FLIGHT International, 2 January 1969 27 1-p turbine. Take
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FLIGHT International, 2 January 1969 27 h-p and 1-p turbines. Take-ofi 9,8501b; b.p.r. 1.0-1; mass flow 2031b/sec; pressure ratio 16.8:1; length HOin; width 41in; height 45in; weight 2,2201b. RB.163-25 Mk 512 Aft-fan Civil twin-spool/free-turbine aft-fan turbofan. Study engine for projected BAC One-Eleven 600, com- prising Spey-25 Mk 512 with addition of aft-fan driven by free- turbine operating in Spey exhaust flow to give increased thrust with reduced s.f.c. and take-off noise. Overall b.p.r. is increased to 5.7:1 with initial rating of about 15,0001b rising with develop- ment to 17,000-18,0O01b. Intended later that aft-fan unit (which has own annular intake) would have reversible pitch fan blades to eliminate for separate thrust reverser. RB.162 Military single-shaft lift engine. Second-generation Rolls- Royce lift engine powering experimental V/STOL aircraft. Develop- ment is financed by the British, German and French governments, and Rolls-Royce. A 7,0001b thrust version of the RB.162 proposed for STOL version of Boeing 737 using eight liftjets with swivel exhaust nozzles. Applications Dassault Mirage III V, 8 XRB.162-31 (5,6001b). Dornier Do31E, 8XRB.162-4D (4,4001b). VFW VAK/191B. 2XRB.162-81 (6,0001b). (RB162-81) Six-stage compressor, annular combustor, single-stage turbine. Take-off"6,0001b (with 10 per cent air bleed); pressure ratio 4.25:1; length 50in; diameter 29in; weight 3751b. RB.162 Civil single-shaft turbojet booster. Through close similarity between operational and design requirements of liftjets and booster engines, RB.162 has been readily adapted to booster role. Its sole application to date is in the Hawker Siddeley Trident 3B (1 xRB.162-86) where the booster engine is mounted above the centre Spey main turbofan. Booster improves short-field and engine-out performance, gives rapid climb out and reduces fly-over noise. (RB.162-86) Configuration same as RB.162 liftjet. Take-off 5,2501b (available —27°C to +20°C, s.l.s.); length 54in; diameter 29in; weight 5601b. Tyne Civil and military twin-spool turboprop. Sole example of a twin-spool turboprop to enter service, the Tyne for its French and German application is license-manufactured by the European Con- sortium comprising Hispano-Suiza, MAN Turbo, Fabrique Nation- ale and Rolls-Royce. Applications Aviation Traders Merchantman (Vanguard conver- sion), 4 x Tyne R Tyl Mk 506 (4,785 e.h.p.) or Tyne R Tytl Mk 512 (5,325 e.h.p.). BAC Vanguard 951, 4xTyne R Tyl Mk 506 (4,785 e.h.p.). BAC Vanguard 952, 4xTyne R Tyll Mk 512 (5,325 e.h.p.). Breguet 1150 Atlantic, 2 X Tyne R Ty20 Mk 21 (6,105 e.h.p.). Canadair CL-44D-4, 4xTyne R Tyl2 Mk 515 (5,500 e.h.p.). Canadair CL-44J & CC-106 Yukon, 4xTyne R Tyl2 Mk 515/10 (5,730 e.h.p.). Short Belfast C Mk 1, 4xTyne R Tyl2 Mk 101 (5,715 e.h.p.). Transall C-160D, 2xTyne R Ty20 Mk 22 (6,100 e.h.p.). (Tyne R Ty20) Six-stage 1-p compressor, nine-stage h-p com- pressor, cannular combustor with ten flame tubes, single-stage h-p turbine, three-stage 1-p turbine. Integral, front-mounted gear- box. Take-off 5,855 e.h.p.; mass flow 46.51b/sec; pressure ratio 13.5:1; length 108.7in; diameter 43.2in; weight 2,2181b. RB.108 Military single-shaft lift engine. Pioneer lift engine power- ing experimental V/STOL aircraft and hover rigs. Applications Dassault Balzac, 8 X RB.108. Dornier Hover Rig, 4XRB.108. EWR-Stud Hover Rig, 3XRB.108. EWR WipDe Rig, 1XRB.108. Fiat Hover Rig 2XRB.108. Short SCI, 5XRB.108. VFW SG-1262 Hover Rig, 5 x RB.108. (RB.108) Eight-stage compressor, annular combustor, single-stage turbine. Take-off 2,2101b (total, with 11 per cent air bleed); mass flow 38.851b/sec; pressure ratio 5.33:1: length 48.3in; diameter 20.8in; weight 2691b. Gazelle Military free-turbine turboshaft. Originally of Napier design, has prime application in the Westland Wessex helicopter. Applications Westland Belvedere HC.l, 2 XGazelle NGa2 Mk 101 1,465 s.h.p.). Westland Wessex HAS Mk 1, lxGazelle NGal3 Mk 161 (1,450 s.h.p.). Westland Wessex HAS Mk 3, IX Gazelle NGa22 Mk 165 (1,600 s.h.p.). Westland HAS Mk 31, lxGazelle Mk 162 (1,540 sJi.p.). (Gazelle NGa22 Mk 165) Eleven-stage compressor, tubular com- bustor with six flame tubes, two-stage compressor-turbine, single- stage power turbine. Integral rear-mounted gearbox. Take-off 1,600 s.h.p.; mass flow 17!61b/sec; pressure ratio 6.35:1; length 75in; diameter 33.5in; weight 8701b. Conway RCo.42 and 43 Civil and military twin-spool turbofan. Final variants of the Conway, developed specifically to power the BAC VC10 and Super VC10. Applications BAC VC10, 4 X Conway RCo.42 Mk 540 (20,3701b). BAC VC10 C Mk 1, 4xConway RCo.43 Mk 301 (22,5001b). BAC Super VC10, 4xConway RCo.43 Mk 550 (21,8001b). (Conway RCo.43 Mk 550) Four-stage fan/l-p compressor plus four-stage i-p compressor, nine-stage h-p compressor, cannular combustor with ten flame tubes, single-stage h-p turbine, two-stage 1-p turbine. Take-off 21,8001b; b.p.r. 0.6:1; mass flow 3751b/see; pressure ratio 15.8:1; length 154in; diameter 50in; weight 5,1011b. Conway R.Co.17 Miltary twin-spool turbofan. Sole application is the Handley Page Victor B2 as the 20,6001b Mk 201. Conway R.Co.12 Civil twin-spool turbofan. Pioneering commercial turbofan derived from the original military engine for the Vickers V.1000. Applications Boeing 707-420, 4 x Conway R.Co.12 Mk 508 (17,5001b). Douglas DC-8 Series 40, 4XConway R.Co.12 Mk 509 (17,5001b). (Conway R.Co.12 Mk 509) Seven-stage fan/l-p compressor, nine- stage h-p compressor, cannular combustor with ten flame tubes, single-stage h-p turbine, two-stage l-p turbine. Take-off 17,0001b; b.p.r. 0.3:1; mass flow 2801b/sec; pressure ratio 14:1; length 136in; diameter 42in; weight 4,5421b. RB.146 Avon 300 Military single-shaft augmented turbojet. Most powerful military Avon, introduced for later versions of the BAC Lightning. License-manufactured by Flygmotor as RM6, with Swedish afterburner, for Saab 35 Draken series. Applications BAC Lightning F6, T5 and T. Mk 55, 2 X Avon Mk 301 (12,6901b, or 16,8601b with afterburning). BAC Lightning F.53, 2xAvon Mk 302-C (11,1001b, or 16,3001b with afterburning). Avon RA.29 Civil and military single-shaft turbojet. Derived from the Avon 200 series for commercial operation. Applications Hawker Siddeley Comet 4 & 4C, 4 x Avon RA.29/l Mk 524B (10,2501b). Hawker Siddeley Comet 4B, 4 x Avon RA.29/1 Mk 525B (10,2501b). Sud-Aviation Caravelle III, 2 x Avon RA.29/3 Mk 527B (11,4001b). Sud-Aviation Caravelle VI N, 2 x Avon RA.29/3 Mk 531B (12,2001b). Sud-Aviation Caravelle VI R, 2 X Avon RA.29/3 Mk 533R (12,6001b). (Avon RA.29/1) Sixteen-stage compressor, cannular combustor, three-stage turbine. Take-off 10,2501b; pressure ratio 9.08:1; length 126in ; diameter 39in ; weight 3,3431b. RB.90 Avon 200 Military single-shaft augmented turbojet. Major military version of the Avon. License-manufactured by Fabrique Nationale, and by Flygmotor as RMS with Swedish afterburner to power Saab Lansen. Applications BAC 221, lxAvon RA.28R (14,4301b with after- burning). BAC Canberra Mk 9, 2 x Avon RA.24 Mk 206 (11,2501b). BAC Lightning F2, 3 & 5, 2xAvon RA.24R Mk 210 (11,2501b, or 14,3701b with afterburning). BAC Scimitar Fl, 2 x Avon RA.24 Mk 202 (11,2501b). Hawker Siddeley Hunter Mks 9, 10 & 12, lxAvon RA.28 Mk 207 (10,1501b). Hawker Siddeley Sea Vixen FAW2, 2 X Avon RA.24 Mk 208 (11,2501b). (RB.90 Avon RA.28 Mk 208) Fifteen-stage compressor, cannular combustor, two-stage turbine. Take-off 11,2501b; length 126.9in; diameter 28in. Dart Civil and military single-shaft turboprop. Outstandingly successful turboprop, still in quantity production since starting in 1953. Applications BAC Project 201, 2 x Dart RDa.7 (2,230 e.h.p.). BAC Viscount 700, 4 X Dart RDa.6 Mk 510 (1,670 e.h.p.). BAC Viscount 800, 4xDart RDa.6 Mk 510 (1,670 e.h.p.), or Dart RDa.7 Mk 520 (1,815 ch.p.), or Dart RDa.7/1 Mk 525F (1,910 e.h.p.), or Dart RDa.7/2 Mk 530 (2,020 e.h.p.). Breguet 1050 Alize, IX Dart RDa.7 Mk 21 (2,020 e.h.p.). Cavalier Aircraft Mustang 3 Conversion, lxDart RDa.6 Mk 510 (1,440 s.h.p.) or Dart RDa. 7/2 Mk 529 (2,185 s.h.p.). Convair 600/640, 2 X Dart RDa.lO Mk 542^1 (3,025 e.p.h.). FairchUd Hiller F-27, 2xDart RDa.6 Mk 511 (1,670 e.h.p.). Fairchild Hiller F-27A & F, 2xDart RDa.7 Mk 528-7E (2,105 e.h.p.). Fairchild Hiller F-27B, 2 X Dart RDa.6 Mk 514-7 (1,850 e.h.p.). Fairchild Hiller F-27J, F-227 & Under joint development and manufacture by Rolls-Royce's Bristol Engine Division and Snecma in France, the M45H civil twin-spool turbofan has been designed to meet the economical fuel consump- tion requirements of Germany's VFW6I4 short-haul airliner
Transcript of FLIGHT International, 2 January 1969 27 1-p turbine. Take
FLIGHT International, 2 January 1969 27
h-p and 1-p turbines. Take-ofi 9,8501b; b.p.r. 1.0-1; mass flow 2031b/sec; pressure ratio 16.8:1; length HOin; width 41in; height 45in; weight 2,2201b. RB.163-25 Mk 512 Aft-fan Civil twin-spool/free-turbine aft-fan turbofan. Study engine for projected BAC One-Eleven 600, comprising Spey-25 Mk 512 with addition of aft-fan driven by free-turbine operating in Spey exhaust flow to give increased thrust with reduced s.f.c. and take-off noise. Overall b.p.r. is increased to 5.7:1 with initial rating of about 15,0001b rising with development to 17,000-18,0O01b. Intended later that aft-fan unit (which has own annular intake) would have reversible pitch fan blades to eliminate for separate thrust reverser.
RB.162 Military single-shaft lift engine. Second-generation Rolls-Royce lift engine powering experimental V/STOL aircraft. Development is financed by the British, German and French governments, and Rolls-Royce. A 7,0001b thrust version of the RB.162 proposed for STOL version of Boeing 737 using eight liftjets with swivel exhaust nozzles. Applications Dassault Mirage III V, 8 XRB.162-31 (5,6001b). Dornier Do31E, 8XRB.162-4D (4,4001b). VFW VAK/191B. 2XRB.162-81 (6,0001b). (RB162-81) Six-stage compressor, annular combustor, single-stage turbine. Take-off"6,0001b (with 10 per cent air bleed); pressure ratio 4.25:1; length 50in; diameter 29in; weight 3751b. RB.162 Civil single-shaft turbojet booster. Through close similarity between operational and design requirements of liftjets and booster engines, RB.162 has been readily adapted to booster role. Its sole application to date is in the Hawker Siddeley Trident 3B (1 xRB.162-86) where the booster engine is mounted above the centre Spey main turbofan. Booster improves short-field and engine-out performance, gives rapid climb out and reduces fly-over noise. (RB.162-86) Configuration same as RB.162 liftjet. Take-off 5,2501b (available —27°C to +20°C, s.l.s.); length 54in; diameter 29in; weight 5601b. Tyne Civil and military twin-spool turboprop. Sole example of a twin-spool turboprop to enter service, the Tyne for its French and German application is license-manufactured by the European Consortium comprising Hispano-Suiza, MAN Turbo, Fabrique Nation-ale and Rolls-Royce. Applications Aviation Traders Merchantman (Vanguard conversion), 4 x Tyne R Tyl Mk 506 (4,785 e.h.p.) or Tyne R Tytl Mk 512 (5,325 e.h.p.). BAC Vanguard 951, 4xTyne R Tyl Mk 506 (4,785 e.h.p.). BAC Vanguard 952, 4xTyne R Tyll Mk 512 (5,325 e.h.p.). Breguet 1150 Atlantic, 2 X Tyne R Ty20 Mk 21 (6,105 e.h.p.). Canadair CL-44D-4, 4xTyne R Tyl2 Mk 515 (5,500 e.h.p.). Canadair CL-44J & CC-106 Yukon, 4xTyne R Tyl2 Mk 515/10 (5,730 e.h.p.). Short Belfast C Mk 1, 4xTyne R Tyl2 Mk 101 (5,715 e.h.p.). Transall C-160D, 2xTyne R Ty20 Mk 22 (6,100 e.h.p.). (Tyne R Ty20) Six-stage 1-p compressor, nine-stage h-p compressor, cannular combustor with ten flame tubes, single-stage h-p turbine, three-stage 1-p turbine. Integral, front-mounted gearbox. Take-off 5,855 e.h.p.; mass flow 46.51b/sec; pressure ratio 13.5:1; length 108.7in; diameter 43.2in; weight 2,2181b. RB.108 Military single-shaft lift engine. Pioneer lift engine powering experimental V/STOL aircraft and hover rigs. Applications Dassault Balzac, 8 X RB.108. Dornier Hover Rig, 4XRB.108. EWR-Stud Hover Rig, 3XRB.108. EWR WipDe Rig, 1XRB.108. Fiat Hover Rig 2XRB.108. Short S C I , 5XRB.108. VFW SG-1262 Hover Rig, 5 x RB.108. (RB.108) Eight-stage compressor, annular combustor, single-stage turbine. Take-off 2,2101b (total, with 11 per cent air bleed); mass flow 38.851b/sec; pressure ratio 5.33:1: length 48.3in; diameter 20.8in; weight 2691b. Gazelle Military free-turbine turboshaft. Originally of Napier design, has prime application in the Westland Wessex helicopter. Applications Westland Belvedere HC.l, 2 XGazelle NGa2 Mk 101 1,465 s.h.p.). Westland Wessex HAS Mk 1, lxGazelle NGal3 Mk 161 (1,450 s.h.p.). Westland Wessex HAS Mk 3, IX Gazelle NGa22 Mk 165 (1,600 s.h.p.). Westland HAS Mk 31, lxGazelle Mk 162 (1,540 sJi.p.). (Gazelle NGa22 Mk 165) Eleven-stage compressor, tubular combustor with six flame tubes, two-stage compressor-turbine, single-stage power turbine. Integral rear-mounted gearbox. Take-off 1,600 s.h.p.; mass flow 17!61b/sec; pressure ratio 6.35:1; length 75in; diameter 33.5in; weight 8701b.
Conway RCo.42 and 43 Civil and military twin-spool turbofan. Final variants of the Conway, developed specifically to power the BAC VC10 and Super VC10. Applications BAC VC10, 4 X Conway RCo.42 Mk 540 (20,3701b). BAC VC10 C Mk 1, 4xConway RCo.43 Mk 301 (22,5001b). BAC Super VC10, 4xConway RCo.43 Mk 550 (21,8001b). (Conway RCo.43 Mk 550) Four-stage fan/l-p compressor plus four-stage i-p compressor, nine-stage h-p compressor, cannular combustor with ten flame tubes, single-stage h-p turbine, two-stage
1-p turbine. Take-off 21,8001b; b.p.r. 0 .6 :1; mass flow 3751b/see; pressure ratio 15.8:1; length 154in; diameter 50in; weight 5,1011b. Conway R.Co.17 Miltary twin-spool turbofan. Sole application is the Handley Page Victor B2 as the 20,6001b Mk 201. Conway R.Co.12 Civil twin-spool turbofan. Pioneering commercial turbofan derived from the original military engine for the Vickers V.1000. Applications Boeing 707-420, 4 x Conway R.Co.12 Mk 508 (17,5001b). Douglas DC-8 Series 40, 4XConway R.Co.12 Mk 509 (17,5001b). (Conway R.Co.12 Mk 509) Seven-stage fan/l-p compressor, nine-stage h-p compressor, cannular combustor with ten flame tubes, single-stage h-p turbine, two-stage l-p turbine. Take-off 17,0001b; b.p.r. 0.3:1; mass flow 2801b/sec; pressure ratio 14 :1 ; length 136in; diameter 42in; weight 4,5421b. RB.146 Avon 300 Military single-shaft augmented turbojet. Most powerful military Avon, introduced for later versions of the BAC Lightning. License-manufactured by Flygmotor as RM6, with Swedish afterburner, for Saab 35 Draken series. Applications BAC Lightning F6, T5 and T. Mk 55, 2 X Avon Mk 301 (12,6901b, or 16,8601b with afterburning). BAC Lightning F.53, 2xAvon Mk 302-C (11,1001b, or 16,3001b with afterburning). Avon RA.29 Civil and military single-shaft turbojet. Derived from the Avon 200 series for commercial operation. Applications Hawker Siddeley Comet 4 & 4C, 4 x Avon RA.29/l Mk 524B (10,2501b). Hawker Siddeley Comet 4B, 4 x Avon RA.29/1 Mk 525B (10,2501b). Sud-Aviation Caravelle III, 2 x Avon RA.29/3 Mk 527B (11,4001b). Sud-Aviation Caravelle VI N, 2 x Avon RA.29/3 Mk 531B (12,2001b). Sud-Aviation Caravelle VI R, 2 X Avon RA.29/3 Mk 533R (12,6001b). (Avon RA.29/1) Sixteen-stage compressor, cannular combustor, three-stage turbine. Take-off 10,2501b; pressure ratio 9.08:1; length 126in ; diameter 39in ; weight 3,3431b. RB.90 Avon 200 Military single-shaft augmented turbojet. Major military version of the Avon. License-manufactured by Fabrique Nationale, and by Flygmotor as RMS with Swedish afterburner to power Saab Lansen. Applications BAC 221, lxAvon RA.28R (14,4301b with afterburning). BAC Canberra Mk 9, 2 x Avon RA.24 Mk 206 (11,2501b). BAC Lightning F2, 3 & 5, 2xAvon RA.24R Mk 210 (11,2501b, or 14,3701b with afterburning). BAC Scimitar F l , 2 x Avon RA.24 Mk 202 (11,2501b). Hawker Siddeley Hunter Mks 9, 10 & 12, lxAvon RA.28 Mk 207 (10,1501b). Hawker Siddeley Sea Vixen FAW2, 2 X Avon RA.24 Mk 208 (11,2501b). (RB.90 Avon RA.28 Mk 208) Fifteen-stage compressor, cannular combustor, two-stage turbine. Take-off 11,2501b; length 126.9in; diameter 28in. Dart Civil and military single-shaft turboprop. Outstandingly successful turboprop, still in quantity production since starting in 1953. Applications BAC Project 201, 2 x Dart RDa.7 (2,230 e.h.p.). BAC Viscount 700, 4 X Dart RDa.6 Mk 510 (1,670 e.h.p.). BAC Viscount 800, 4xDart RDa.6 Mk 510 (1,670 e.h.p.), or Dart RDa.7 Mk 520 (1,815 ch.p.), or Dart RDa.7/1 Mk 525F (1,910 e.h.p.), or Dart RDa.7/2 Mk 530 (2,020 e.h.p.). Breguet 1050 Alize, IX Dart RDa.7 Mk 21 (2,020 e.h.p.). Cavalier Aircraft Mustang 3 Conversion, l x D a r t RDa.6 Mk 510 (1,440 s.h.p.) or Dart RDa. 7/2 Mk 529 (2,185 s.h.p.). Convair 600/640, 2 X Dart RDa.lO Mk 542^1 (3,025 e.p.h.). FairchUd Hiller F-27, 2xDar t RDa.6 Mk 511 (1,670 e.h.p.). Fairchild Hiller F-27A & F, 2xDart RDa.7 Mk 528-7E (2,105 e.h.p.). Fairchild Hiller F-27B, 2 X Dart RDa.6 Mk 514-7 (1,850 e.h.p.). Fairchild Hiller F-27J, F-227 &
Under joint development and manufacture by Rolls-Royce's Bristol Engine Division and Snecma in France, the M45H civil twin-spool turbofan has been designed to meet the economical fuel consumption requirements of Germany's VFW6I4 short-haul airliner
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