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Rolls-Royce Olympus

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436:, being further developed through several subsequent versions to eventually provide reliable airline service. The Olympus 593 is a prime example of "propulsion and airframe integration". To optimise the performance of the engine when used at speeds from takeoff up to Mach 2 on Concorde, a variable intake and a variable throat nozzle with thrust reversing system were developed. Looking ahead to future supersonic transports, due to noise limits for supersonic transport category airplanes, studies were conducted on ejector suppressors, leading to the conclusion that "a new, low bypass ratio version of the 593 could be suitable for future generations of supersonic transport aircraft". 320: 351:
supervising the first test run and displaying the confidence he had in the design, slammed the throttle to give a surge-free acceleration to maximum power. The thrustmeter showed 10,000 lbf (44 kN). The next development was the BOl.1/2 which produced 9,500 lbf (42 kN) thrust in December 1950. Examples of the similar BOl.1/2A were constructed for US manufacturer Curtiss-Wright which had bought a licence for developing the engine as the TJ-32 or J67 for the projected
303:. This two-spool design eliminated the need for features such as variable inlet guide vanes (Avon, J79), inlet ramps (J65), variable stators (J79) or compressor bleed (Avon) which were required on single spool compressors with pressure ratios above about 6:1. Without these features an engine could not be started nor run at low speeds without destructive blade vibrations. Nor could they accelerate to high speeds with fast acceleration times (" 31: 311:. The design was progressively modified and the centrifugal HP compressor was replaced by an axial HP compressor. This reduced the diameter of the new engine to the design specification of 40 in (100 cm). The Bristol Type 172 was cancelled though development continued for the Avro Vulcan and other projects. 371:
of 63,668 ft (19,406 m). Fitted with more powerful Mk 102 engines, the Canberra increased the record to 65,876 ft (20,079 m) in August 1955. The first production Olympus, the Mk 101, entered service in late 1952 at a rated thrust of 11,000 lb, a weight of 3,650 lb, and with a
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The BOl.1 first ran on 16 May 1950 and was designed to produce 9,140 lbf (40.7 kN) thrust and to be free from destructive rotating stall on start up to idle speed and to be free from surging on fast accelerations to maximum thrust. The engine started without a problem and Hooker,
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The first engine, its development designation being BOl.1 (Bristol Olympus 1), had six LP compressor stages and eight HP stages, each driven by a single-stage turbine. The combustion system was novel in that ten connected flame tubes were housed within a
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The thrust required of the new engine, then designated B.E.10 (later Olympus), would initially be 9,000 lbf (40 kN) with growth potential to 12,000 lbf (53 kN). The
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Avro Vulcan Phase 6 (B3): BOl.23, a development of the Mk 301. Different engine configurations, BOl.21, BOl.21/2 and BOl.23, with either reheat or an
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in the US as the TJ-32 or J67 (military designation) and the TJ-38 'Zephyr', although none saw use. The Olympus was also developed with success as
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system. Separate combustion cans would have exceeded the diameter beyond the design limit, and a true annular system was considered too advanced.
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The Olympus was developed extensively throughout its production run, and the many variants can be described as belonging to four main groups.
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and was to be powered by four or six Bristol engines of 9,000 lbf (40 kN) thrust to the Ministry engine specification TE.1/46.
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which first flew with these engines derated to 8,000 lbf (36 kN) thrust in August 1952. In May 1953, this aircraft reached a
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The engine was by now ready for air testing and the first flight engines, designated Olympus Mk 99, were fitted into a
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Preserved Bristol Siddeley Olympus Mk 301 Engine Change Unit (ECU) complete with ancillaries and bulkheads.
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and continued development funding. The engine first ran in 1950 and quickly outperformed its design goals.
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Bristol T198: Mk 591. Early supersonic airliner design (132 seats). The engine was a civilianised BOl.22R.
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Further derivatives of the Olympus were produced for ship propulsion and land-based power generation.
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At the end of World War II, the Bristol Engine Company's major effort was the development of the
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http://webserver.dmt.upm.es/zope/DMT/Members/jmtizon/turbomaquinas/NASA-SP36_extracto.pdf
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would be an unheard of 9:1. To achieve this, the initial design used a low-pressure (LP)
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The first reheat variant, the Bristol Siddeley Olympus Mk 320, powered the cancelled
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Avro 718: BOl.3 The Type 718 was a military transport aircraft with up to 110 seats.
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Over the years, the Olympus was proposed for numerous other applications including:
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for a jet-powered bomber, powered by four new engines which would be supplied by
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aircraft engine design, first run in May 1950 and preceded only by the
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in 1966. Through this period the engine was further developed as the
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https://www.ecfr.gov/current/title-14/chapter-I/subchapter-C/part-36
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Avro 739 to OR339 (the requirement that culminated in TSR2): BOl.21R
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Advanced Olympus for Next Generation Supersonic Transport Aircraft
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Advanced Olympus for Next Generation Supersonic Transport Aircraft
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company tested a license-developed version known as the J67 and a
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Collection (Derby - UK) Mk 101 and Mk 593 and a Marine version.
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engines. By the end of 1946, the company had only 10 hours of
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submitted a proposal for a medium-range bomber to the same
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design to OR339: BOl.14R, BOl.15R. Developed from BOl.6R.
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was appointed as Chief Engineer of Bristol Aero Engines.
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Joe Baugher's Encyclopedia of American Military Aircraft
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Engines Limited (BSEL), which in turn was taken over by
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experience with a small experimental engine called the
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designated TJ-38 Zephyr. Neither design was produced.
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Bristol T204 to OR339: BOl.22SR (simplified reheat)
179:Initially used in the Vulcan, later versions added 1486:Articles and topics related to Rolls-Royce Olympus 475: 4148: 160:The design dates to a November 1946 proposal by 1406:Barnsley, UK: Pen % Sword Aviation, 2012, 1364:. Derby, UK: Rolls-Royce Heritage Trust, 1990. 1309:, 4 December 1999. Retrieved: 16 February 2011. 658: 432:, this was developed during the 1960s into the 264:then in development. In early 1947, the parent 1420:. Marlsborough, UK: Airlife Publishing, 2002. 3176: 2736: 1911: 1509: 1392:. Bishop-Auckland, UK: Pentland Books, 2001. 1271: 1269: 1267: 1265: 1263: 1261: 1259: 1257: 1255: 1253: 1251: 1249: 1247: 1245: 1243: 1241: 1239: 1237: 1235: 1233: 1231: 1229: 1227: 1225: 299:, each being driven by its own single-stage 1171: 1169: 1167: 1165: 1027: 1025: 646:Museum of Science and Industry (Manchester) 16:Supersonic turbojet engine with afterburner 3183: 3169: 2743: 2729: 1918: 1904: 1516: 1502: 704:127.1 in (10.59 ft; 3.23 m) 689: 417:. These engines were further developed by 1222: 1147: 893:. Gatwick Aviation Museum. Archived from 869:"The Rolls-Royce Olympus Aircraft Engine" 549:Handley Page HP98: Pathfinder variant of 4162:Rolls-Royce aircraft gas turbine engines 1162: 1022: 318: 206:Versions of the engine were licensed to 1390:The Vulcan B.Mk2 from a Different Angle 578:Martin/General Dynamics RB-57F Canberra 405:variants were designed and produced by 4149: 1201:: CS1 maint: archived copy as title ( 950:: CS1 maint: archived copy as title ( 314: 3164: 2724: 1899: 1497: 1484: 1138: 1111: 779:0.817 lb/(lbf⋅h) (23.1 g/(kN⋅s)) 614: 610:: Development of Mk 555 with aft fan. 1099:"Supersonic Transport (SST) Engines" 710:40 in (3.3 ft; 1.0 m) 1296: 332:system: a hybrid of separate flame 187:. Bristol Aero Engines merged with 77:Rolls-Royce Bristol Engine Division 13: 594:: BOl.21 for possible sale to RAF. 323:Gas-flow diagram of Olympus Mk 101 14: 4178: 4157:Bristol Siddeley aircraft engines 1477:: YouTube Playlist from AgentJayZ 1432: 1378:. London, UK: Grub Street, 2009. 1293:Addendum to Avro Brochure IPB 104 1323:A36 - SAABs atombombare avslöjad 747:HP single stage, LP single stage 428:supersonic strike aircraft. For 73:Bristol Siddeley Engines Limited 29: 1362:Olympus – the first forty years 1332: 1312: 1287: 1213: 1132: 1120: 1105: 1091: 1082: 1073: 1064: 1051: 1034: 1013: 652:South Yorkshire Aircraft Museum 580:: Mk 701 developed from Mk 301. 574:Hawker P.1129 to OR339: BOl.15R 453: 2358:Rolls-Royce Barnoldswick (RB) 1446:image of Olympus power station 1061:, Sutton Publishing, 2006, p36 994: 985: 976: 967: 958: 918: 909: 883: 861: 815:Rolls-Royce/Snecma Olympus 593 757: 729:axial 6 LP stages, 8 HP stages 556:Handley Page Victor B1: Mk 104 476:Proposed aircraft applications 434:Rolls-Royce/Snecma Olympus 593 390:Rolls-Royce/Snecma Olympus 593 201:Rolls-Royce/Snecma Olympus 593 113:Rolls-Royce/Snecma Olympus 593 1: 844: 720: 716:3,615 lb (1,640 kg) 698:axial flow two-spool turbojet 635:Charlwood Surrey – Two Mk 320 280:. The Bristol design was the 221: 132:) was the world's second two- 3194:gas turbine aircraft engine 1554:Horizontally opposed engines 770:11,000 lbf (49 kN) 659:Specifications (Olympus 101) 386:Rolls-Royce Olympus variants 7: 2576:Aero-derivative industrial 792: 592:Republic F-105 Thunderchief 559:Handley Page Victor Phase 3 484:C104 which led to the C105 379: 10: 4183: 2712:Rolls-Royce Heritage Trust 1439:Rolls-Royce Heritage Trust 810:Rolls-Royce Marine Olympus 686:Bristol Aero Engine School 640:Rolls-Royce Heritage Trust 623:North, Manchester – Mk 101 394:Rolls-Royce Marine Olympus 383: 226: 183:for use in the supersonic 117:Rolls-Royce Marine Olympus 4105: 3848: 3504: 3202: 3135: 3108: 3075: 3045: 2970: 2895: 2888: 2829: 2765: 2704: 2633: 2605: 2584: 2575: 2357: 2300: 2198: 2104: 2081: 2041: 1945: 1936: 1867: 1834: 1810: 1762: 1704: 1686: 1635: 1571: 1552: 1540:Bristol Aeroplane Company 1538: 1491: 775:Specific fuel consumption 668:"The Operational Olympus" 413:and powered the subsonic 295:and a high-pressure (HP) 272:B.35/46 which led to the 266:Bristol Aeroplane Company 162:Bristol Aeroplane Company 37: 28: 23: 1404:The Avro Type 698 Vulcan 839:List of aircraft engines 343:In 1950, Dr (later Sir) 150:and later models in the 2042:By company designation: 1418:Not Much of an Engineer 1329:issue No. 4, April 1991 1321:quoting Berns, Lennart 1159:25 October 1957, p. 647 1079:Baxter 1990, pp. 22, 24 1019:Baxter 1990, pp. 16, 18 982:Baxter 1990, pp. 13, 18 827:Pratt & Whitney J75 738:cannular 10 flame tubes 690:General characteristics 633:Gatwick Aviation Museum 191:Motors in 1959 to form 144:Pratt & Whitney J57 4167:1950s turbojet engines 4107:Adaptive cycle engines 3192:United States military 973:Baxter 1990, pp. 10–13 804:Bristol Siddeley BS100 784:Thrust-to-weight ratio 583:Gloster P492/3: Mk 591 531:Bristol T205: Mark 551 324: 297:centrifugal compressor 130:Bristol B.E.10 Olympus 2597:Rolls-Royce Meteorite 891:"Rolls-Royce Olympus" 684:Lecture Notes, Vulcan 369:world record altitude 322: 2708:Rolls-Royce Holdings 2641:Alan Arnold Griffith 1452:Good image of Mk 301 1340:Historien om Viggen 1006:20 July 2018 at the 565:Handley Page Pacific 522:Bristol T201: Mk 551 510:Bristol T172: B.E.10 500:Avro 750: 2 x Mk 551 497:Avro 740: 3 x Mk 551 407:Bristol Aero Engines 166:Bristol Aero Engines 69:Bristol Aero Engines 2696:Spirito Mario Viale 1927:Rolls-Royce Limited 1284:Fildes 2012, p. 407 1275:Baxter 1990, p. 172 1219:Fildes 2012, p. 424 1139:Gupta, P.C (1980). 1112:Gupta, P.C (1980). 798:Related development 621:Imperial War Museum 419:Rolls-Royce Limited 315:Initial development 278:Handley Page Victor 126:Rolls-Royce Olympus 3196:designation system 2646:R.W. Harvey-Bailey 2592:Rolls-Royce Meteor 2578:and marine engines 1475:The Mighty Olympus 1465:"Olympian Heights" 1304:"Republic XF-103." 1088:Baxter 1990, p. 32 1070:Baxter 1990, p. 20 1031:Baxter 1990, p. 18 991:Baxter 1990, p. 13 964:Baxter 2012, p. 20 915:Baxter 2012, p. 16 821:Comparable engines 627:RAF Museum Cosford 615:Engines on display 562:Handley Page HP107 325: 189:Armstrong Siddeley 92:Major applications 4144: 4143: 4138: 4137: 3158: 3157: 3071: 3070: 2718: 2717: 2629: 2628: 2077: 2076: 1893: 1892: 1863: 1862: 1682: 1681: 1450:enginehistory.org 1426:978-1-85310-285-1 1416:Hooker, Stanley. 1412:978 1 84884 284 7 1402:Fildes, David W. 1384:978-1-906502-30-0 1376:Vulcan Test Pilot 1370:978-0-9511710-9-7 1319:Knowledge article 897:on 8 January 2017 871:. Air Power World 122: 121: 4174: 3185: 3178: 3171: 3162: 3161: 2897:Whirlwind family 2893: 2892: 2759:aircraft engines 2745: 2738: 2731: 2722: 2721: 2582: 2581: 2263:(as Turbo-Union) 2257:(with MAN Turbo) 2236:(with MAN Turbo) 2096:Rolls-Royce RZ.2 1973:Eagle XVI (X-16) 1943: 1942: 1920: 1913: 1906: 1897: 1896: 1702: 1701: 1688:Bristol Siddeley 1550: 1549: 1529:Bristol Siddeley 1518: 1511: 1504: 1495: 1494: 1482: 1481: 1388:Bullman, Craig. 1374:Blackman, Tony. 1347: 1336: 1330: 1316: 1310: 1300: 1294: 1291: 1285: 1282: 1276: 1273: 1220: 1217: 1211: 1206: 1200: 1192: 1190: 1188: 1179:. Archived from 1173: 1160: 1151: 1145: 1144: 1136: 1130: 1124: 1118: 1117: 1109: 1103: 1102: 1095: 1089: 1086: 1080: 1077: 1071: 1068: 1062: 1055: 1049: 1038: 1032: 1029: 1020: 1017: 1011: 1010:p.44 and fig.27a 998: 992: 989: 983: 980: 974: 971: 965: 962: 956: 955: 949: 941: 939: 937: 928:. Archived from 922: 916: 913: 907: 906: 904: 902: 887: 881: 880: 878: 876: 865: 681: 680:on 29 July 2013. 676:. Archived from 411:Bristol Siddeley 293:axial compressor 193:Bristol Siddeley 128:(originally the 109: 93: 55: 33: 21: 20: 4182: 4181: 4177: 4176: 4175: 4173: 4172: 4171: 4147: 4146: 4145: 4140: 4139: 4134: 4101: 3844: 3509: 3500: 3198: 3189: 3159: 3154: 3131: 3104: 3067: 3041: 2966: 2884: 2825: 2761: 2749: 2719: 2714: 2700: 2681:Arthur Rowledge 2625: 2601: 2585:Piston engines: 2577: 2571: 2359: 2353: 2296: 2194: 2100: 2073: 2037: 1932: 1924: 1894: 1889: 1859: 1830: 1806: 1782:Coupled Proteus 1758: 1693: 1678: 1631: 1567: 1542: 1534: 1522: 1487: 1444:Turbine Support 1435: 1430: 1351: 1350: 1337: 1333: 1317: 1313: 1301: 1297: 1292: 1288: 1283: 1279: 1274: 1223: 1218: 1214: 1207:Avro Type List 1194: 1193: 1186: 1184: 1183:on 3 March 2016 1177:"Archived copy" 1175: 1174: 1163: 1152: 1148: 1137: 1133: 1125: 1121: 1110: 1106: 1097: 1096: 1092: 1087: 1083: 1078: 1074: 1069: 1065: 1056: 1052: 1039: 1035: 1030: 1023: 1018: 1014: 1008:Wayback Machine 999: 995: 990: 986: 981: 977: 972: 968: 963: 959: 943: 942: 935: 933: 932:on 2 April 2015 926:"Archived copy" 924: 923: 919: 914: 910: 900: 898: 889: 888: 884: 874: 872: 867: 866: 862: 847: 795: 760: 723: 692: 666: 661: 617: 587:Republic XF-103 478: 456: 396: 384:Main articles: 382: 317: 257:or core of the 229: 224: 214:and industrial 115: 107: 99: 91: 75: 71: 54:National origin 53: 17: 12: 11: 5: 4180: 4170: 4169: 4164: 4159: 4142: 4141: 4136: 4135: 4133: 4132: 4127: 4122: 4117: 4111: 4109: 4103: 4102: 4100: 4099: 4094: 4089: 4084: 4079: 4074: 4069: 4064: 4059: 4053: 4052: 4047: 4042: 4037: 4032: 4027: 4022: 4017: 4012: 4007: 4002: 3997: 3992: 3987: 3982: 3977: 3972: 3967: 3962: 3957: 3952: 3947: 3942: 3937: 3932: 3927: 3922: 3917: 3912: 3907: 3901: 3900: 3895: 3890: 3885: 3880: 3875: 3870: 3865: 3860: 3854: 3852: 3846: 3845: 3843: 3842: 3837: 3832: 3827: 3822: 3817: 3812: 3807: 3802: 3797: 3791: 3790: 3785: 3780: 3775: 3770: 3764: 3763: 3758: 3752: 3751: 3746: 3741: 3736: 3731: 3726: 3721: 3716: 3711: 3706: 3701: 3696: 3691: 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family 2968: 2967: 2965: 2964: 2959: 2954: 2949: 2944: 2939: 2933: 2932: 2927: 2922: 2917: 2912: 2907: 2901: 2899: 2890: 2889:Wright radials 2886: 2885: 2883: 2882: 2877: 2872: 2867: 2862: 2857: 2852: 2847: 2842: 2836: 2834: 2827: 2826: 2824: 2823: 2818: 2813: 2808: 2803: 2798: 2793: 2788: 2783: 2778: 2772: 2770: 2768:inline engines 2763: 2762: 2748: 2747: 2740: 2733: 2725: 2716: 2715: 2705: 2702: 2701: 2699: 2698: 2693: 2688: 2683: 2678: 2673: 2668: 2666:Adrian Lombard 2663: 2658: 2656:Stanley Hooker 2653: 2648: 2643: 2637: 2635: 2631: 2630: 2627: 2626: 2624: 2623: 2618: 2616:Marine Olympus 2612: 2610: 2603: 2602: 2600: 2599: 2594: 2588: 2586: 2579: 2573: 2572: 2570: 2569: 2564: 2559: 2554: 2549: 2544: 2539: 2534: 2529: 2524: 2519: 2514: 2509: 2504: 2499: 2494: 2489: 2484: 2479: 2474: 2469: 2464: 2459: 2454: 2449: 2444: 2439: 2434: 2429: 2424: 2419: 2414: 2409: 2404: 2399: 2394: 2389: 2384: 2379: 2374: 2369: 2363: 2361: 2355: 2354: 2352: 2351: 2346: 2341: 2336: 2331: 2326: 2321: 2316: 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1661: 1656: 1651: 1645: 1643: 1640:radial engines 1633: 1632: 1630: 1629: 1624: 1619: 1614: 1609: 1604: 1599: 1594: 1589: 1584: 1578: 1576: 1573:Radial engines 1569: 1568: 1566: 1565: 1559: 1557: 1547: 1544:Piston engines 1536: 1535: 1521: 1520: 1513: 1506: 1498: 1492: 1489: 1488: 1479: 1478: 1472: 1462: 1453: 1447: 1441: 1434: 1433:External links 1431: 1429: 1428: 1414: 1400: 1386: 1372: 1360:Baxter, Alan. 1357: 1356: 1355: 1349: 1348: 1331: 1311: 1302:Baugher, Joe. 1295: 1286: 1277: 1221: 1212: 1161: 1146: 1131: 1119: 1104: 1090: 1081: 1072: 1063: 1050: 1033: 1021: 1012: 993: 984: 975: 966: 957: 917: 908: 882: 859: 858: 857: 856: 852: 851: 846: 843: 842: 841: 830: 829: 818: 817: 812: 807: 806:(Olympus core) 794: 791: 790: 789: 780: 771: 759: 756: 755: 754: 753:AVTUR or AVTAG 748: 739: 730: 722: 719: 718: 717: 711: 705: 699: 691: 688: 660: 657: 656: 655: 649: 643: 636: 630: 624: 616: 613: 612: 611: 605: 603:Saab 37 Viggen 600: 595: 589: 584: 581: 575: 572: 566: 563: 560: 557: 554: 547: 541: 535: 532: 529: 526: 523: 520: 517: 514: 511: 508: 501: 498: 495: 492: 489: 477: 474: 473: 472: 467: 462: 455: 452: 441:Curtiss-Wright 381: 378: 376:of 250 hours. 345:Stanley Hooker 316: 313: 289:pressure ratio 253:which was the 228: 225: 223: 220: 208:Curtiss-Wright 203:for Concorde. 120: 119: 110: 108:Developed into 104: 103: 94: 88: 87: 84: 80: 79: 66: 62: 61: 59:United Kingdom 56: 50: 49: 44: 40: 39: 35: 34: 26: 25: 15: 9: 6: 4: 3: 2: 4179: 4168: 4165: 4163: 4160: 4158: 4155: 4154: 4152: 4131: 4128: 4126: 4123: 4121: 4118: 4116: 4113: 4112: 4110: 4108: 4104: 4098: 4095: 4093: 4090: 4088: 4085: 4083: 4080: 4078: 4075: 4073: 4070: 4068: 4065: 4063: 4060: 4058: 4055: 4054: 4051: 4048: 4046: 4043: 4041: 4038: 4036: 4033: 4031: 4028: 4026: 4023: 4021: 4018: 4016: 4013: 4011: 4008: 4006: 4003: 4001: 3998: 3996: 3993: 3991: 3988: 3986: 3983: 3981: 3978: 3976: 3973: 3971: 3968: 3966: 3963: 3961: 3958: 3956: 3953: 3951: 3948: 3946: 3943: 3941: 3938: 3936: 3933: 3931: 3928: 3926: 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2604: 2598: 2595: 2593: 2590: 2589: 2587: 2583: 2580: 2574: 2568: 2565: 2563: 2560: 2558: 2555: 2553: 2550: 2548: 2545: 2543: 2540: 2538: 2535: 2533: 2530: 2528: 2525: 2523: 2520: 2518: 2515: 2513: 2510: 2508: 2505: 2503: 2500: 2498: 2495: 2493: 2490: 2488: 2485: 2483: 2480: 2478: 2475: 2473: 2470: 2468: 2465: 2463: 2460: 2458: 2455: 2453: 2450: 2448: 2445: 2443: 2440: 2438: 2435: 2433: 2430: 2428: 2425: 2423: 2420: 2418: 2415: 2413: 2410: 2408: 2405: 2403: 2400: 2398: 2395: 2393: 2390: 2388: 2385: 2383: 2380: 2378: 2375: 2373: 2370: 2368: 2365: 2364: 2362: 2356: 2350: 2347: 2345: 2342: 2340: 2337: 2335: 2332: 2330: 2327: 2325: 2322: 2320: 2317: 2315: 2312: 2311: 2309: 2307: 2303: 2299: 2293: 2292:Trent (RB203) 2290: 2288: 2285: 2283: 2280: 2278: 2275: 2273: 2270: 2268: 2265: 2262: 2259: 2256: 2253: 2251: 2248: 2246: 2243: 2241: 2238: 2235: 2232: 2230: 2227: 2225: 2222: 2220:(with SNECMA) 2219: 2216: 2214: 2211: 2209: 2206: 2205: 2203: 2201: 2197: 2191: 2188: 2186: 2183: 2181: 2178: 2176: 2173: 2171: 2168: 2166: 2163: 2161: 2158: 2156: 2153: 2151: 2148: 2146: 2143: 2141:(with SNECMA) 2140: 2137: 2134: 2130: 2127: 2125: 2122: 2120: 2117: 2115: 2112: 2111: 2109: 2107: 2103: 2097: 2094: 2092: 2089: 2088: 2086: 2084: 2080: 2070: 2067: 2065: 2062: 2060: 2057: 2055: 2052: 2050: 2047: 2046: 2044: 2040: 2034: 2031: 2029: 2026: 2024: 2021: 2019: 2016: 2014: 2011: 2009: 2006: 2004: 2001: 1999: 1996: 1994: 1991: 1989: 1986: 1984: 1981: 1979: 1976: 1974: 1971: 1969: 1966: 1964: 1961: 1959: 1956: 1954: 1951: 1950: 1948: 1944: 1941: 1939: 1935: 1931: 1928: 1921: 1916: 1914: 1909: 1907: 1902: 1901: 1898: 1886: 1883: 1881: 1878: 1876: 1873: 1872: 1870: 1866: 1856: 1853: 1851: 1848: 1846: 1843: 1842: 1840: 1837: 1833: 1827: 1824: 1822: 1819: 1818: 1816: 1813: 1809: 1803: 1800: 1798: 1795: 1793: 1790: 1788: 1785: 1783: 1780: 1778: 1775: 1774: 1772: 1769: 1765: 1761: 1755: 1752: 1750: 1747: 1745: 1742: 1740: 1737: 1735: 1732: 1729: 1725: 1722: 1720: 1717: 1716: 1714: 1711: 1707: 1703: 1700: 1697: 1692: 1689: 1685: 1675: 1672: 1670: 1667: 1665: 1662: 1660: 1657: 1655: 1652: 1650: 1647: 1646: 1644: 1641: 1638: 1634: 1628: 1625: 1623: 1620: 1618: 1615: 1613: 1610: 1608: 1605: 1603: 1600: 1598: 1595: 1593: 1590: 1588: 1585: 1583: 1580: 1579: 1577: 1574: 1570: 1564: 1561: 1560: 1558: 1555: 1551: 1548: 1545: 1541: 1537: 1533: 1530: 1526: 1519: 1514: 1512: 1507: 1505: 1500: 1499: 1496: 1490: 1483: 1476: 1473: 1470: 1466: 1463: 1460: 1458: 1454: 1451: 1448: 1445: 1442: 1440: 1437: 1436: 1427: 1423: 1419: 1415: 1413: 1409: 1405: 1401: 1399: 1398:1-85821-899-3 1395: 1391: 1387: 1385: 1381: 1377: 1373: 1371: 1367: 1363: 1359: 1358: 1353: 1352: 1345: 1342: 1339: 1335: 1328: 1324: 1320: 1315: 1308: 1305: 1299: 1290: 1281: 1272: 1270: 1268: 1266: 1264: 1262: 1260: 1258: 1256: 1254: 1252: 1250: 1248: 1246: 1244: 1242: 1240: 1238: 1236: 1234: 1232: 1230: 1228: 1226: 1216: 1210:Avro Heritage 1209: 1204: 1198: 1182: 1178: 1172: 1170: 1168: 1166: 1158: 1155: 1150: 1142: 1135: 1129:, para 36.301 1128: 1123: 1115: 1108: 1100: 1094: 1085: 1076: 1067: 1060: 1054: 1047: 1046:9780906393352 1043: 1037: 1028: 1026: 1016: 1009: 1005: 1002: 997: 988: 979: 970: 961: 953: 947: 931: 927: 921: 912: 896: 892: 886: 870: 864: 860: 854: 853: 849: 848: 840: 837: 836: 835: 834: 833:Related lists 828: 825: 824: 823: 822: 816: 813: 811: 808: 805: 802: 801: 800: 799: 787: 785: 781: 778: 776: 772: 769: 767: 762: 761: 752: 749: 746: 744: 740: 737: 735: 731: 728: 725: 724: 715: 712: 709: 706: 703: 700: 697: 694: 693: 687: 685: 679: 675: 674: 669: 665: 653: 650: 647: 644: 641: 637: 634: 631: 628: 625: 622: 619: 618: 609: 606: 604: 601: 599: 596: 593: 590: 588: 585: 582: 579: 576: 573: 570: 569:Hawker P.1121 567: 564: 561: 558: 555: 552: 548: 545: 542: 539: 536: 533: 530: 527: 524: 521: 518: 515: 512: 509: 506: 502: 499: 496: 493: 490: 487: 483: 482: 481: 471: 468: 466: 463: 461: 458: 457: 451: 448: 446: 442: 439:The American 437: 435: 431: 427: 422: 420: 416: 412: 408: 404: 399: 395: 391: 387: 377: 375: 370: 366: 365: 361: 356: 354: 348: 346: 341: 339: 335: 331: 321: 312: 310: 306: 302: 298: 294: 290: 285: 283: 279: 275: 271: 270:specification 267: 263: 260: 256: 255:gas generator 252: 248: 244: 241: 238: 234: 219: 217: 213: 209: 204: 202: 198: 194: 190: 186: 182: 177: 175: 171: 167: 163: 158: 156: 153: 149: 145: 141: 138: 135: 131: 127: 118: 114: 111: 106: 105: 102: 98: 95: 90: 89: 85: 82: 81: 78: 74: 70: 67: 65:Manufacturer 64: 63: 60: 57: 52: 51: 48: 45: 42: 41: 36: 32: 27: 22: 19: 3376: 2995:Twin Cyclone 2661:Gordon Lewis 2651:Ernest Hives 2607:Gas turbines 2360:designations 2128: 1978:Eagle (H-24) 1968:Eagle (V-12) 1930:aero engines 1885:Gordon Lewis 1723: 1719:Gyron Junior 1637:Sleeve valve 1532:aero engines 1468: 1456: 1417: 1403: 1389: 1375: 1361: 1354:Bibliography 1343: 1334: 1326: 1322: 1314: 1306: 1298: 1289: 1280: 1215: 1185:. Retrieved 1181:the original 1156: 1149: 1140: 1134: 1122: 1113: 1107: 1093: 1084: 1075: 1066: 1059:Bill Gunston 1053: 1036: 1015: 996: 987: 978: 969: 960: 934:. Retrieved 930:the original 920: 911: 901:13 September 899:. Retrieved 895:the original 885: 875:13 September 873:. Retrieved 863: 832: 831: 820: 819: 797: 796: 782: 773: 763: 750: 741: 732: 726: 713: 707: 701: 695: 683: 678:the original 671: 663: 662: 608:Vickers VC10 544:de Havilland 538:Bristol T223 534:Bristol T213 525:Bristol T202 516:Bristol T180 513:Bristol T177 479: 454:Applications 449: 438: 423: 400: 397: 362: 357: 349: 342: 326: 286: 230: 216:gas turbines 205: 178: 174:Air Ministry 159: 129: 125: 123: 18: 3511:Turboshafts 3114:turboshafts 2801:T-4 Tornado 2796:T-3 Tornado 2791:T-2 Tornado 2786:T-1 Tornado 2781:Gipsy L-320 2686:Henry Royce 2621:Marine Spey 2306:Turboshafts 2139:Olympus 593 1768:Turboshafts 1698:(1959-1966) 1691:gas turbine 1546:(1920-1956) 1461:of BOl.1/2A 758:Performance 727:Compressor: 714:Dry weight: 460:Avro Vulcan 415:Avro Vulcan 336:and a true 307:") without 274:Avro Vulcan 197:Rolls-Royce 148:Avro Vulcan 97:Avro Vulcan 4151:Categories 3825:LHTEC T800 3506:Turboprops 3110:Turboprops 3005:Cyclone 22 2302:Turboprops 1875:Roy Fedden 1764:Turboprops 1187:28 October 845:References 751:Fuel type: 734:Combustors 721:Components 486:Avro Arrow 403:non-reheat 222:Background 137:axial-flow 83:First run 3850:Turbofans 3204:Turbojets 3077:Turbojets 2985:Cyclone 9 2980:Cyclone 7 2830:Lawrance 2706:See also 2634:Designers 2200:Turbofans 2106:Turbojets 2023:Peregrine 1868:Designers 1710:Turbofans 1706:Turbojets 1654:Centaurus 1346:2005 No 4 1327:Flygrevyn 855:Citations 708:Diameter: 664:Data from 571:: BOl.21R 465:BAC TSR-2 445:turboprop 426:BAC TSR-2 262:turboprop 237:Centaurus 185:BAC TSR-2 170:V bombers 101:BAC TSR-2 3830:APW T800 3648:variants 3053:L-3 Gale 2756:Lawrance 2477:RB168-62 2240:RB168-62 2133:variants 1946:By name: 1728:variants 1659:Hercules 1197:cite web 1004:Archived 946:cite web 936:22 March 793:See also 764:Maximum 629:– Mk 320 488:: BOl.3" 470:Concorde 430:Concorde 401:Initial 380:Variants 360:Canberra 330:cannular 305:spool up 282:Type 172 247:turbojet 233:Hercules 152:Concorde 140:turbojet 47:Turbojet 24:Olympus 3646: ( 3137:Ramjets 2990:Cyclone 2832:radials 2816:IV-1560 2811:IV-1460 2766:Wright 2229:Pegasus 2190:Welland 2131: ( 2129:Olympus 2119:Derwent 2033:Vulture 2018:Pennine 2008:Kestrel 1998:Griffon 1993:Goshawk 1953:Buzzard 1855:Stentor 1812:Ramjets 1802:Theseus 1797:Proteus 1749:Phoebus 1739:Pegasus 1734:Orpheus 1726: ( 1724:Olympus 1669:Perseus 1622:Phoenix 1617:Pegasus 1607:Neptune 1602:Mercury 1597:Lucifer 1592:Jupiter 1525:Bristol 1471:article 1459:cutaway 1048:, p.142 743:Turbine 702:Length: 598:Saab 36 505:aft fan 338:annular 301:turbine 259:Proteus 251:Phoebus 227:Origins 3058:R-1200 3046:Others 3037:R-4090 3032:R-3350 3027:R-2600 3022:R-1820 3017:R-1750 3012:R-1300 2962:R-1670 2957:R-1510 2821:V-1950 2752:Wright 2522:RB.193 2462:RB.162 2334:Nimbus 2255:RB.193 2245:RB.175 2224:Medway 2213:Conway 2180:Thames 2160:RB.162 2155:RB.145 2150:RB.108 2145:RB.106 2069:Type R 2064:Type F 2059:Type G 2054:Type H 2013:Merlin 1988:Falcon 1958:Condor 1845:BS.605 1787:Nimbus 1777:BS.360 1744:BS.100 1674:Taurus 1649:Aquila 1563:Cherub 1469:Flight 1457:Flight 1424:  1410:  1396:  1382:  1368:  1344:Protec 1157:Flight 1044:  766:thrust 673:Flight 551:Victor 392:, and 243:piston 240:radial 212:marine 181:reheat 4130:XA103 4125:XA102 4120:XA101 4115:XA100 3985:YF120 3462:YJ101 2952:R-975 2947:R-790 2942:R-760 2937:R-540 2930:J-6-9 2925:J-6-7 2920:J-6-5 2806:V-720 2567:RB508 2562:RB410 2557:RB235 2552:RB220 2547:RB211 2542:RB203 2537:RB207 2532:RB202 2527:RB199 2517:RB183 2512:RB181 2507:RB178 2502:RB177 2497:RB176 2492:RB175 2487:RB174 2482:RB172 2472:RB168 2467:RB163 2457:RB153 2452:RB146 2447:RB145 2442:RB142 2437:RB141 2432:RB140 2427:RB109 2422:RB108 2417:RB106 2344:Tweed 2339:Trent 2329:Gnome 2314:Clyde 2282:RB235 2277:RB220 2272:RB211 2267:RB202 2261:RB199 2250:RB178 2234:RB153 2208:Adour 2185:Viper 2165:RB176 2091:Larch 1963:Crecy 1850:Gamma 1792:Orion 1754:Viper 1664:Orion 1627:Titan 1612:Orion 1587:Hydra 1582:Draco 1467:1961 1154:Arrow 850:Notes 696:Type: 364:WD952 353:F-102 309:surge 134:spool 86:1950 43:Type 4097:F415 4092:F414 4087:F412 4082:F408 4077:F405 4072:F404 4067:F402 4062:F401 4057:F400 4050:F138 4045:F137 4040:F136 4035:F135 4030:F130 4025:F129 4020:F128 4015:F127 4010:F126 4005:F125 4000:F124 3995:F122 3990:F121 3980:F119 3975:F118 3970:F117 3965:F113 3960:F112 3955:F110 3950:F109 3945:F108 3940:F107 3935:F106 3930:F105 3925:F104 3920:F103 3915:F102 3910:F101 3905:F100 3898:TF41 3893:TF39 3888:TF37 3883:TF35 3878:TF34 3873:TF33 3868:TF32 3863:TF31 3858:TF30 3840:T901 3835:T900 3820:T708 3815:T706 3810:T703 3805:T702 3800:T701 3795:T700 3788:T408 3783:T407 3778:T406 3773:T405 3768:T400 3761:T101 3756:T100 3496:J700 3489:J403 3484:J402 3479:J401 3474:J400 3467:J102 3457:J100 3437:YJ93 3307:XJ49 3267:XJ41 3252:XJ38 3150:RJ55 3145:RJ47 2754:and 2710:and 2412:RB93 2407:RB82 2402:RB80 2397:RB53 2392:RB50 2387:RB44 2382:RB41 2377:RB39 2372:RB37 2367:RB23 2349:Tyne 2319:Dart 2287:Spey 2218:M45H 2170:Soar 2124:Nene 2114:Avon 2049:PV12 2003:Hawk 1826:Odin 1821:Thor 1694:and 1422:ISBN 1408:ISBN 1394:ISBN 1380:ISBN 1366:ISBN 1203:link 1189:2011 1042:ISBN 952:link 938:2015 903:2016 877:2016 788:3.04 682:and 638:The 409:and 334:cans 276:and 235:and 124:The 3749:T80 3744:T78 3739:T76 3734:T74 3729:T73 3724:T72 3719:T71 3714:T70 3709:T69 3704:T68 3699:T67 3694:T66 3689:T65 3684:T64 3679:T63 3674:T62 3669:T61 3664:T60 3659:T58 3654:T57 3644:T56 3639:T55 3634:T54 3629:T53 3624:T52 3619:T51 3614:T50 3609:T49 3604:T48 3599:T47 3594:T46 3589:T45 3584:T44 3579:T43 3574:T42 3569:T41 3564:T40 3559:T39 3554:T38 3549:T37 3544:T36 3539:T35 3534:T34 3529:T33 3524:T31 3519:T30 3452:J99 3447:J97 3442:J95 3432:J91 3427:J89 3422:J87 3417:J85 3412:J83 3407:J81 3402:J79 3397:J75 3392:J73 3387:J71 3382:J69 3377:J67 3372:J65 3367:J63 3362:J61 3357:J60 3352:J59 3347:J58 3342:J57 3337:J56 3332:J55 3327:J54 3322:J53 3317:J52 3312:J51 3302:J48 3297:J47 3292:J46 3287:J45 3282:J44 3277:J43 3272:J42 3262:J40 3257:J39 3247:J37 3242:J36 3237:J35 3232:J34 3227:J33 3222:J32 3217:J31 3212:J30 3127:T49 3122:T35 3100:J67 3095:J65 3090:J61 3085:J59 2915:J-5 2910:J-4 2905:J-3 2880:L-5 2875:L-4 2870:L-3 2865:L-2 2860:L-1 2855:J-2 2850:J-1 2845:C-2 2840:A-3 2324:Gem 2175:Tay 2028:"R" 1983:Exe 374:TBO 155:SST 4153:: 1766:/ 1708:/ 1527:/ 1325:, 1224:^ 1199:}} 1195:{{ 1164:^ 1024:^ 948:}} 944:{{ 670:. 421:. 388:, 157:. 3650:) 3508:/ 3184:e 3177:t 3170:v 3112:/ 2776:E 2744:e 2737:t 2730:v 2609:: 2304:/ 2135:) 1919:e 1912:t 1905:v 1838:: 1814:: 1770:: 1730:) 1712:: 1642:: 1575:: 1556:: 1517:e 1510:t 1503:v 1205:) 1191:. 1101:. 954:) 940:. 905:. 879:. 786:: 777:: 768:: 745:: 736:: 553:.

Index


Turbojet
United Kingdom
Bristol Aero Engines
Bristol Siddeley Engines Limited
Rolls-Royce Bristol Engine Division
Avro Vulcan
BAC TSR-2
Rolls-Royce/Snecma Olympus 593
Rolls-Royce Marine Olympus
spool
axial-flow
turbojet
Pratt & Whitney J57
Avro Vulcan
Concorde
SST
Bristol Aeroplane Company
Bristol Aero Engines
V bombers
Air Ministry
reheat
BAC TSR-2
Armstrong Siddeley
Bristol Siddeley
Rolls-Royce
Rolls-Royce/Snecma Olympus 593
Curtiss-Wright
marine
gas turbines

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