Английская Википедия:Continental O-300

Материал из Онлайн справочника
Версия от 09:41, 21 февраля 2024; EducationBot (обсуждение | вклад) (Новая страница: «{{Английская Википедия/Панель перехода}} {{Short description|American piston aircraft engine}} {{Use dmy dates|date=July 2022}} {{Use American English|date=July 2022}} <!-- This article is a part of Wikipedia:WikiProject Aircraft. Please see Wikipedia:WikiProject Aircraft/page content for recommended layout. --> {|{{Infobox Aircraft Begin |name= O-300 |image = Rolls-Royce Continental O-300.JPG |caption = Rolls-Ro...»)
(разн.) ← Предыдущая версия | Текущая версия (разн.) | Следующая версия → (разн.)
Перейти к навигацииПерейти к поиску

Шаблон:Short description Шаблон:Use dmy dates Шаблон:Use American English

Шаблон:Infobox Aircraft Engine

The Continental O-300 and the C145 are a family of air-cooled flat-6 aircraft piston engines built by Teledyne Continental Motors.[1]

First produced in 1947, versions were still in production Шаблон:As of. It was produced under licence in the United Kingdom by Rolls-Royce in the 1960s.

Development

Файл:Field maintenance on a 1956 model Cessna 172.JPG
Continental O-300 engine installation in a Cessna 172

The C-145 was developed from the Шаблон:Convert C-125 engine. Both powerplants share the same crankcase, although the C-145 produces an additional Шаблон:Convert through a longer piston stroke, higher compression ratio of 7.0:1 and different carburetor jetting.[1]

The O-300 is a modernized C-145 and retains the same weight, dimensions, bore, stroke, compression ratio, displacement and output power of the earlier engine.[1]

GO-300

The GO-300 employs a reduction gearbox, so that the engine turns at 3200 rpm to produce a propeller rpm of 2400. The GO-300 produces Шаблон:Convert whereas the ungeared O-300 produces Шаблон:Convert.[1]

The GO-300 engine has a TBO (Time Between Overhaul) of 1200 hours, while 1800 hours is the standard for ungeared O-300 engines. The GO-300 engine suffered reliability problems as a result of pilots mishandling the engine and operating it at too low an engine rpm. This caused the Cessna Skylark to develop a poor reputation for engine reliability. Many Skylarks flying today have been converted to different, larger-displacement, direct-drive engines.[2]

Variants

C145
Six-cylinder, Шаблон:Convert, direct-drive engine.[1]
C145-2
O-300
Modernized C145, Шаблон:Convert, direct drive engine.[1]
O-300-A
O-300-B
O-300-C
O-300-D
O-300-E
Limited production for the Beagle B.218X twin that never went into production[3]
GO-300
Geared O-300, Шаблон:Convert at 3200 crankshaft rpm, 2400 propeller rpm.[1]
GO-300-A
GO-300-C
GO-300-D
Voyager 300
Liquid-cooled, fuel-injected version developing Шаблон:Convert at 2,700 rpm.
Rolls-Royce-Continental O-300
Licence production in the United Kingdom.

Applications

Файл:Cessna175ASkylark03.jpg
Cessna 175 showing the cowling bulge behind the propeller hub created by the GO-300 reduction gearbox

O-300

GO-300

Voyager 300

Specifications (O-300)

Reference: Engines for Homebuilt Aircraft & Ultralights[1] Шаблон:Pistonspecs

See also

Шаблон:Aircontent

References

Шаблон:Commons category Шаблон:Reflist

Шаблон:Continental aeroengines Шаблон:US military piston aeroengines

  1. 1,0 1,1 1,2 1,3 1,4 1,5 1,6 1,7 Christy, Joe: Engines for Homebuilt Aircraft & Ultralights, pages 60-63. TAB Books, 1983. Шаблон:ISBN
  2. Шаблон:Cite web
  3. Flight Global, 21 March 1963, p. 399
  4. Шаблон:Cite web