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Honeywell TPE331

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Turboprop aircraft engine
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TPE331 / T76
TPE331-14
TypeTurboprop
National originUnited States
Manufacturer
First run1960
Major applications
Number built13,500+[1]
Developed intoGarrett TPF351

TheHoneywell TPE331 (military designation:T76) is aturboprop engine. It was designed in the 1950s byGarrett AiResearch, and produced since 1999 by its successorHoneywell Aerospace. The engine's power output ranges from 575 to 1,650shaft horsepower (429 to 1,230 kW).[2][3][4]

Design and development

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Garrett AiResearch designed the TPE331 from scratch in 1959 for the military.[5] "Designed as a 575-horsepower engine it was not a scaled-down version of a larger engine, as competitors were offering."[6]The TPE331 originated in 1961 as a gas turbine (the "331") to power helicopters.[6] It first went into production in 1963.[7] More than 700 had been shipped by the end of 1973.[6] It was designed to be both aturboshaft (TSE331)[8] and a turboprop (TPE331), but the turboshaft version never went into production. The first engine was produced in 1963, installed on theAero Commander in 1964 and put into production on the Aero Commander Turbo Commander in June 1965.[citation needed]

Performance

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The 715 shp TPE331-6 used in theBeechcraft 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.[9]

Variants

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Military variants (T76)

[edit]
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)

[edit]
USFAATC Variants
ModelCertified[a]
TPE331-11967-12[14]
TPE331-1U
TPE331-1UA
TPE331-21967-12[14]
TPE331-2U
TPE331-2UA
TPE331-31969-03-28
TPE331-3U1969-03-28
TPE331-3UW1969-03-28
TPE331-3W1969-03-28
TPE331-5[b]1970-05-15
TPE331-5A1988-05-04
TPE331-5AB1992-07-21
TPE331-5B1992-07-21
TPE331-5U1970-05-15
TPE331-6[c]1970-05-15
TPE331-6A1978-01-20
TPE331-6U1970-05-15
TPE331-8[d]1976-11-19
TPE331-8A1981-12-24
TPE331-91976-11-19
TPE331-9U1976-11-19
TPE331-101978-01-20
TPE331-10A1980-12-12
TPE331-10AV1996-07-19
TPE331-10B1980-12-12
TPE331-10G1984-08-14
TPE331-10GP1994-12-14
TPE331-10GR1984-08-14
TPE331-10GT1994-12-14
TPE331-10J1988-05-04
TPE331-10N1992-02-06
TPE331-10P1994-12-14
TPE331-10R1982-06-25
TPE331-10T1994-04-14
TPE331-10U1978-01-20
TPE331-10UA1982-07-29
TPE331-10UF1982-06-25
TPE331-10UG1984-08-14
TPE331-10UGR1984-08-14
TPE331-10UJ1988-05-04
TPE331-10UK1988-11-04
TPE331-10UR1983-11-14
TPE331-11U1979-09-28
TPE331-11UA1982-06-25
TPE331-121984-12-19
TPE331-12B[e]1986-12-10
TPE331-12JR1997-10-31
TPE331-12UA1988-05-04
TPE331-12UAN2014-05-09
TPE331-12UAR1987-12-18
TPE331-12UER1991-07-22
TPE331-12UHR1993-01-07
TSE331-3U[f]1970-04-30
TPE331-14A1984-04-26
TPE331-14B1984-04-26
TPE331-14F1989-05-24
TPE331-14GR1992-07-13
TPE331-14HR1992-07-13
TPE331-15AW1988-12-05
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
  1. ^Dates from FAA type certificates E4WE[10] (TPE331 model series 3, 5, 6, 8, 9, 10, 11, and 12) and E18NE[11] (series 14 and 15). No certification date information available from type certificates E3WE[12] (series 1 and 2) and E2WE[13] (series 25, 29, 43, 45, 47, 51, 55, 57, and 61).
  2. ^Powered the Rockwell Aero CommanderTurbo Commander 690,CASA 212-100,Mitsubishi MU-2N, andDornier 228.[15]
  3. ^Powered theMitsubishi MU-2S/K/L/M andBeech B-100.[15]
  4. ^Powered theCessna Conquest 441.[16]
  5. ^Powered theShorts Tucanotrainer aircraft and theCASA 212-400regional airliner.[17]
  6. ^Used on theSikorsky S-55 military helicopter.[18]
  7. ^Renamed toTPF351-20 in early 1988.[19] Was the rear-fuselage powerplant for theEmbraer/FMA CBA 123 Vector. Flown on aBoeing 720testbed 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.[20]
  8. ^Entered service on theVolpar Super Turbo 18 in February 1966.[21]

Applications

[edit]

Fitted with TPE-331s as a replacement for their original engines

[edit]

Specifications

[edit]
Cutaway view of a TPE-331

General characteristics

  • Type: Single-shaftturboprop with integralgearbox
  • Length: 46 inches (1,200 mm) (TPE331-43A),[7] 42.82 in (1,088 mm) (TPE331-10)[22]
  • Diameter: 21 inches (530 mm) (TPE331-43A)[7]
  • Dry weight: 336 lb (152 kg) (TPE331-43A),[7] 385 lb (175 kg) (TPE331-10)[22]

Components

Performance

See also

[edit]

Comparable engines

Related lists

References

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  1. ^Brecken, Steve (July 2016)."Honeywell Continues to Hone Turboprop Engine for 50th Anniversary" (Press release). Phoenix, Arizona:Honeywell Aerospace.Archived from the original on 2019-07-04.
  2. ^"TPE331 Spec Chart".Honeywell Aerospace. Archived fromthe original(PDF) on 2014-09-03. Retrieved2014-08-29.
  3. ^"TPE".Products & Services.Honeywell Aerospace. Archived fromthe original on 2010-09-08.
  4. ^"TPE331-14 Turboprop Engine"(PDF).Honeywell Aerospace. 2006-07-10. Archived fromthe original(PDF) on 2014-09-03. Retrieved2014-08-29.
  5. ^"TPE331 Engines Offers Super Performance on Dornier 228 Aircraft" (Press release). Phoenix, Arizona:Honeywell Aerospace. 2017-04-11. Archived fromthe original on 2017-12-12. Retrieved2017-12-12.
  6. ^abcSchoneberger, 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.
  7. ^abcdef"Garrett TPE331".Collection.Canadian Museum of Flight.Archived from the original on 2019-07-04.
  8. ^Wilkinson, Paul H. (1964).Aircraft engines of the World 1964/65 (20th ed.). London: Sir Isaac Pitman & Sons Ltd. p. 43.
  9. ^George, Fred (2017-01-30)."Used Aircraft Report: Beech King Air B100".Business & Commercial Aviation. Aviation Week Network.
  10. ^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)
  11. ^Honeywell (AlliedSignal, Garrett) (February 1, 2000).E18NE.Federal Aviation Administration (FAA) (Report). Type Certificate Data Sheet (9 ed.).
  12. ^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)
  13. ^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)
  14. ^abLeyes & Fleming 1999, p. 648.
  15. ^abLeyes & Fleming 1999, p. 652.
  16. ^Leyes & Fleming 1999, p. 653.
  17. ^Leyes & Fleming 1999, p. 656.
  18. ^Leyes & Fleming 1999, p. 661.
  19. ^"Garrett engine is redesignated". Regional Airline Report.Airline Executive. February 1988. p. 12.ISSN 0278-6702.
  20. ^Leyes & Fleming 1999, pp. 710–711.
  21. ^Leyes & Fleming 1999, p. 645.
  22. ^abcdef"TPE331-10 Turboprop Engine"(PDF).Honeywell Aerospace. April 2006. Archived fromthe original(PDF) on 2012-07-19.
  23. ^"TPE331-10 Turboprop Engine"(PDF).Honeywell Aerospace. February 2024.Archived(PDF) from the original on 2023-01-05.

Bibliography

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External links

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Wikimedia Commons has media related toGarrett TPE331.
Turboprops/Turboshafts
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United States military gas turbine aircraft enginedesignation system
Turbojets
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