| 词条 | Lycoming TIO-541 | ||||||||||
| 释义 |
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] 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 developmentThe TIO-541 family of engines covers a range from {{convert|310|hp|kW|0|abbr=on}} to {{convert|450|hp|kW|0|abbr=on}}. 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 {{convert|450|hp|kW|0|abbr=on}} 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
Six-cylinder, turbocharged, fuel-injected, {{convert|310|hp|kW|0|abbr=on}} engine, dry weight {{convert|449|lb|kg|0|abbr=on}}, 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]
Six-cylinder, turbocharged, fuel-injected, {{convert|380|hp|kW|0|abbr=on}} engine, dry weight {{convert|595|lb|kg|0|abbr=on}}, 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]
Six-cylinder, turbocharged, fuel-injected, {{convert|380|hp|kW|0|abbr=on}} engine, dry weight {{convert|595|lb|kg|0|abbr=on}}, AiResearch T-1823 turbosupercharger, certified 16 December 1966. Similar to the -E1A4 but without the cabin pressurization venturi.[1]
Six-cylinder, turbocharged, fuel-injected, {{convert|380|hp|kW|0|abbr=on}} engine, dry weight {{convert|586|lb|kg|0|abbr=on}}, 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]
Six-cylinder, turbocharged, fuel-injected, {{convert|380|hp|kW|0|abbr=on}} engine, dry weight {{convert|584|lb|kg|0|abbr=on}}, 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]
Six-cylinder, turbocharged, fuel-injected, geared, {{convert|450|hp|kW|0|abbr=on}} engine, dry weight {{convert|663|lb|kg|0|abbr=on}}, 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]
Six-cylinder, turbocharged, fuel-injected, geared, {{convert|400|hp|kW|0|abbr=on}} engine, dry weight {{convert|703|lb|kg|0|abbr=on}}, 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]
Six-cylinder, turbocharged, fuel-injected, geared, {{convert|450|hp|kW|0|abbr=on}} engine, dry weight {{convert|706|lb|kg|0|abbr=on}}, 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]
Six-cylinder, turbocharged, fuel-injected, geared, {{convert|450|hp|kW|0|abbr=on}} engine, dry weight {{convert|710|lb|kg|0|abbr=on}}, 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]
Six-cylinder, turbocharged, fuel-injected, geared, {{convert|425|hp|kW|0|abbr=on}} engine, dry weight {{convert|706|lb|kg|0|abbr=on}}, 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]
Six-cylinder, turbocharged, fuel-injected, geared, {{convert|450|hp|kW|0|abbr=on}} engine, dry weight {{convert|714|lb|kg|0|abbr=on}}, 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
Specifications (TIO-541-A1A){{pistonspecs||ref=TYPE CERTIFICATE DATA SHEET NO. E10EA[1] |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) |length= |diameter= |width= |height= |weight=449 lb (249 kg) dry |valvetrain= |supercharger= |turbocharger=AiResearch turbosupercharger model T-1823 |fuelsystem=Bendix RSA 10AD1 |fueltype=100LL avgas |oilsystem= |coolingsystem=air-cooled |power=310 hp (233 kW) at 2575 rpm |specpower=0.57 hp/in³ (26.7 kW/L) |compression=7.30:1 |fuelcon= |specfuelcon= |oilcon= |power/weight=0.69 hp/lb (0.94 kW/kg) |designer= |reduction_gear= |general_other= |components_other= |performance_other= }} See also
References1. ^1 2 3 4 5 6 7 8 9 {{cite web|url = http://www.airweb.faa.gov/Regulatory_and_Guidance_Library/rgMakeModel.nsf/0/A584A5C24AB8B5438525670E0056C9B8?OpenDocument&Highlight=541|title = TYPE CERTIFICATE DATA SHEET NO. E10EA, Revision 7|accessdate = 2009-01-13|last = Federal Aviation Administration|authorlink = |date=April 1986}} {{Lycoming aeroengines}}2. ^1 2 3 4 5 6 7 8 {{cite web|url = http://www.airweb.faa.gov/Regulatory_and_Guidance_Library/rgMakeModel.nsf/0/74E5837A82A0F00B8525670E0056E19F?OpenDocument&Highlight=541|title = TYPE CERTIFICATE DATA SHEET NO. E19EA, Revision 4|accessdate = 2009-01-13|last = Federal Aviation Administration|authorlink = |date=April 1986}} 2 : Aircraft piston engines 1960–1969|Lycoming aircraft engines |
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