Knowledge (XXG)

Bristol Proteus

Source πŸ“

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powerplant anti-icing system could deal with severe icing conditions of the type considered likely in parts of the world where the Britannia would operate. However, during route-proving flights in Africa in April 1956 a different type of icing was encountered for which the anti-icing systems were ineffective. Modifications were made that were effective against this second type of icing. BOAC started services in February 1957 but later in the year a third type of icing was encountered on flights to Australia. When flying in icing conditions for prolonged periods the accumulation of ice on the surfaces of the reverse-flow air intake – inherited from the original intended Brabazon II and Princess installation – and subsequent shedding through the engine caused flame-outs. The engine would auto-relight with a long tongue of flame from the jetpipe which was of concern to the passengers. Although the problem was not inherently dangerous, it was avoided with restrictions in the flight manual (it could be avoided by not flying in cloud above a certain height). Modifications for the third type were successfully tested in icing conditions encountered during flights from Singapore in April 1958. BOAC, the launch customer for the Britannia, were unyielding in their demands for rectification, and attempted to maximise the extent of the problem in public, damaging sales prospects of the Britannia and delaying the aircraft's entry into service by two years, as well as almost bankrupting Bristol Aircraft.
316: 202: 585: 418: 42: 186:: "You know, Stanley, when we designed the Proteus I decided we should make the engine with the lowest fuel consumption in the world, regardless of its weight and bulk. So far, we have achieved the weight and bulk!" The redesigned Proteus 3 (700 series) gave 3,780 shp and weighed nearly 1,000 lb less than the previous design. It came too late for the first prototype Britannia and 219:
In 1954 a potentially troublesome design feature in the propeller gearbox, straight-cut gears, finally made itself known during a flight carrying a delegation from the Dutch airline KLM, a potential customer. A gearwheel stripped its teeth and the resulting damage set fire to the aircraft which made
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Another use of the Proteus was for remote power generation in the South West of England in what were called "Pocket Power Stations". The regional electricity board installed several 2.7 MW remote operated generation sets for peak load powered by the Proteus. Designed to run for ten years many
228:, Hooker's former boss, sent Rolls-Royce engineers to assist the Bristol team. This unasked-for generosity to what was, after all, a commercial competitor thawed the cold relationship that had existed between Hives and Hooker since Hooker's departure from Rolls-Royce concerning development of the 177:
The Proteus 2 (Mk.600 series) was supposed to produce 3,200 shp and weigh 3,050 lb. It was overweight and underpowered, weighing 3,800 lb producing 2,500 shp, and plagued with mechanical problems with virtually every part including compressor blades, turbine blades and bearings which failed at
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Developing an anti-icing system for the engine intake turned out to be a lengthy exercise. It had to be able to deal with the type of icing considered likely to cause problems to Britannias. Icing tests on a Proteus installation in an Ambassador aircraft in Canada showed that the engine and
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The Mk.705 of 3,900 hp (2,900 kW) was the first version used the Bristol Britannia 100 and some 300 series aircraft. The Mk.755 of 4,120 hp (3,070 kW) was used on the 200 series (not built) and other 300s, and the Mk.765 of 4,445 hp (3,315 kW) was used on the
174:, performance was poor and the first centrifugal compressor stage was removed. The first Proteus, the Proteus 1, also ran with the original compressor, as first tested in the Phoebus, but by 1950 had been redesigned as the Proteus 2 with only a single centrifugal stage. 571:. In this installation four "Marine Proteus" engines were clustered in the rear of the craft, exhausts pointed rearward. The engines drove horizontal power shafts that delivered power to one of four "pylons" positioned at the corners of the boat. At the pylons, 575:
used the horizontal torque to power a vertical shaft, with a lift fan at the bottom and propeller at the top. The two at the front required long shafts running above the passenger cabin, as all four engines were mounted at the rear of the craft.
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that delivered just over 4,000 hp (3,000 kW). The Proteus was a reverse-flow gas turbine. Because the second turbine drove no compressor stages, but only the propeller, this engine was classified as a
198:, but this project was cancelled. Only three Princesses were built, only one of which flew, and by the time the second Britannia was ready for testing the Proteus 3 was installed. 190:
flying-boat though. Eight engines on the Princess were mounted in four pairs with each pair driving two propellers through a gearbox in opposite directions. They were known as
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The Proteus was to power a very large airliner for use after the war. Design work started in September 1944 with its free turbine and propeller gearbox based on the earlier
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to speed development of the engine by not hindering it with gearbox problems. It was test-flown in May 1946 fitted to the bomb bay of an
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A specially modified Proteus 705 with drive shafts at front and rear of the engine to drive front and rear differential gearboxes on
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Twin Proteus 600 series engines driving contra-rotating propellers through a combining gearbox, developed specifically for the
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Turbojet History And Development 1930–1960 Volume 1 Great Britain and Germany, Anthony L. Kay, The Crowood Press Ltd. 2007,
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Not Much of an Engineer, An Autobiography, Sir Stanley Hooker assisted by Bill Gunston, Airlife Publishing 2002,
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https://www.flightglobal.com/pdfarchive/view/1958/1958%20-%200437.html?search=april%20chasing%20gremlin
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https://www.flightglobal.com/pdfarchive/view/1958/1958%20-%200436.html?search=april%20chasing%20gremlin
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allocated the Proteus a designation which was apparently little used. Officially the Proteus was named
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fast patrol boats, and subsequently in many fast patrol boats of similar design built for export by
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frequent intervals even at low power levels. This led to the famous quote of Proteus Chief Engineer
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engine. The compressor had 12 axial and 2 centrifugal stages. The gas generator was built as a
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Meteor Eject! Adventures of a cold-war fighter pilot, Nick Carter 2000, Woodfield Publishing,
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Twin Proteus 710 engines driving contra-rotating propellers for the Bristol Brabazon I Mk.II.
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Proteus, and later the Rolls-Royce Proteus. The Proteus was to have been superseded by the
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Military engines similar to the Proteus 765, to power the Bristol 253 Britannia C.Mk.1.
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an emergency landing on the mud in the river Severn estuary. Hearing of this failure,
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and electrical generating sets. It was also used to power a land-speed record car, the
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Marinised Proteus engines have been used to power ships and hovercraft such as the
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which would have given a Britannia a 75% increase in power for cruising faster.
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were still in use forty years later. A working example is preserved at the
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Used for industrial applications such as power generation, notably by the
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The engines slated for use in the Coupled-Proteus installations of the
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The fully developed initial version, renamed as the Proteus 700 series.
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https://www.flightglobal.com/pdfarchive/view/1957/1957%20-%201600.html
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https://www.flightglobal.com/pdfarchive/view/1955/1955%20-%200547.html
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Initial production versions, renamed as Proteus 600 series engines.
1302:, A sectional view of Proteus 755 turboprop, showing gasflow paths 583: 558: 440: 422: 416: 314: 200: 319:
Donald Campbell's Bluebird CN7 (powered by a Bristol Proteus 705)
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As with most gas turbine engines of the 1940s, 50s, and 60s the
1329: 1223:. South Western Electricity Historical Society. Archived from 1035:. South Western Electricity Historical Society. Archived from 302:
The engines used in the Coupled-Proteus installations for the
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Initial production engines renamed from Proteus series 2.
1175:. London: Conway Maritime Press Ltd. pp. 210–235. 1010:. London: Conway Maritime Press Ltd. pp. 210–235. 1270:. London: Samson Low, Marston & Company, Ltd 1951. 1193:. Cambridge, England. Patrick Stephens Limited, 1989. 941:"World Encyclopedia of Aero Engines – 5th edition" by 542:
and her sisters were also powered by the Proteus. The
1292:"Advert by Bristol for the Proteus 755 and Britannia" 596:. Turbine itself is within the sound enclosure beyond 1699: 1666: 1642: 1594: 1536: 1518: 1467: 1403: 1384: 1370: 694:. (early models had a single-stage power turbine) 1341: 1166:. London: Sampson, Low, Marston & Co Ltd. 986:. London: Sampson, Low, Marston & Co Ltd. 977: 975: 973: 971: 8: 969: 967: 965: 963: 961: 959: 957: 955: 953: 951: 690:Two-stage gas generator turbine, two-stage 1533: 1381: 1348: 1334: 1326: 1268:Jane's All The World's Aircraft 1951–1952 1162:Taylor, John W.R. FRHistS. ARAeS (1962). 1058:"BHC/Saunders Roe SRN4 Mountbatten Class" 1001: 999: 997: 995: 993: 982:Taylor, John W.R. FRHistS. ARAeS (1962). 182:to Chief Engineer of the Engine Division 1164:Jane's All the World's Aircraft 1962–63 984:Jane's All the World's Aircraft 1962–63 830: 27:1940s British turboprop aircraft engine 31: 1173:Saunders and Saro Aircraft since 1917 1008:Saunders and Saro Aircraft since 1917 521:Proteus engine was used to power the 7: 1247:, Flightglobal archive, 9 April 1954 332:The engine used among others in the 727:) residual thrust giving 3,780 eshp 135:. After the merger of Bristol with 1191:World Encyclopedia of Aero Engines 25: 1155:"Pocket Power Station wins award" 1120:"Pocket Power Station wins award" 495:Bristol Type 167 Brabazon I Mk.II 40: 1083:Internal Fire - Museum of Power 945:, Sutton Publishing, 2006, p.36 609:Specifications (Proteus Mk.705) 603:Internal Fire - Museum of Power 454:South Western Electricity Board 336:land speed record-breaking car. 1221:"SWEB's Pocket Power Stations" 1157:. BBC Mid Wales. 11 June 2010. 1122:. BBC Mid Wales. 11 June 2010. 1078:"SWEB's Pocket Power Stations" 1033:"SWEB's Pocket Power Stations" 1: 1748:Mixed-compressor gas turbines 510:After testing on the frigate 1386:Horizontally opposed engines 1281:SWEB's Pocket Power Stations 1207:. Airlife Publishing, 1985. 557:The Proteus was used on the 548:Sparviero-class patrol boats 437:Brave-class fast patrol boat 127:, small naval patrol craft, 748:273 imp gal/hr (1,241 L/hr) 405:Saunders-Roe SR.45 Princess 1764: 550:used a Proteus to drive a 49:Preserved Bristol Proteus 1372:Bristol Aeroplane Company 753:Specific fuel consumption 48: 39: 34: 1743:Bristol aircraft engines 1067:, James' Hovercraft Site 814:List of aircraft engines 18:Bristol-Siddeley Proteus 1738:1940s turboprop engines 1266:Bridgman, Leonard, ed. 1205:Not Much of an Engineer 1139:Retrieved: 28 July 2009 1133:Flightglobal archive – 668:, followed by a single 623:General characteristics 588:Generator of a Proteus 107:'s first mass-produced 1322:article on the Proteus 1306:"Power for the Giants" 1171:London, Peter (1988). 1106:A History of the World 1102:"Pocket Power Station" 1063:7 January 2010 at the 1006:London, Peter (1988). 732:Overall pressure ratio 597: 428: 344:Bristol Brabazon Mk.II 320: 216: 151:Design and development 139:the engine became the 105:Bristol Engine Company 1203:Hooker, Sir Stanley. 762:Power-to-weight ratio 713:Maximum power output: 587: 580:Pocket Power Stations 500:Saunders-Roe Princess 458:Pocket Power Stations 420: 318: 304:Saunders-Roe Princess 258:Bristol BPr.n Proteus 244:Series 250 aircraft. 204: 188:Saunders-Roe Princess 92:Saunders-Roe Princess 1227:on 24 September 2015 1039:on 24 September 2015 865:Hooker, 1985, p.128. 594:Internal Fire Museum 590:Pocket Power Station 472:Bluebird-Proteus CN7 334:Bluebird-Proteus CN7 133:Bluebird-Proteus CN7 1300:. 19 February 1954. 1286:Bristol Engine data 1241:"Aero Engines 1954" 1090:on 18 January 2009. 723:) + 1,200 lb (5.33 410:Coupled-Proteus 710 400:Coupled-Proteus 610 209:Britannia Model 102 776:Comparable engines 692:free power turbine 651:2,850 lb (1293 kg) 645:39.5 in (1,003 mm) 598: 506:Other applications 449:Industrial Proteus 429: 321: 254:Ministry of Supply 217: 213:Manchester Airport 137:Armstrong Siddeley 83:Major applications 1725: 1724: 1695: 1694: 1514: 1513: 1316:"Bristol Proteus" 854:978 1 86126 912 6 746:Fuel consumption: 742:44 lb/s (20 kg/s) 701:Aviation kerosene 639:113 in (2,870 mm) 490:Bristol Britannia 206:Britannia Airways 163:, and called the 122:Bristol Britannia 120:. 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1364:aero engines 1319: 1309: 1295: 1267: 1249:, retrieved 1244: 1229:. Retrieved 1225:the original 1219:Gale, John. 1204: 1190: 1172: 1163: 1147:Bibliography 1137:9 April 1954 1134: 1128: 1114: 1105: 1096: 1088:the original 1081: 1072: 1053: 1041:. Retrieved 1037:the original 1031:Gale, John. 1026: 1007: 983: 943:Bill Gunston 937: 926: 909: 898: 887: 870: 861: 844: 833: 807: 806: 797:Napier Eland 792:Lycoming T55 775: 774: 766:1.165 shp/lb 760: 751: 745: 739: 730: 712: 697: 684: 681:Reverse-flow 675: 661: 648: 642: 636: 628: 616: 613: 612: 599: 589: 561: 556: 544:Italian Navy 538: 527: 513: 509: 479:Applications 306:flying boat. 270:Avro Lincoln 257: 251: 238: 234: 218: 191: 176: 172:Avro Lincoln 164: 154: 118:free-turbine 100: 98: 29: 1600:Turboshafts 1530:(1959-1966) 1523:gas turbine 1378:(1920-1956) 1231:25 February 1043:25 February 882:, p.132-134 782:Allison T56 707:Performance 670:centrifugal 662:Compressor: 649:Dry weight: 562:Mountbatten 389:Proteus 765 384:Proteus 762 379:Proteus 761 374:Proteus 760 369:Proteus 758 364:Proteus 757 359:Proteus 756 354:Proteus 755 349:Proteus 750 339:Proteus 710 329:Proteus 705 324:Proteus 700 309:Proteus 625 299:Proteus 610 293:Proteus 600 226:Rolls-Royce 180:Frank Owner 109:gas turbine 1732:Categories 1707:Roy Fedden 1596:Turboprops 820:References 698:Fuel type: 677:Combustors 656:Components 569:hovercraft 523:Royal Navy 444:hovercraft 426:hovercraft 222:Lord Hives 129:hovercraft 74:First run 1700:Designers 1542:Turbofans 1538:Turbojets 1486:Centaurus 643:Diameter: 632:Turboprop 614:Data from 573:gearboxes 519:marinised 346:airliner. 232:in 1948. 113:turboprop 58:Turboprop 1560:variants 1491:Hercules 1061:Archived 771:See also 552:pump jet 484:Aircraft 439:and the 248:Variants 161:turbojet 125:airliner 103:was the 35:Proteus 1687:Stentor 1644:Ramjets 1634:Theseus 1629:Proteus 1581:Phoebus 1571:Pegasus 1566:Orpheus 1558: ( 1556:Olympus 1501:Perseus 1454:Phoenix 1449:Pegasus 1439:Neptune 1434:Mercury 1429:Lucifer 1424:Jupiter 1357:Bristol 1318:a 1949 1312:article 1308:a 1948 1251:28 July 921:, p.218 719:(2,475 686:Turbine 637:Length: 592:at the 566:Channel 514:Exmouth 215:in 1965 1677:BS.605 1619:Nimbus 1609:BS.360 1576:BS.100 1506:Taurus 1481:Aquila 1395:Cherub 1320:Flight 1310:Flight 1297:Flight 1245:Flight 1211:  1197:  1179:  1135:Flight 1108:. BBC. 1014:  917:  878:  856:,p.141 852:  715:3,320 617:Flight 534:Vosper 530:-class 1682:Gamma 1624:Orion 1586:Viper 1496:Orion 1459:Titan 1444:Orion 1419:Hydra 1414:Draco 825:Notes 736:7.2:1 672:stage 666:axial 629:Type: 559:SR.N4 539:Spica 528:Brave 441:SR.N4 423:SR.N4 54:Type 1658:Odin 1653:Thor 1526:and 1253:2009 1233:2013 1209:ISBN 1195:ISBN 1177:ISBN 1045:2013 1012:ISBN 915:ISBN 876:ISBN 850:ISBN 512:HMS 230:Avon 99:The 717:shp 525:'s 470:'s 456:in 242:RAF 224:of 211:at 1734:: 1598:/ 1540:/ 1359:/ 1294:. 1243:, 1104:. 1080:. 992:^ 950:^ 725:kN 721:kW 517:a 90:, 1670:: 1646:: 1602:: 1562:) 1544:: 1474:: 1407:: 1388:: 1349:e 1342:t 1335:v 1235:. 1215:. 1185:. 1047:. 1020:. 764:: 755:: 734:: 688:: 679:: 619:. 474:. 446:. 407:. 168:, 20:)

Index

Bristol-Siddeley Proteus

Turboprop
Bristol Siddeley
Bristol Britannia
Saunders-Roe Princess
Bristol Engine Company
gas turbine
turboprop
free-turbine
Bristol Britannia
airliner
hovercraft
Bluebird-Proteus CN7
Armstrong Siddeley
Bristol Siddeley
Bristol Orion
Bristol Theseus
turbojet
Bristol Phoebus
Avro Lincoln
Frank Owner
Stanley Hooker
Saunders-Roe Princess
Bristol Brabazon

Britannia Airways
Britannia Model 102
Manchester Airport
Lord Hives

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