's designs were much more reliable by comparison. The equivalent British engine would run for 150 hours between overhauls and had twice the power-to-weight ratioand half the specific fuel consumption. By the end of the war every major engine company in Britain was working on jet designs based on the Whittle pattern, or licensed outright.
With the W.2 design proceeding smoothly, Whittle was sent to
Boston, Massachusettsin mid-1942 to help the General Electricjet programme. GE, the primary supplier of turbochargers in the U.S., was well-suited to quickly starting jet production. A combination of the W.2B design and a simple airframe from Bell Aircraftflew in autumn of 1942 as the Bell XP-59A Airacomet.
Whittle's developments at Power Jets continued, the W.2/700 later being fitted with an
afterburner("reheat" in British terminology), as well as experimental water injection to cool the engine and allow higher power settings without melting the turbine. Whittle also turned his attention to the axial-flow (straight-through) engine type as championed by Griffith, designing the L.R.1. Other developments included the use of fans to provide greater mass-flow, either at the front of the engine as in a modern turbofanor at the rear, which is much less common but somewhat simpler.
Whittle's work had caused a minor revolution within the British engine manufacturing industry, and even before the E.28/39 flew most companies had set up their own research efforts. In 1939,
Metropolitan-Vickersset up a project to develop an axial-flow design as a turbopropbut later re-engineered the design as a pure jet known as the Metrovick F.2. Rolls-Royce had already copied the W.1 to produce the low-rated WR.1 but later stopped work on this project after taking over Rover's efforts. In 1941, de Havilland started a jet fighter project, the Spider Crabndash later called Vampirendash along with their own engine to power it; Frank Halford's Goblin (Halford H.1). Armstrong Siddeleyalso developed an axial-flow design, the ASX but reversed Vickers' thinking and later modified it into a turboprop instead, the Python.
During a demonstration of the E.28/39 to
Winston Churchillin April 1943, Whittle proposed to Stafford Cripps, Minister of Aircraft Production, that all jet development be nationalised. He pointed out that the company had been funded by private investors who helped develop the engine successfully, only to see production contracts go to other companies. Nationalisation was the only way to repay those debts and ensure a fair deal for everyone, and he was willing to surrender his shares in Power Jets to make this happen. In October, Cripps told Whittle that he decided a better solution would be to nationalise Power Jets only. Whittle believed that he had triggered this decision, but Cripps had already been considering how best to maintain a successful jet programme and act responsibly regarding the state's substantial financial investment, while at the same time wanting to establish a research centre that could utilise Power Jets' talents, and had come to the conclusion that national interests demanded the setting up of a Government-owned establishment. [Nahum 2004, pp. 101, 105.] On December 1 Cripps advised Power Jets' directors that the Treasury would not pay more than £100,000 for the company.
In January 1944 Whittle was awarded the
CBEin the New Year Honours. Later that month after further negotiations the Ministry made another offer of £135,500 for Power Jets, which was reluctantly accepted after the Ministry refused arbitration on the matter. Since Whittle had already offered to surrender his shares he would receive nothing at all, while Williams and Tinling each received almost £46,800 for their stock, and investors of cash or services had a three-fold return on their original investment. [Nahum 2004, p. 102.] Whittle met with Cripps to personally object to the nationalisation efforts and how they were being handled, but to no avail. The final terms were agreed on 28 March, and Power Jets officially became Power Jets (Research and Development) Ltd, with Roxbee Cox as Chairman, Constant of RAE Head of Engineering Division, and Whittle as Chief Technical Advisor. On 5 April 1944, the Ministry sent Whittle an award of only £10,000 for his shares.
From the end of March, Whittle spent six months in hospital recovering from nervous exhaustion, and resigned from Power Jets (R and D) Ltd in January 1946. In July the company was merged with the gas turbine division of RAE to form the
National Gas Turbine Establishment(NGTE) at Farnborough, and 16 Power Jets engineers, following Whittle's example, also resigned. [Nahum 2004, pp. 118–119.]
After the War
socialist, Whittle's experiences with nationalisation changed his mind and he later campaigned for the Conservative Party (especially for his friend Dudley Williams, who was Managing Director of Power Jets and became the Conservative Member of Parliamentfor Exeter).
In 1946 Whittle accepted a post as Technical Advisor on Engine Design and Production to Controller of Supplies (Air); was made Commander, the U.S.
Legion of Merit; and was awarded the Order of the Bath(CB) in 1947. During May 1948 Whittle received an ex-gratia award of £100,000 from the Royal Commission on Awards to Inventors in recognition of his work on the jet engine, and two months later he was made a Knight of the Order of the British Empire(KBE).
During a lecture tour in the U.S. he again broke down and retired from the RAF on medical grounds on 26 August 1948, leaving with the rank of Air Commodore. He joined BOAC as a technical advisor on aircraft gas turbines and travelled extensively over the next few years, viewing jet engine developments in the United States, Canada, Africa, Asia and the Middle East. He left BOAC in 1952 and spent the next year working on a biography, "Jet: The Story of a Pioneer". He was awarded the
Royal Society of Arts' Albert Medal that year.
Returning to work in 1953, he accepted a position as a Mechanical Engineering Specialist in one of Shell Oil's subsidiaries where he developed a new type of self-powered drill, driven by a turbine running on the lubricating mud that is pumped into the borehole during drilling. Normally a well is drilled by attaching rigid sections of pipe together and powering the cutting head by spinning the pipe, but Whittle's design removed the need for a strong mechanical connection between the drill and the head frame, allowing for much lighter piping to be used. He gave the
Royal Institution Christmas Lecturesin 1954 on the "The Story of Petroleum".
Whittle left Shell in 1957 to work for Bristol Aero Engines who picked up the project in 1961, setting up "Bristol Siddeley Whittle Tools" to further develop the concept. In 1966 Rolls-Royce purchased Bristol Siddeley, but the financial pressures and eventual bankruptcy due to cost overruns of the RB211 project led to the slow wind-down and eventual disappearance of Whittle's "turbo-drill". The design would eventually appear only in the late 1990s, when it was combined with a continuous coiled pipe to allow uninterrupted drilling at any angle. "Continuous-coil drilling" has the ability to drill straight down into a pocket of oil and then sideways through the pocket to allow the oil to flow out faster.
In 1976, Whittle's marriage to Dorothy was dissolved and he re-married to American Hazel S Hall ("Tommie"). He emigrated to the U.S. and the next year accepted the position of NAVAIR Research Professor at the
United States Naval Academy( Annapolis, Maryland). [http://www.raf.mod.uk/history_old/whittle4.html Whittle's biography on the RAF history website p. 4] Retrieved: 19 July 2008] His research concentrated on the boundary layerbefore his professorship became part-time from 1978 to 1979. The part-time post enabled him to write a textbook entitled "Gas turbine aero-thermodynamics: with special reference to aircraft propulsion", published in 1981. Having first met Hans von Ohainin 1966, Whittle again met him at Wright-Patterson Air Force Basein 1978 while von Ohain was working there as the Aero Propulsion Laboratory's Chief Scientist. Initially upset because he believed von Ohain's engine had been developed after seeing Whittle's patent, he eventually became convinced that von Ohain's work was in fact independent. [ [http://www.ascho.wpafb.af.mil/encounter.htm Verbatim transcript of a two-day conference, "An Encounter Between the Jet Engine Inventors", held at Wright-Patterson Air Base May 3–4 1978] Retrieved: 19 July 2008] The two became good friends and often toured the U.S. giving talks together.
In 1986 Whittle was appointed a member of the
Order of Merit(Commonwealth). He was made a Fellow of the Royal Society, and of the Royal Aeronautical Society, and in 1991 he and von Ohain were awarded the Charles Stark Draper Prizefor their work on turbojet engines.
Whittle died of lung cancer on 9 August, 1996, at his home in
Columbia, Maryland. He was cremated in America and his ashes were flown to England where they were placed in a memorial in a church in Cranwell.
Coventry, England, UK
* The "Whittle Arch" statue is a large double wing-like structure situated outside the
Coventry Transport Museum, Millennium Place, CoventryCity Centre.
* A statue of Whittle by Faith Winter is situated under the Whittle Arch. It was unveiled on the 1 June 2007 by his son, Ian Whittle, during a televised event. It shows Whittle at
RAF Cranwelllooking towards the sky observing the first test flight of a Gloster-Whittle E28/39 on 15 May 1941.
* There is a school named after Whittle in the
Walsgravesuburb of Coventry. It was called Frank Whittle Primary up until 1997, before being re-named Sir Frank Whittle Primary School. A jet engine replica sits in the reception area of the school, donated by Whittle himself before his death.
* There is a commemorative plaque on the house in Newcombe Road,
Earlsdon, Coventry, in which he was born and brought up until the age of nine years.
Hearsall Common, near to Whittle's birthplace in Coventry, a plaque commemorates where Whittle gained inspiration when he saw an aircraft land.
Coventry Universityhas named one its buildings after him.
* The main hangar at the
Midland Air Museumis called the "The Sir Frank Whittle Jet Heritage Centre".
* Whittle house is one of the four "houses" at
Finham Park School.
* A full-scale model of the E.28/39 Whittle has been erected just outside the northern boundary of
Farnborough Airfieldin Hampshire, UK.
* A similar memorial has been erected in the middle of a
roundaboutoutside Lutterworthwhere much of Whittle's development, including the invention of the jet engine, was carried out.
Sir Frank Whittle Medalis awarded annually by the Royal Academy of Engineeringto an engineer, normally resident in the UK, for outstanding and sustained achievement which has contributed to the well-being of the nation. [ [http://www.raeng.org.uk/prizes/whittle/ The Royal Academy of Engineering website] Retrieved: 20 July 2008 ]
* Two roads in
Derbyare named Sir Frank Whittle Road and Sir Frank Whittle Way, as a tribute to his work at Rolls-Royce.
* Whittle Parkway in Burnham is named after him.
* One of the main buildings at the
Royal Air Force CollegeCranwell is called Whittle Hall. It houses the Officer & Aircrew Cadet Training Unit and the Air Power Studies Division of King's College London.
* Cambridge University Engineering Department has a Whittle Laboratory.
* A road in Rugby is named Whittle Close.
* Whittle Close in
Clitheroeis named after him.
* Sir Frank Whittle Way, a new road in Blackpool Business park, Blackpool.
* "The Jet"
public housein Leamington Spa, known as "The Jet and Whittle" until recent times, is named in honour of Whittle.
* The Whittle Gas field in the Southern North Sea operated by BP.Fact|date=December 2007
* "The Whittle Inn" near the
Gloster Aircraft Company's former test runway in Hucclecote, Gloucestershireis named after Whittle; the nearby Tescohas a picture of a Gloster Meteorincorporated in part of its glass frontage.
* The bar/restaurant in
Royal Mail's management college at Coton House, Churchoveris named the "Whittle Bar".
Timeline of jet power
* Frank Whittle (1953). "Jet: The story of a pioneer". Frederick Muller Ltd.
* Frank Whittle (1981). "Gas turbine aero-thermodynamics: with special reference to aircraft propulsion". Pergamon.
* John Golley (1997). "Genesis of the Jet: Frank Whittle and the Invention of the Jet Engine". Crowood Press. ISBN 1-85310-860-X.
* David S Brooks (1997). "Vikings at Waterloo: Wartime Work on the Whittle Jet Engine by the Rover Company". Rolls-Royce Heritage Trust. ISBN 1-872922-08-2
* Andrew Nahum (2004). "Frank Whittle: Invention of the Jet". Icon Books Ltd. ISBN 1-84046-538-7
* [http://www.admin.cam.ac.uk/news/press/dpp/2004010801 News report - Memorial for University of Cambridge Student who Invented The Jet Engine]
* [http://www-g.eng.cam.ac.uk/125/achievements/whittle/telgraph.htm More about Frank Whittle] .
* [http://www.raf.mod.uk/history_old/whittle1.html More about Frank Whittle and the jet age at the 'Royal Air Force History' website]
NAME= Whittle, Frank
SHORT DESCRIPTION= RAF officer, Jet engine pioneer
DATE OF BIRTH=
1 June 1907
PLACE OF BIRTH= Earlsdon,
DATE OF DEATH=
9 August 1996
PLACE OF DEATH=
Columbia, Maryland. United States
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Frank Whittle — Naissance 1er juin 1907 Coventry Décès 9 … Wikipédia en Français
Frank Whittle — Sir Frank Whittle KBE (* 1. Juni 1907 in Coventry; † 9. August 1996 in Columbia, Maryland) war ein englischer Pilot, Erfinder und Geschäftsmann. Seine größte Leistung war die Erfindung des Strahltriebwerks, das er unabhängig und zeit … Deutsch Wikipedia
Frank Whittle — Saltar a navegación, búsqueda Imagen de Frank Whittle Frank Whittle (1/06/1907 9/08/1996) fue un ingeniero aeronáutico y militar británico de la Royal Air Force. Comparte con el alemán Hans von Ohain, investigando de forma separada, el invento… … Wikipedia Español
Frank Whittle — noun English aeronautical engineer who invented the jet aircraft engine (1907 1996) • Syn: ↑Whittle, ↑Sir Frank Whittle • Instance Hypernyms: ↑aeronautical engineer * * * Frank Whittle [ … Useful english dictionary
Frank Whittle — ➡ Whittle * * * … Universalium
Sir Frank Whittle Medal — The Sir Frank Whittle Medal is awarded annually by the Royal Academy of Engineering to an engineer, [cite web title = The Sir Frank Whittle Medal web page work = The Royal Academy of Engineering web page publisher = date = 2006 url =… … Wikipedia
Sir Frank Whittle — noun English aeronautical engineer who invented the jet aircraft engine (1907 1996) • Syn: ↑Whittle, ↑Frank Whittle • Instance Hypernyms: ↑aeronautical engineer … Useful english dictionary
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