143:
189:(BPR) of about 1.2, was decided by Rolls-Royce. The bypass ratio was chosen for long-range, with low fuel consumption, particularly when throttled back. The selected BPR also gave a higher reheat boost than with smaller values used on similar engines. The design of the individual modules was shared between Rolls-Royce, MTU and Fiat according to their existing expertise. Rolls-Royce designed the fan using scaled-down Pegasus knowledge, the combustor, the high pressure (HP) turbine and the
47:
231:
introduced to improve the life of the blades for the
European operating conditions and revised cooling hole arrangements were introduced at the same time to reduce the detrimental effect of sand on blade cooling. With incorporation of these blade processing and cooling changes "Desert Storm Tornado aircraft flew some of the most arduous missions of any Allied aircraft with reliability no worse than peacetime and no engines were rejected for HP Turbine blade defects."
193:. The reheat used cold air combustion techniques, described by Sotheran and which were derived from their experience with ramjets and plenum chamber burning (PCB) in Pegasus front nozzles. Fiat had built turbines for the Viper so designed the low pressure (LP) turbine as well as the final nozzle. MTU designed the intermediate pressure(IP) and high pressure (HP) compressors, the IP turbine, and the thrust reverser.
196:
A three-spool arrangement reduces the pressure ratio on each compressor so no variable stators were needed. To meet the short afterburner requirement an arrangement known as mix-then-burn, as used in current engines, was not possible because it was too long and heavy. The RB199 used a much shorter
230:
produced new problems. Frequent flying in air carrying different sizes of sand particles caused deposits on the HP turbine blades from sand passing through the combustor. In addition, sand carried with the cooling air through the blades blocked the cooling holes. Single crystal blades were being
158:
MRCA. The engine requirements to meet the
Panavia MRCA specification were significant advances over current engines in thrust-to-weight ratio, fuel consumption and size. The final selection of the engine for the MRCA was made between a new European collaboration,
182:, where the three-shaft RB211 engine was in development, three shafts were considered better. Rolls-Royce took over Bristol Siddeley in 1967 so the configuration for the RB199 was decided jointly, a three-shaft engine.
234:
Looking back on the RB199 program in 2002 Chief
Engineer for the RB199, Dr.Gordon Lewis, concluded "The final production standard provided satisfactory reliability and performance."
705:, AGARD Conference Proceedings CP No.558, Erosion, Corrosion, Foreign Object Damage Effects in Gas Turbine Engines,Paper 1, Out of Area Experiences with the RB199 in Tornado
211:
Service flying with the Royal Air Force, German Navy and German and
Italian Air Forces in the European environment showed normal failure mechanisms for turbine blades,
895:
226:
Sand ingestion tests had been done and passed as part of the qualification for service introduction but operating in desert conditions with the
223:) so development started on replacing the initial production equiaxed blades with single-crystal ones which last longer at high temperatures.
888:
795:
881:
868:
246:
Initial variant powered first
Tornado IDS deliveries, with a 38.7kN (8700lbf) dry thrust, 66.01kN (14840lbf) with afterburner.
1411:
1401:
719:
666:
646:
617:
583:
563:
546:
529:
332:
746:
1364:
1074:
851:
687:
1138:
812:
1406:
1238:
338:
1115:
932:
318:
1284:
163:, with the RB199, and Pratt & Whitney who proposed the JTF16. The Panavia MRCA would later be called the
55:
1333:
1262:
1166:
1161:
702:
1198:
1082:
1313:
151:
299:
A derivative of the Mk104 (originally designated Mk 104E), powering the first two prototypes of the
500:
575:
1216:
1183:
1007:
971:
1378:
1358:
1270:
1144:
1028:
1012:
953:
463:
433:
208:
that was representative of the
Tornado aircraft. The Vulcan first flew with the RB199 in 1972.
1327:
1191:
1050:
483:
227:
17:
658:
638:
609:
1291:
261:
185:
The overall design concept for the international collaborative program, three shafts and a
8:
957:
922:
792:
300:
216:
200:
The RB199 first ran on 27 September 1971 at
Patchway, UK. It was flight-tested using an
119:
1354:
1256:
1109:
1036:
840:
220:
661:, AGARD Conference Proceedings CP No.422, Combustion and Fuels in Gas Turbine Engines,
612:, AGARD Conference Proceedings CP No.422, Combustion and Fuels in Gas Turbine Engines,
293:
versions and applicable to IDS, with a thrust rating of 42.5 kN (dry) 74.3 kN (reheat)
1372:
999:
977:
847:
715:
683:
662:
642:
613:
579:
559:
542:
525:
322:
175:
146:
Turbo Union RB199 turbofan engine on display at
Montrose Air Station Heritage Centre
1252:
1105:
905:
342:
171:
123:
1129:
1068:
1022:
873:
799:
747:"Montrose Tornado will blow visitors away as Angus air station's star attraction"
596:
290:
253:
212:
164:
131:
95:
1276:
1056:
270:
1395:
1042:
629:
Flight
International, 22 August 1981,RB.199: Compact Tornado power, p.552-558
304:
257:
142:
1090:
1064:
963:
488:
442:
328:
A Turbo-Union RB199 is on public display at the
Morayvia Centre in Kinloss.
186:
150:
The RB199 originated with a requirement, in 1969, to power a new European
46:
1224:
985:
201:
190:
179:
160:
115:
75:
703:
https://archive.org/details/NASA_NTRS_Archive_19950013267?q=agard+cp+558
1319:
1305:
991:
111:
768:
1244:
1210:
1153:
1095:
127:
1123:
944:
913:
108:
65:
1345:
429:
40 kN (9,100 lbf) dry, 73 kN (16,400 lbf) wet
407:
280:
205:
155:
1206:
1177:
926:
714:
The Birth Of Tornado, Royal Air Force Historical Society 2002,
576:
https://archive.org/details/DTIC_ADA129168?q=agard+cp+324,AGARD
558:
The Birth Of Tornado, Royal Air Force Historical Society 2002,
424:
31:
1299:
597:"Reheat Combustion Apparatus for Bypass Gas Turbine Engines"
722:, RB199- The Engine For Tornado by Dr. Gordon Lewis, p.50
680:
Flight International World Aircraft and Systems Directory
659:
https://archive.org/details/DTIC_ADA202495?q=agard+cp+422
641:, AGARD Conference Proceedings CP No.324,Engine Handling,
639:
https://archive.org/details/DTIC_ADA129168?q=agard+cp+324
610:
https://archive.org/details/DTIC_ADA202495?q=agard+cp+422
566:, RB199- The Engine For Tornado by Dr. Gordon Lewis, p.50
178:
and were based on the Pegasus two-spool arrangement. At
337:
A Turbo-Union RB199 Mk.103 is on public display at the
273:, with a thrust rating of 40.5 kN (dry) 73 kN (reheat)
669:,High Performance Turbofan Afterburner Systems p.12-5
620:,High Performance Turbofan Afterburner Systems p.12-2
682:. Reed Business Information Ltd. 2001. p. 187.
903:
839:
921:
578:Conference Proceedings CP No.324,Engine Handling,
1393:
842:Brassey's World Aircraft & Systems Directory
331:A Turbo-Union RB199 is on public display at the
317:A Turbo-Union RB199 is on public display at the
303:(DA1 and DA2) until the initial versions of the
256:strike versions, with a thrust rating of 40.5
889:
541:Rolls-Royce Aero-Engines, Bill Gunston 1989,
349:
732:
730:
728:
412:Single-stage HP, single-stage IP, 2-stage LP
237:
30:"RB199" redirects here. For the galaxy, see
739:
896:
882:
363:
130:. The only production application was the
725:
524:Jane's All The World's Aircraft 1975-76,
137:
114:designed and built in the early 1970s by
141:
14:
1394:
837:
586:CP 324, Round Table Discussion p.RTD-8
877:
311:
174:had already been done to support the
333:Montrose Air Station Heritage Centre
24:
403:3-stage LP, 3-stage IP, 6-stage HP
25:
1423:
862:
197:arrangement known as mix/burn.
45:
805:
786:
773:City of Norwich Aviation Museum
761:
708:
696:
672:
339:City of Norwich Aviation Museum
204:with the engine installed in a
846:. London, England: Brassey's.
838:Taylor, Michael J. H. (1996).
652:
632:
623:
603:
589:
569:
552:
535:
518:
416:
319:Royal Air Force Museum Cosford
271:Tornado F3 Air Defence Variant
13:
1:
506:
394:
56:Royal Air Force Museum Hendon
1412:Three-spool turbofan engines
27:Aircraft turbofan jet engine
7:
1402:Low-bypass turbofan engines
472:
390:976 kg (2,151 lb)
378:3,600 mm (142 in)
170:Advanced engine studies at
10:
1428:
1083:International Aero Engines
749:. The Courier. 20 May 2022
457:Turbine inlet temperature:
384:720 mm (28.3 in)
350:Specifications (RB199-104)
118:, a joint venture between
29:
1371:
1353:
1344:
1326:
1314:MTU Turbomeca Rolls-Royce
1312:
1298:
1283:
1269:
1251:
1237:
1223:
1205:
1190:
1175:
1151:
1136:
1122:
1104:
1081:
1063:
1049:
1035:
1021:
998:
984:
970:
952:
943:
912:
343:Horsham St Faith, Norfolk
238:Variants and applications
152:multirole combat aircraft
53:
44:
39:
736:Taylor 1996, pp. 610–611
501:List of aircraft engines
219:and high cycle fatigue (
869:Rolls-Royce.com - RB199
813:"RB199 Turbofan Engine"
364:General characteristics
279:Derivative used on the
1407:1970s turbofan engines
1271:Europrop International
802:Retrieved:27 July 2009
464:Thrust-to-weight ratio
434:Overall pressure ratio
147:
138:Design and development
1328:Rolls-Royce Turbomeca
1192:Rolls-Royce Turbomeca
1051:GE Honda Aero Engines
484:General Electric F404
228:Royal Saudi Air Force
145:
793:RB199-104 data sheet
1355:Pratt & Whitney
1257:Pratt & Whitney
1110:Pratt & Whitney
958:Rolls-Royce Limited
358:Rolls-Royce and MTU
301:Eurofighter Typhoon
1037:EuroJet Turbo GmbH
904:Joint development
798:2011-06-05 at the
478:Comparable engines
312:Engines on display
154:(MRCA) called the
148:
91:Major applications
1389:
1388:
1385:
1384:
1373:CFM International
1340:
1339:
1000:CFM International
939:
938:
468:7.6 (with reheat)
323:Brooklands Museum
176:BAC/Dassault AFVG
105:Turbo-Union RB199
101:
100:
16:(Redirected from
1419:
1351:
1350:
1065:General Electric
950:
949:
919:
918:
898:
891:
884:
875:
874:
857:
845:
824:
823:
817:
809:
803:
790:
784:
783:
781:
779:
765:
759:
758:
756:
754:
743:
737:
734:
723:
712:
706:
700:
694:
693:
676:
670:
656:
650:
636:
630:
627:
621:
607:
601:
600:
593:
587:
573:
567:
556:
550:
539:
533:
522:
172:Bristol Siddeley
92:
49:
37:
36:
21:
1427:
1426:
1422:
1421:
1420:
1418:
1417:
1416:
1392:
1391:
1390:
1381:
1367:
1336:
1322:
1308:
1294:
1279:
1265:
1247:
1233:
1219:
1201:
1186:
1171:
1147:
1132:
1118:
1100:
1077:
1059:
1045:
1031:
1023:Engine Alliance
1017:
994:
980:
972:BMW Rolls-Royce
966:
935:
908:
902:
865:
860:
854:
828:
827:
815:
811:
810:
806:
800:Wayback Machine
791:
787:
777:
775:
767:
766:
762:
752:
750:
745:
744:
740:
735:
726:
713:
709:
701:
697:
690:
678:
677:
673:
657:
653:
637:
633:
628:
624:
608:
604:
595:
594:
590:
574:
570:
557:
553:
540:
536:
523:
519:
509:
475:
419:
397:
366:
352:
314:
307:were available.
240:
213:thermal fatigue
165:Panavia Tornado
140:
132:Panavia Tornado
96:Panavia Tornado
90:
35:
28:
23:
22:
15:
12:
11:
5:
1425:
1415:
1414:
1409:
1404:
1387:
1386:
1383:
1382:
1377:
1375:
1369:
1368:
1363:
1361:
1348:
1342:
1341:
1338:
1337:
1332:
1330:
1324:
1323:
1318:
1316:
1310:
1309:
1304:
1302:
1296:
1295:
1292:Ardiden/Shakti
1290:
1288:
1281:
1280:
1275:
1273:
1267:
1266:
1261:
1259:
1249:
1248:
1243:
1241:
1235:
1234:
1229:
1227:
1221:
1220:
1215:
1213:
1203:
1202:
1197:
1195:
1188:
1187:
1182:
1180:
1173:
1172:
1170:
1169:
1164:
1158:
1156:
1149:
1148:
1143:
1141:
1134:
1133:
1128:
1126:
1120:
1119:
1114:
1112:
1102:
1101:
1099:
1098:
1093:
1087:
1085:
1079:
1078:
1073:
1071:
1061:
1060:
1055:
1053:
1047:
1046:
1041:
1039:
1033:
1032:
1027:
1025:
1019:
1018:
1016:
1015:
1010:
1004:
1002:
996:
995:
990:
988:
982:
981:
976:
974:
968:
967:
962:
960:
947:
941:
940:
937:
936:
931:
929:
916:
910:
909:
901:
900:
893:
886:
878:
872:
871:
864:
863:External links
861:
859:
858:
852:
834:
833:
832:
826:
825:
804:
785:
769:"Engines List"
760:
738:
724:
707:
695:
688:
671:
651:
631:
622:
602:
588:
568:
551:
534:
516:
515:
514:
513:
508:
505:
504:
503:
492:
491:
486:
474:
471:
470:
469:
460:
454:
451:Air mass flow:
448:
439:
430:
418:
415:
414:
413:
404:
396:
393:
392:
391:
385:
379:
373:
365:
362:
351:
348:
347:
346:
335:
329:
326:
313:
310:
309:
308:
297:
294:
287:
284:
277:
274:
267:
264:
260:(dry) 71.2 kN
250:
247:
244:
239:
236:
139:
136:
99:
98:
93:
87:
86:
83:
79:
78:
73:
69:
68:
63:
59:
58:
51:
50:
42:
41:
26:
9:
6:
4:
3:
2:
1424:
1413:
1410:
1408:
1405:
1403:
1400:
1399:
1397:
1380:
1376:
1374:
1370:
1366:
1362:
1360:
1356:
1352:
1349:
1347:
1343:
1335:
1331:
1329:
1325:
1321:
1317:
1315:
1311:
1307:
1303:
1301:
1297:
1293:
1289:
1286:
1282:
1278:
1274:
1272:
1268:
1264:
1260:
1258:
1254:
1250:
1246:
1242:
1240:
1236:
1232:
1228:
1226:
1222:
1218:
1214:
1212:
1208:
1204:
1200:
1196:
1193:
1189:
1185:
1181:
1179:
1174:
1168:
1165:
1163:
1160:
1159:
1157:
1155:
1150:
1146:
1142:
1140:
1135:
1131:
1127:
1125:
1121:
1117:
1113:
1111:
1107:
1103:
1097:
1094:
1092:
1089:
1088:
1086:
1084:
1080:
1076:
1072:
1070:
1066:
1062:
1058:
1054:
1052:
1048:
1044:
1040:
1038:
1034:
1030:
1026:
1024:
1020:
1014:
1011:
1009:
1006:
1005:
1003:
1001:
997:
993:
989:
987:
983:
979:
975:
973:
969:
965:
961:
959:
955:
951:
948:
946:
942:
934:
930:
928:
924:
920:
917:
915:
911:
907:
899:
894:
892:
887:
885:
880:
879:
876:
870:
867:
866:
855:
853:1-85753-198-1
849:
844:
843:
836:
835:
830:
829:
821:
814:
808:
801:
797:
794:
789:
774:
770:
764:
748:
742:
733:
731:
729:
721:
720:0 9530345 0 X
717:
711:
704:
699:
691:
689:0-617-01289-X
685:
681:
675:
668:
667:92 835 0465 8
664:
660:
655:
648:
647:92 835 0327 9
644:
640:
635:
626:
619:
618:92 835 0465 8
615:
611:
606:
598:
592:
585:
584:92 835 0327 9
581:
577:
572:
565:
564:0 9530345 0 X
561:
555:
548:
547:1 85260 037 3
544:
538:
531:
530:0 531 03250 7
527:
521:
517:
511:
510:
502:
499:
498:
497:
496:
495:Related lists
490:
487:
485:
482:
481:
480:
479:
467:
465:
461:
458:
455:
452:
449:
446:
444:
440:
437:
435:
431:
428:
426:
421:
420:
411:
409:
405:
402:
399:
398:
389:
386:
383:
380:
377:
374:
371:
368:
367:
361:
359:
356:
344:
340:
336:
334:
330:
327:
324:
320:
316:
315:
306:
305:Eurojet EJ200
302:
298:
295:
292:
288:
285:
282:
278:
276:RB 199 Mk104D
275:
272:
269:Powering the
268:
265:
263:
259:
255:
251:
248:
245:
242:
241:
235:
232:
229:
224:
222:
218:
214:
209:
207:
203:
198:
194:
192:
188:
183:
181:
177:
173:
168:
166:
162:
157:
153:
144:
135:
133:
129:
125:
121:
117:
113:
110:
106:
97:
94:
89:
88:
84:
81:
80:
77:
74:
72:Manufacturer
71:
70:
67:
64:
61:
60:
57:
54:RB199 at the
52:
48:
43:
38:
33:
19:
1230:
1176:Rolls-Royce/
1152:Rolls-Royce/
1137:Rolls-Royce/
906:aero engines
841:
831:Bibliography
819:
807:
788:
776:. Retrieved
772:
763:
751:. Retrieved
741:
710:
698:
679:
674:
654:
634:
625:
605:
591:
571:
554:
537:
520:
494:
493:
489:Klimov RD-33
477:
476:
462:
456:
450:
443:Bypass ratio
441:
432:
422:
406:
400:
387:
381:
375:
369:
357:
354:
353:
286:RB199 Mk 105
266:RB199 Mk 104
249:RB199 Mk 103
243:RB199 Mk 101
233:
225:
210:
199:
195:
187:bypass ratio
184:
169:
149:
104:
102:
1225:Turbo-Union
1069:Rolls Royce
986:CFE Company
933:Olympus 593
923:Rolls-Royce
417:Performance
401:Compressor:
388:Dry weight:
291:Tornado ECR
254:Tornado IDS
202:Avro Vulcan
180:Rolls-Royce
161:Turbo Union
120:Rolls-Royce
116:Turbo-Union
76:Turbo-Union
1396:Categories
1287:/Turbomeca
1008:CFM56/F108
507:References
395:Components
325:Weybridge.
112:jet engine
82:First run
1211:Turbomeca
1154:MAN Turbo
945:Turbofans
914:Turbojets
778:27 August
382:Diameter:
355:Data from
296:RB199-122
289:Powering
252:Powering
128:Aeritalia
1346:Propfans
1306:T800-LHT
1277:TP400-D6
1263:T800-APW
1124:PowerJet
1091:SuperFan
796:Archived
649:, p.25-2
473:See also
459:~1,600 K
423:Maximum
372:Turbofan
262:(reheat)
109:turbofan
66:Turbofan
1359:Allison
1116:RTF-180
954:Allison
753:18 June
549:, p.232
453:70 kg/s
408:Turbine
376:Length:
281:BAe EAP
206:nacelle
156:Panavia
1365:578-DX
1334:RTM322
1320:MTR390
1217:Larzac
1207:Snecma
1178:Snecma
1167:RB.193
1162:RB.153
1130:SaM146
1029:GP7000
992:CFE738
927:Snecma
850:
718:
686:
665:
645:
616:
582:
562:
545:
528:
438:23.5:1
425:thrust
191:reheat
40:RB199
32:RB 199
1300:LHTEC
1231:RB199
1199:Adour
1145:RJ500
1096:V2500
1057:HF120
1043:EJ200
978:BR700
816:(PDF)
532:p.112
512:Notes
447:1.1:1
370:Type:
217:creep
107:is a
85:1971
62:Type
18:RB199
1379:RISE
1253:Avco
1245:T900
1239:ATEC
1184:M45H
1139:JAEC
1075:F136
1013:LEAP
964:TF41
848:ISBN
780:2023
755:2022
716:ISBN
684:ISBN
663:ISBN
643:ISBN
614:ISBN
580:ISBN
560:ISBN
543:ISBN
526:ISBN
321:and
126:and
103:The
1285:HAL
1106:MTU
820:MTU
341:in
221:HCF
124:MTU
1398::
818:.
771:.
727:^
258:kN
215:,
167:.
134:.
122:,
1357:/
1255:/
1209:/
1194::
1108:/
1067:/
956:/
925:/
897:e
890:t
883:v
856:.
822:.
782:.
757:.
692:.
599:.
466::
445::
436::
427::
410::
360:.
345:.
283:.
34:.
20:)
Text is available under the Creative Commons Attribution-ShareAlike License. Additional terms may apply.
