ENSIKLOPEDIA Cari Tekan Enter untuk memulai pencarian cepat. Kembali ke Ensiklopedia Arsip Wikipedia Indonesia Lycoming T53 Lycoming T53Turboshaft helicopter engine This article needs additional citations for verification. Please help improve this article by adding citations to reliable sources in this article. Unsourced material may be challenged and removed.Find sources: "Lycoming T53" – news · newspapers · books · scholar · JSTOR (November 2008) (Learn how and when to remove this message) T53 Cutaway view of an early T53 turboprop, with single stage HP and power turbinesTypeTurboshaftNational originUnited StatesManufacturerLycoming EnginesHoneywell AerospaceOzark Aeroworks LLCFirst run~1955[1]Major applicationsAH-1 CobraKaman K-MAXOV-1 MohawkUH-1 IroquoisDeveloped intoLycoming T55 The Lycoming T53, (company designation LTC-1) is a turboshaft engine used on helicopters and (as a turboprop) fixed-wing aircraft since the 1950s. It was designed at the Lycoming Turbine Engine Division in Stratford, Connecticut, by a team headed by Anselm Franz, who was the chief designer of the Junkers Jumo 004 during World War II. A much larger engine, similar in overall design, became the Lycoming T55 produced by Honeywell Aerospace. The T53 model is produced by Ozark Aeroworks LLC. Variants Military designations Lycoming T53-L-1 turboshaft engine at Steven F. Udvar-Hazy Center in Virginia, USA T53-L-1 T53-L-1A 770 hp (570 kW) T53-L-1B 860 hp (640 kW) T53-L-3 T53-L-5 960 hp (720 kW) T53-L-7 T53-L-11 1,100 hp (820 kW) T53-L-13 T53-L-13B 1,400 hp (1,000 kW) improved L-11 T53-L-701 1,400 hp (1,000 kW) turboprop variant used on Mohawk and AIDC T-CH-1 T53-L-703 1,800 hp (1,300 kW) improved durability variant of the L-13B TF12 1,150 hp (860 kW) marine gas turbine fitted to prototype hydrofoil Halobates.[2] Civil designations T5307A commercial L-7 T5309A commercial L-9A T5309B commercial L-9B T5309C similar to T5309A but with L-11 combustion chamber T5311A 1100 shp (820 kW) T5313A 1400 shp (1044 kW) commercial variant of the L-13 T5313B 1400 shp (1044 kW) commercial variant of the L-13 T5317A 1500 shp (1119 kW) improved variant of the L-13 T5317A-1 T5317B T5317BCV LTC1B-1 LTC1B-2 company designation for L-1A LTC1F-1 company designation for L-3 LTC1F-2 company designation for L-7 LTC1K-1 company designation for L-5 LTC1K-2 company designation for L-9 LTC1K-2A company designation for L-9A LTC1K-2B company designation for L-9B LTC1K-4 company designation for L-13 LTC1K-4A for tilt-wing / tilt-rotor aircraft (Canadair CL-84 Dynavert) LTC1K-4K 1550 shp (1156 kW) direct drive variant of the L-13B LTC1K-5 company designation for L-11 Kawasaki KT5311AKawasaki production for Fuji-Bell 204B helicopters Applications Aircraft AIDC T-CH-1 (T53-L-701) AIDC XC-2 Bell 204B (T5311A) Bell 205A (T5313B) Bell 205A-1 (T5313B and T5317A) Bell AH-1 Cobra (T53-L-703) Bell UH-1H Iroquois (T53-L-703) Bell XV-15 (LTC1K-4K) Canadair CL-84 Dynavert Doak VZ-4 Eagle Single (T5317A, T5317B, or T5317BCV)[3][4] F+W C-3605 Grumman OV-1D Mohawk (T53-L-701) Kaman HH-43 Huskie Kaman K-MAX (T5317A-1) Ryan VZ-3 Vertiplane Vertol VZ-2 (YT53) Railway DB Class 210, diesel railway locomotive Specifications (T53-L-701) Data from Flight International [5] General characteristicsType: Turboshaft Length: 58.4 in (1,483 mm) Diameter: 23 in (584 mm) Dry weight: 688 lb (312 kg) ComponentsCompressor: 5-stage axial and 1-stage centrifugal Combustors: reverse flow Turbine: 2-stage high pressure turbine; 2-stage power turbine PerformanceMaximum power output: 1,451 shp (1,082 kW) Overall pressure ratio: 7.4 Air mass flow: 10.7 lb/s (4.853 kg/s) Power-to-weight ratio: 2.109 hp/lb See also Related developmentLycoming T55 Related listsList of aircraft engines References ↑ "sir roy | roy dobson | managing director | 1955 | 1400 | Flight Archive". Archived from the original on 2017-05-17. ↑ Schuegenpflug, Hermann, Wilcoxson, Tony, Luz, Michael (2010). FROM THE JEFF (B) TO THE SSC AND BEYOND, TF MARINE GAS TURBINES A DEVELOPMENT STUDY. Paper Number GT2010-23659. The American Society of Mechanical Engineers. p. 2 ↑ "Eagle Single | Airframe Customizations | Eagle Copters". Retrieved 6 May 2020. ↑ "Eagle Copters Obtains U.S. FAA Certification for the Eagle Single". Retrieved 6 June 2023. ↑ Turbine Engines of the World, 1975 Gunston, Bill (2006). World Encyclopedia of Aero Engines, 5th Edition. Phoenix Mill, Gloucestershire, England, UK: Sutton Publishing Limited. p. 132. ISBN 0-7509-4479-X. External links Wikimedia Commons has media related to Lycoming T53. Honeywell T53 page Ozark Aeroworks, LLC vteLycoming aircraft enginesOpposed piston engines O-145 O-233 IO-233 O-235 O-290 O-320 O-340 O-360 (O-360 variants) IO-390 O-435 O-480 O-540 TIO-541 GSO-580 IO-580 IO-720 O-1230 Radial engines and H engines R-680 XR-7755 XH-2470 Aircraft diesel engines DEL-120 Turbofans PLF1 ALF 502/YF102 LF 507 Turboprops/Turboshafts AGT1500 LTS101/LTP101 T53 T55 Aero-derivative marine gas turbines TF-40 Joint developmentAvco (Lycoming)/Pratt & Whitney: T800-APW (Turboshaft)See also AlliedSignal Aerospace/Honeywell Aerospace vteGarrett/AlliedSignal/Honeywell aircraft enginesTurboprops/Turboshafts AGT1500* HTS900 LTS101/LTP101* T53* T55* TPE331 TPF351 Turbofans ALF 502/LF507* ATF3 F109 FX5 HTF7000 (AS907) TFE731 Joint developmentCFE Company: CFE738 (Turbofan) GE/Honeywell: LV100 (Turboshaft) ITEC: F124/TFE1042 F125 (Turbofans) LHTEC: CTS800 (Turboshaft) ATEC: T900 (Turboshaft) Note: AVCO Lycoming/Textron Lycoming engines marked with * vteUnited States military gas turbine aircraft engine designation systemTurbojets J30 J31 J32 J33 J34 J35 J36 J37 XJ38 J39 J40 XJ41 J42 J43 J44 J45 J46 J47 J48 XJ49 J51 J52 J53 J54 J55 J56 J57 J58 J59 J60 J61 J63 J65 J67 J69 J71 J73 J75 J79 J81 J83 J85 J87 J89 J91 YJ93 J95 J97 J99 J100 YJ101 J102 J400 J401 J402 J403 J700 Turboprops/Turboshafts T30 T31 T33 T34 T35 T36 T37 T38 T39 T40 T41 T42 T43 T44 T45 T46 T47 T48 T49 T50 T51 T52 T53 T54 T55 T56 (variants) T57 T58 T60 T61 T62 T63 T64 T65 T66 T67 T68 T69 T70 T71 T72 T73 T74 T76 T78 T80 T100 T101 T400 T405 T406 T407 T408 T700 T701 T702 T703 T706 T708 LHTEC T800 APW T800 T900 T901 Turbofans TF30 TF31 TF32 TF33 TF34 TF35 TF37 TF39 TF41 F100 F101 F102 F103 F104 F105 F106 F107 F108 F109 F110 F112 F113 F117 F118 F119 YF120 F121 F122 F124 F125 F126 F127 F128 F129 F130 F135 F136 F137 F138 F400 F401 F402 F404 F405 F408 F412 F414 F415 Adaptive cycle engines XA100 XA101 XA102 XA103
