dbo:abstract
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- The Progress D-236 was an experimental aircraft engine, a hybrid between a turbofan and a turboprop known as a propfan. Also known as the Lotarev D-236T, the three-shaft geared engine was designed in the 1980s and 1990s to power proposed propfan aircraft such as the Tupolev Tu-334, Ilyushin Il-118, and Ilyushin Il-88. Based on the core of the Ukrainian Progress D-36 turbofan, the D-236 was the first Soviet propfan, and as of 2019 it is still one of only four different unshrouded, contra-rotating propfan engines to have flown in service or in flight testing. (en)
- Д-236Т — гвинто-вентиляторний двигун Д-236 розроблений ЗМКБ «Прогрес» на базі Д-36 для перевірки ряду конструктивних рішень, які знайшли продовження в подальших проектах ЗМКБ «Прогрес». (uk)
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- 22393 (xsd:nonNegativeInteger)
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dbo:wikiPageRevisionID
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dbo:wikiPageWikiLink
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dbp:developedFrom
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dbp:firstRun
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dbp:length
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- N/A
*Width:
*Height:
*Propeller diameter: (en)
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dbp:lists
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- * List of aircraft engines (en)
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dbp:majorApplications
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dbp:manufacturer
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dbp:nationalOrigin
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dbp:numberBuilt
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dbp:power
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- during takeoff; during cruise (en)
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dbp:related
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- * Lotarev D-36
* Lotarev D-136
* Progress D-436
* Progress D-27 (en)
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dbp:seeAlso
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- * Europrop TP400
* Kuznetsov NK-12
* Kuznetsov NK-93 (en)
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dbp:similarEngines
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- * General Electric GE36
* Pratt & Whitney/Allison 578-DX
* Rolls-Royce RB3011 (en)
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dbp:specfuelcon
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dbp:type
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- dbr:Propfan
- Three-shaft geared tractor-configuration propfan (en)
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dbp:weight
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- Engine and gearbox: ; Propeller: ; Total: (en)
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rdfs:comment
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- The Progress D-236 was an experimental aircraft engine, a hybrid between a turbofan and a turboprop known as a propfan. Also known as the Lotarev D-236T, the three-shaft geared engine was designed in the 1980s and 1990s to power proposed propfan aircraft such as the Tupolev Tu-334, Ilyushin Il-118, and Ilyushin Il-88. Based on the core of the Ukrainian Progress D-36 turbofan, the D-236 was the first Soviet propfan, and as of 2019 it is still one of only four different unshrouded, contra-rotating propfan engines to have flown in service or in flight testing. (en)
- Д-236Т — гвинто-вентиляторний двигун Д-236 розроблений ЗМКБ «Прогрес» на базі Д-36 для перевірки ряду конструктивних рішень, які знайшли продовження в подальших проектах ЗМКБ «Прогрес». (uk)
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rdfs:label
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- Progress D-236 (en)
- Д-236Т (uk)
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