Honeywell TPE331
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The Honeywell TPE331 (military designation: T76) is a turboprop engine. It was designed in the 1950s by Garrett AiResearch, and produced since 1999 by its successor Honeywell Aerospace. The engine's power output ranges from 575 to 1,650 shaft horsepower (429 to 1,230 kW).[1][2][3]
Design and development
Garrett AiResearch designed the TPE331 from scratch in 1959 for the military.[4] "Designed as a 575-horsepower engine it was not a scaled-down version of a larger engine, as competitors were offering."[5] The TPE331 originated in 1961 as a gas turbine (the "331") to power helicopters.[5] It first went into production in 1963.[6] More than 700 had been shipped by the end of 1973.[5] It was designed to be both a turboshaft (TSE331)[7] and a turboprop (TPE331), but the turboshaft version never went into production. The first engine was produced in 1963, installed on the Aero Commander in 1964 and put into production on the Aero Commander Turbo Commander in June 1965.[citation needed]
Performance
The 715 shp TPE331-6 used in the Beechcraft King Air B100 has a 400 hr fuel nozzle cleaning interval, 1,800 hr hot section inspection interval, and a 5,400 hr. time between overhaul; approval is possible for 3,000 hr HSIs and 6,000 hr overhauls, and engine reserves are cheaper than for the PT6A.[8]
Variants
Military variants (T76)
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- T76-G-2
- T76-G-4
- T76-G-6
- T76-G-8
- T76-G-10
- T76-G-12
- T76-G-12A
- T76-G-14
- T76-G-16
- T76-G-410
- T76-G-411
- T76-G-416
- T76-G-417
- T76-G-418
- T76-G-419
- T76-G-420
- T76-G-421
Commercial variants (TPE331)
| Model | Certified[a] |
|---|---|
| TPE331-1 | 1967-12Lua error in package.lua at line 80: module 'Module:Footnotes/anchor_id_list' not found. |
| TPE331-1U | |
| TPE331-1UA | |
| TPE331-2 | 1967-12Lua error in package.lua at line 80: module 'Module:Footnotes/anchor_id_list' not found. |
| TPE331-2U | |
| TPE331-2UA | |
| TPE331-3 | 1969-03-28 |
| TPE331-3U | 1969-03-28 |
| TPE331-3UW | 1969-03-28 |
| TPE331-3W | 1969-03-28 |
| TPE331-5[b] | 1970-05-15 |
| TPE331-5A | 1988-05-04 |
| TPE331-5AB | 1992-07-21 |
| TPE331-5B | 1992-07-21 |
| TPE331-5U | 1970-05-15 |
| TPE331-6[c] | 1970-05-15 |
| TPE331-6A | 1978-01-20 |
| TPE331-6U | 1970-05-15 |
| TPE331-8[d] | 1976-11-19 |
| TPE331-8A | 1981-12-24 |
| TPE331-9 | 1976-11-19 |
| TPE331-9U | 1976-11-19 |
| TPE331-10 | 1978-01-20 |
| TPE331-10A | 1980-12-12 |
| TPE331-10AV | 1996-07-19 |
| TPE331-10B | 1980-12-12 |
| TPE331-10G | 1984-08-14 |
| TPE331-10GP | 1994-12-14 |
| TPE331-10GR | 1984-08-14 |
| TPE331-10GT | 1994-12-14 |
| TPE331-10J | 1988-05-04 |
| TPE331-10N | 1992-02-06 |
| TPE331-10P | 1994-12-14 |
| TPE331-10R | 1982-06-25 |
| TPE331-10T | 1994-04-14 |
| TPE331-10U | 1978-01-20 |
| TPE331-10UA | 1982-07-29 |
| TPE331-10UF | 1982-06-25 |
| TPE331-10UG | 1984-08-14 |
| TPE331-10UGR | 1984-08-14 |
| TPE331-10UJ | 1988-05-04 |
| TPE331-10UK | 1988-11-04 |
| TPE331-10UR | 1983-11-14 |
| TPE331-11U | 1979-09-28 |
| TPE331-11UA | 1982-06-25 |
| TPE331-12 | 1984-12-19 |
| TPE331-12B[e] | 1986-12-10 |
| TPE331-12JR | 1997-10-31 |
| TPE331-12UA | 1988-05-04 |
| TPE331-12UAN | 2014-05-09 |
| TPE331-12UAR | 1987-12-18 |
| TPE331-12UER | 1991-07-22 |
| TPE331-12UHR | 1993-01-07 |
| TSE331-3U[f] | 1970-04-30 |
| TPE331-14A | 1984-04-26 |
| TPE331-14B | 1984-04-26 |
| TPE331-14F | 1989-05-24 |
| TPE331-14GR | 1992-07-13 |
| TPE331-14HR | 1992-07-13 |
| TPE331-15AW | 1988-12-05 |
| TPE331-16[g] | N/A |
| TPE331-25A | |
| TPE331-25AA | |
| TPE331-25AB | |
| TPE331-25B | |
| TPE331-25C | |
| TPE331-25D | |
| TPE331-25DA | |
| TPE331-25DB | |
| TPE331-25E | |
| TPE331-25F | |
| TPE331-25FA | |
| TPE331-29A | |
| TPE331-43 | |
| TPE331-43-A | |
| TPE331-43-B | |
| TPE331-45 | |
| TPE331-47 [h] | |
| TPE331-47-A | |
| TPE331-47-B | |
| TPE331-51 | |
| TPE331-55 | |
| TPE331-55-A | |
| TPE331-55-B | |
| TPE331-57 | |
| TPE331-57-B | |
| TPE331-61 | |
| TPE331-61-A |
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- ^ Dates from FAA type certificates E4WE[9]Template:R/superscript (TPE331 model series 3, 5, 6, 8, 9, 10, 11, and 12) and E18NE[10]Template:R/superscript (series 14 and 15). No certification date information available from type certificates E3WE[11]Template:R/superscript (series 1 and 2) and E2WE[12]Template:R/superscript (series 25, 29, 43, 45, 47, 51, 55, 57, and 61).
- ^ Powered the Rockwell Aero Commander Turbo Commander 690, CASA 212-100, Mitsubishi MU-2N, and Dornier 228.Lua error in package.lua at line 80: module 'Module:Footnotes/anchor_id_list' not found.
- ^ Powered the Mitsubishi MU-2S/K/L/M and Beech B-100.Lua error in package.lua at line 80: module 'Module:Footnotes/anchor_id_list' not found.
- ^ Powered the Cessna Conquest 441.Lua error in package.lua at line 80: module 'Module:Footnotes/anchor_id_list' not found.
- ^ Powered the Shorts Tucano trainer aircraft and the CASA 212-400 regional airliner.Lua error in package.lua at line 80: module 'Module:Footnotes/anchor_id_list' not found.
- ^ Used on the Sikorsky S-55 military helicopter.Lua error in package.lua at line 80: module 'Module:Footnotes/anchor_id_list' not found.
- ^ Renamed to TPF351-20 in early 1988.[13] Was the rear-fuselage powerplant for the Embraer/FMA CBA 123 Vector. Flown on a Boeing 720 testbed aircraft and Vector prototype starting in July 1990. Development of the aircraft and engine was suspended in 1992, when the engine was nine months from certification.Lua error in package.lua at line 80: module 'Module:Footnotes/anchor_id_list' not found.
- ^ Entered service on the Volpar Super Turbo 18 in February 1966.Lua error in package.lua at line 80: module 'Module:Footnotes/anchor_id_list' not found.
Applications
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Fitted with TPE-331s as a replacement for their original engines
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Specifications
General characteristics
- Type: Single-shaft turboprop with integral gearbox
- Length: 46 inches (1,200 mm) (TPE331-43A),[6] 42.82 in (1,088 mm) (TPE331-10)[14]
- Diameter: 21 inches (530 mm) (TPE331-43A)[6]
- Dry weight: 336 lb (152 kg) (TPE331-43A),[6] 385 lb (175 kg) (TPE331-10)[14]
Components
- Compressor: Two-stage centrifugal
- Combustors: Reverse annular
- Turbine: Three-stage axial
- Fuel type: Jet A, Jet B, Jet A-1, JP-8, JP-1, JP-4, JP-5, JP8+100[15]
Performance
- Maximum power output: 575 hp (429 kW) (TPE331-43A),[6] 940 hp (700 kW) (TPE331-10)[14]
- Overall pressure ratio: 10.55:1 (TPE331-10)[14]
- Specific fuel consumption: 0.534 lb/(hp⋅h) (325 g/kWh) (TPE331-10)[14]
- Power-to-weight ratio: 1.71 hp/lb (2.81 kW/kg) (TPE331-43A),[6] 2.44 hp/lb (4.01 kW/kg) (TPE331-10)[14]
See also
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Related lists
References
- ^ Page Module:Citation/CS1/styles.css has no content."TPE331 Spec Chart". Honeywell Aerospace. Archived from the original (PDF) on 2014-09-03. Retrieved 2014-08-29.
- ^ Page Module:Citation/CS1/styles.css has no content."TPE". Products & Services. Honeywell Aerospace. Archived from the original on 2010-09-08.
- ^ Page Module:Citation/CS1/styles.css has no content."TPE331-14 Turboprop Engine" (PDF). Honeywell Aerospace. 2006-07-10. Archived from the original (PDF) on 2014-09-03. Retrieved 2014-08-29.
- ^ Page Module:Citation/CS1/styles.css has no content."TPE331 Engines Offers Super Performance on Dornier 228 Aircraft" (Press release). Phoenix, Arizona: Honeywell Aerospace. 2017-04-11. Archived from the original on 2017-12-12. Retrieved 2017-12-12.
- ^ a b c Page Module:Citation/CS1/styles.css has no content.Schoneberger, William A.; Scholl, Robert R. H. (1985). Out of Thin Air: Garrett's First 50 Years. Garrett Corporation. pp. 153, 174–175, 203. ISBN 9780961702908.
- ^ a b c d e f Page Module:Citation/CS1/styles.css has no content."Garrett TPE331". Collection. Canadian Museum of Flight. Archived from the original on 2019-07-04.
- ^ Page Module:Citation/CS1/styles.css has no content.Wilkinson, Paul H. (1964). Aircraft engines of the World 1964/65 (20th ed.). London: Sir Isaac Pitman & Sons Ltd. p. 43.
- ^ Page Module:Citation/CS1/styles.css has no content.George, Fred (2017-01-30). "Used Aircraft Report: Beech King Air B100". Business & Commercial Aviation. Aviation Week Network.
- ^ Page Module:Citation/CS1/styles.css has no content.Honeywell (AlliedSignal, Garrett, AiResearch) (May 22, 2014). E4WE. Federal Aviation Administration (FAA) (Report). Type Certificate Data Sheet (34 ed.).
{{cite report}}: CS1 maint: multiple names: authors list (link) - ^ Page Module:Citation/CS1/styles.css has no content.Honeywell (AlliedSignal, Garrett) (February 1, 2000). E18NE. Federal Aviation Administration (FAA) (Report). Type Certificate Data Sheet (9 ed.).
- ^ Page Module:Citation/CS1/styles.css has no content.Honeywell (AlliedSignal, Garrett, AiResearch) (February 1, 2000). E3WE. Federal Aviation Administration (FAA) (Report). Type Certificate Data Sheet (8 ed.).
{{cite report}}: CS1 maint: multiple names: authors list (link) - ^ Page Module:Citation/CS1/styles.css has no content.Honeywell (AlliedSignal, Garrett, AiResearch) (February 1, 2000). E2WE. Federal Aviation Administration (FAA) (Report). Type Certificate Data Sheet (8 ed.).
{{cite report}}: CS1 maint: multiple names: authors list (link) - ^ Page Module:Citation/CS1/styles.css has no content."Garrett engine is redesignated". Regional Airline Report. Airline Executive. February 1988. p. 12. ISSN 0278-6702.
- ^ a b c d e f Page Module:Citation/CS1/styles.css has no content."TPE331-10 Turboprop Engine" (PDF). Honeywell Aerospace. April 2006. Archived from the original (PDF) on 2012-07-19.
- ^ Page Module:Citation/CS1/styles.css has no content."TPE331-10 Turboprop Engine" (PDF). Honeywell Aerospace. February 2024. Archived (PDF) from the original on 2023-01-05.
Bibliography
Page Template:Refbegin/styles.css has no content.
- Page Module:Citation/CS1/styles.css has no content.Leyes, Richard A., II; Fleming, William A. (1999). [[[:Template:GBurl]] The history of North American small gas turbine aircraft engines]. Reston, VA: National Air and Space Museum and American Institute of Aeronautics and Astronautics (AIAA). pp. [[[:Template:GBurl]] 632]–[[[:Template:GBurl]] 661]. ISBN 1-56347-332-1. OCLC 247550535.
{{cite book}}: Check|url=value (help)CS1 maint: multiple names: authors list (link) - Page Module:Citation/CS1/styles.css has no content.McClellan, J. Mac (July 1983). [[[:Template:GBurl]] "Turboprop progress: Garrett stakes its fortune on engines that offer reliability with minimum maintenance"]. Flying. Vol. 110, no. 7. pp. 31–32. ISSN 0015-4806.
{{cite magazine}}: Check|url=value (help) - Page Module:Citation/CS1/styles.css has no content.Frignac, J-P.; Privoznik, E. J. (March 12–15, 1979). The growth and evolution of the TPE331. Gas Turbine Conference & Exhibit & Solar Energy Conference. doi:10.1115/79-GT-164. ISBN 978-0-7918-7968-9. OCLC 8518974705.
External links
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Wikimedia Commons has media related to [[commons:Template:If then show|Template:If then show]].
- TPE 331 Cost Protection Programs
- TPE 331 Engine Conversions
- Power and fuel flow versus altitude and speed, for version 10. (Archive)
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