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Lycoming TIO-541

The Lycoming TIO-541 engine is a turbocharged, fuel-injected, horizontally opposed, six-cylinder aircraft engine featuring three cylinders per side, manufactured by Lycoming Engines.[1][2]

TIO-541
Lycoming TIO-541
Type Piston aero-engine
National origin United States
Manufacturer Lycoming Engines
First run 1963
Major applications Beechcraft Duke
Beechcraft Baron
Produced 1965–present
Developed from Lycoming O-540

The TIO-541 family of engines includes the TIGO-541 turbocharged, fuel-injected, geared, horizontally opposed engine.[2]

There is no carburetted, non-turbocharged version of the engine, which would have been designated O-541 and therefore the base model is the TIO-541.[1]

Design and development

The TIO-541 family of engines covers a range from 310 hp (231 kW) to 450 hp (336 kW). The engine has a fuel injection system which meters fuel in proportion to the induction airflow. The engine has a displacement of 541.5 cubic inches (8.87 litres) and produces a maximum of 450 hp (336 kW) in its TIGO-541 version. The cylinders have air-cooled heads.[1][2]

The first TIO-541-A1A was type certified on 23 February 1965 on the regulatory basis of CAR 13 effective 15 June 1956 as amended to 13-1 through 13-4.[1]

Variants

TIO-541-A1A
Six-cylinder, turbocharged, fuel-injected, 310 hp (231 kW) engine, dry weight 449 lb (204 kg), AiResearch T-1823 turbosupercharger, certified 23 February 1965. Has top induction, down exhaust and side-mounted accessory drives. Provisions for a single-acting, controllable-pitch propeller and internal piston cooling oil jets.[1]
TIO-541-E1A4
Six-cylinder, turbocharged, fuel-injected, 380 hp (283 kW) engine, dry weight 595 lb (270 kg), AiResearch T-1823 turbosupercharger, certified 16 December 1966. Similar to the -A1A but with higher horsepower rating, different cylinder heads, cam shaft, crankshaft and extra counterweights. Incorporates cabin pressurization venturi.[1]
TIO-541-E1B4
Six-cylinder, turbocharged, fuel-injected, 380 hp (283 kW) engine, dry weight 595 lb (270 kg), AiResearch T-1823 turbosupercharger, certified 16 December 1966. Similar to the -E1A4 but without the cabin pressurization venturi.[1]
TIO-541-E1C4
Six-cylinder, turbocharged, fuel-injected, 380 hp (283 kW) engine, dry weight 586 lb (266 kg), AiResearch T-1879 turbosupercharger, certified 21 October 1969. Similar to the -E1A4 but with a different turbosupercharger with cast bracket, cast transition and a separate wastegate.[1]
TIO-541-E1D4
Six-cylinder, turbocharged, fuel-injected, 380 hp (283 kW) engine, dry weight 584 lb (265 kg), AiResearch T-1879 turbosupercharger, certified 21 October 1969. Similar to the -E1B4 but with a different turbosupercharger with cast bracket, cast transition and a separate wastegate.[1]
TIGO-541-B1A
Six-cylinder, turbocharged, fuel-injected, geared, 450 hp (336 kW) engine, dry weight 663 lb (301 kg), AiResearch T-1879 turbosupercharger, certified 12 February 1970. Similar to the -C1A but with a higher power rating and without provisions for cabin bleed air.[2]
TIGO-541-C1A
Six-cylinder, turbocharged, fuel-injected, geared, 400 hp (298 kW) engine, dry weight 703 lb (319 kg), AiResearch T-1879 turbosupercharger, certified 19 November 1968. Has internal piston cooling oil jets, side-mounted accessory drives and a single oil supply from the propeller governor. Provisions for a reverse-pitch propeller control.[2]
TIGO-541-D1A
Six-cylinder, turbocharged, fuel-injected, geared, 450 hp (336 kW) engine, dry weight 706 lb (320 kg), AiResearch T-18A21 turbosupercharger, certified 26 June 1969. Similar to the -C1A but with a higher power rating and a different turbocharger with provisions for cabin bleed air.[2]
TIGO-541-D1B
Six-cylinder, turbocharged, fuel-injected, geared, 450 hp (336 kW) engine, dry weight 710 lb (322 kg), AiResearch T-18A51 turbosupercharger, certified 3 December 1976. Similar to the -D1A but with an integral wastegate turbocharger and a revised exhaust system and with low drag cylinders.[2]
TIGO-541-E1A
Six-cylinder, turbocharged, fuel-injected, geared, 425 hp (317 kW) engine, dry weight 706 lb (320 kg), AiResearch T-18A21 turbosupercharger, certified 26 June 1969. Similar to the -D1A but with a lower power rating, different turbocharger spring rate and a variable absolute pressure controller.[2]
TIGO-541-G1AD
Six-cylinder, turbocharged, fuel-injected, geared, 450 hp (336 kW) engine, dry weight 714 lb (324 kg), AiResearch T-18A21 turbosupercharger, certified 1 May 1975. Similar to the -D1A but it includes an intercooler, a dual magneto and a fuel injector with fuel head enrichment.[2]

Applications

TIO-541
TIGO-541

Specifications (TIO-541-A1A)

Data from TYPE CERTIFICATE DATA SHEET NO. E10EA[1]

General characteristics

  • Type: Six-cylinder, air-cooled, horizontally opposed, direct-drive, fuel-injected, turbosupercharged aircraft engine
  • Bore: 5.125 in (130 mm)
  • Stroke: 4.375 (111 mm)
  • Displacement: 541.5 in³ (8.87 litres)
  • Dry weight: 449 lb (249 kg) dry

Components

  • Turbocharger: AiResearch turbosupercharger model T-1823
  • Fuel system: Bendix RSA 10AD1
  • Fuel type: 100LL avgas
  • Cooling system: air-cooled

Performance

See also

References

  1. ^ a b c d e f g h i j Federal Aviation Administration (April 1986). "TYPE CERTIFICATE DATA SHEET NO. E10EA, Revision 7". Retrieved 2009-01-13.
  2. ^ a b c d e f g h i Federal Aviation Administration (April 1986). "TYPE CERTIFICATE DATA SHEET NO. E19EA, Revision 4". Retrieved 2009-01-13.

lycoming, engine, turbocharged, fuel, injected, horizontally, opposed, cylinder, aircraft, engine, featuring, three, cylinders, side, manufactured, lycoming, engines, 541type, piston, aero, enginenational, origin, united, statesmanufacturer, lycoming, enginesf. The Lycoming TIO 541 engine is a turbocharged fuel injected horizontally opposed six cylinder aircraft engine featuring three cylinders per side manufactured by Lycoming Engines 1 2 TIO 541Lycoming TIO 541Type Piston aero engineNational origin United StatesManufacturer Lycoming EnginesFirst run 1963Major applications Beechcraft DukeBeechcraft BaronProduced 1965 presentDeveloped from Lycoming O 540The TIO 541 family of engines includes the TIGO 541 turbocharged fuel injected geared horizontally opposed engine 2 There is no carburetted non turbocharged version of the engine which would have been designated O 541 and therefore the base model is the TIO 541 1 Contents 1 Design and development 2 Variants 3 Applications 4 Specifications TIO 541 A1A 4 1 General characteristics 4 2 Components 4 3 Performance 5 See also 6 ReferencesDesign and development EditThe TIO 541 family of engines covers a range from 310 hp 231 kW to 450 hp 336 kW The engine has a fuel injection system which meters fuel in proportion to the induction airflow The engine has a displacement of 541 5 cubic inches 8 87 litres and produces a maximum of 450 hp 336 kW in its TIGO 541 version The cylinders have air cooled heads 1 2 The first TIO 541 A1A was type certified on 23 February 1965 on the regulatory basis of CAR 13 effective 15 June 1956 as amended to 13 1 through 13 4 1 Variants EditTIO 541 A1A Six cylinder turbocharged fuel injected 310 hp 231 kW engine dry weight 449 lb 204 kg AiResearch T 1823 turbosupercharger certified 23 February 1965 Has top induction down exhaust and side mounted accessory drives Provisions for a single acting controllable pitch propeller and internal piston cooling oil jets 1 TIO 541 E1A4 Six cylinder turbocharged fuel injected 380 hp 283 kW engine dry weight 595 lb 270 kg AiResearch T 1823 turbosupercharger certified 16 December 1966 Similar to the A1A but with higher horsepower rating different cylinder heads cam shaft crankshaft and extra counterweights Incorporates cabin pressurization venturi 1 TIO 541 E1B4 Six cylinder turbocharged fuel injected 380 hp 283 kW engine dry weight 595 lb 270 kg AiResearch T 1823 turbosupercharger certified 16 December 1966 Similar to the E1A4 but without the cabin pressurization venturi 1 TIO 541 E1C4 Six cylinder turbocharged fuel injected 380 hp 283 kW engine dry weight 586 lb 266 kg AiResearch T 1879 turbosupercharger certified 21 October 1969 Similar to the E1A4 but with a different turbosupercharger with cast bracket cast transition and a separate wastegate 1 TIO 541 E1D4 Six cylinder turbocharged fuel injected 380 hp 283 kW engine dry weight 584 lb 265 kg AiResearch T 1879 turbosupercharger certified 21 October 1969 Similar to the E1B4 but with a different turbosupercharger with cast bracket cast transition and a separate wastegate 1 TIGO 541 B1A Six cylinder turbocharged fuel injected geared 450 hp 336 kW engine dry weight 663 lb 301 kg AiResearch T 1879 turbosupercharger certified 12 February 1970 Similar to the C1A but with a higher power rating and without provisions for cabin bleed air 2 TIGO 541 C1A Six cylinder turbocharged fuel injected geared 400 hp 298 kW engine dry weight 703 lb 319 kg AiResearch T 1879 turbosupercharger certified 19 November 1968 Has internal piston cooling oil jets side mounted accessory drives and a single oil supply from the propeller governor Provisions for a reverse pitch propeller control 2 TIGO 541 D1A Six cylinder turbocharged fuel injected geared 450 hp 336 kW engine dry weight 706 lb 320 kg AiResearch T 18A21 turbosupercharger certified 26 June 1969 Similar to the C1A but with a higher power rating and a different turbocharger with provisions for cabin bleed air 2 TIGO 541 D1B Six cylinder turbocharged fuel injected geared 450 hp 336 kW engine dry weight 710 lb 322 kg AiResearch T 18A51 turbosupercharger certified 3 December 1976 Similar to the D1A but with an integral wastegate turbocharger and a revised exhaust system and with low drag cylinders 2 TIGO 541 E1A Six cylinder turbocharged fuel injected geared 425 hp 317 kW engine dry weight 706 lb 320 kg AiResearch T 18A21 turbosupercharger certified 26 June 1969 Similar to the D1A but with a lower power rating different turbocharger spring rate and a variable absolute pressure controller 2 TIGO 541 G1AD Six cylinder turbocharged fuel injected geared 450 hp 336 kW engine dry weight 714 lb 324 kg AiResearch T 18A21 turbosupercharger certified 1 May 1975 Similar to the D1A but it includes an intercooler a dual magneto and a fuel injector with fuel head enrichment 2 Applications EditTIO 541Beechcraft Baron Beechcraft Duke Mooney Mustang Moynet 360 6 JupiterTIGO 541Piper PA 31P 425 Navajo Norman Dube Aerocruiser 450 TurboSpecifications TIO 541 A1A EditData from TYPE CERTIFICATE DATA SHEET NO E10EA 1 General characteristics Type Six cylinder air cooled horizontally opposed direct drive fuel injected turbosupercharged aircraft engine Bore 5 125 in 130 mm Stroke 4 375 111 mm Displacement 541 5 in 8 87 litres Dry weight 449 lb 249 kg dryComponents Turbocharger AiResearch turbosupercharger model T 1823 Fuel system Bendix RSA 10AD1 Fuel type 100LL avgas Cooling system air cooledPerformance Power output 310 hp 233 kW at 2575 rpm Specific power 0 57 hp in 26 7 kW L Compression ratio 7 30 1 Power to weight ratio 0 69 hp lb 0 94 kW kg See also EditList of aircraft enginesReferences Edit Wikimedia Commons has media related to Lycoming TIO 541 a b c d e f g h i j Federal Aviation Administration April 1986 TYPE CERTIFICATE DATA SHEET NO E10EA Revision 7 Retrieved 2009 01 13 a b c d e f g h i Federal Aviation Administration April 1986 TYPE CERTIFICATE DATA SHEET NO E19EA Revision 4 Retrieved 2009 01 13 Retrieved from https en wikipedia org w index php title Lycoming TIO 541 amp oldid 1020026193, wikipedia, wiki, book, books, library,

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