Cosmos Mercury: Difference between revisions
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|ref= |
|ref=British Piston Engines and their Aircraft<ref name= "Lumsden p.92"/>, Jane's All the World's Aircraft 1919<ref name=JAWA1919>Janes 1919, p.p.63b-65b</ref> |
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|type=14-cylinder air-cooled two-row [[radial engine]] |
|type=14-cylinder air-cooled two-row [[radial engine]] |
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|bore=4.375 |
|bore={{cvt|4.375|in|0}} |
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|stroke=5.8 |
|stroke={{cvt|5.8|in|0}} |
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|displacement=1 |
|displacement={{cvt|1223|cuin|l|1}} |
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|length= |
|length= |
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|diameter= |
|diameter={{cvt|41.625|in|0}} |
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|width= |
|width= |
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|height= |
|height= |
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|weight={{cvt|582|lb|0}} including synchronisation gear |
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|weight= |
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|valvetrain=2 valves per cylinder, [[poppet valve]] |
|valvetrain=2 valves per cylinder, [[poppet valve]] |
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|supercharger= |
|supercharger= |
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|oilsystem= |
|oilsystem= |
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|coolingsystem=Air-cooled |
|coolingsystem=Air-cooled |
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|power=<br> |
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:'''Maximum''' {{cvt|347|hp|0}} at 2,000 rpm at sea level |
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:'''Normal''' {{cvt|315|hp|0}} at 1,800 rpm at sea level |
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|specpower= |
|specpower= |
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|compression=5.3:1 |
|compression=5.3:1 |
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|oilcon= |
|oilcon= |
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|power/weight= |
|power/weight= |
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| designer = [[Roy Fedden]] |
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| reduction_gear = |
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| general_other = |
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| components_other = 2x M.L. 7-cylinder magnetoes delivering sparks through a 14-cylinder Remy distributor with coil. |
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| performance_other = |
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===Bibliography=== |
===Bibliography=== |
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{{refbegin}} |
{{refbegin}} |
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* Gunston |
* {{cite book |last1=Gunston |first1=Bill |title=World Encyclopaedia of Aero Engines |year=1989 |publisher=Patrick Stephens Limited |location=Cambridge, England |isbn=978-1-85260-163-8 |edition=2nd |page=44}} |
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* Lumsden |
* {{cite book |last1=Lumsden |first1=Alec |title=British Piston Engines and their Aircraft |year=2003 |publisher=Airlife Publishing |location=Marlborough, Wiltshire |isbn=978-1-85310-294-3 |page=92 }} |
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* {{cite book |title=Jane's All the World's Aircraft 1919 |editor1-last=Grey |editor1-first=C.G. |edition=Facsimile |year=1969 |publisher=David & Charles Limited |location=London |isbn=07153-4647-4 |pages=63b-65b}} |
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* {{cite journal |date=July 3, 1919 |title=The Cosmos Aero Engines |journal=[[Flight (magazine)|Flight]] |volume=XI |issue=27 |id=No. 549 |pages=869–871}} |
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{{refend}} |
{{refend}} |
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==External links== |
==External links== |
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<!--Dead link[http://www.flightglobal.com/pdfarchive/view/1919/1919%20-%200871.html page 871].--> |
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*{{cite journal |date=July 3, 1919 |title=The Cosmos Aero Engines |format=PDF |journal=[[Flight (magazine)|Flight]] |volume=XI |issue=27 |id=No. 549 |pages=869–871 |url=http://www.flightglobal.com/pdfarchive/view/1919/1919%20-%200869.html |accessdate=January 12, 2011 }} Contemporary article on Cosmos Engineering's air-cooled radial engines. Photos of the Mercury are on page 869, and a short technical description is on [http://www.flightglobal.com/pdfarchive/view/1919/1919%20-%200871.html page 871]. |
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*[http://www.flightglobal.com/pdfarchive/view/1919/1919%20-%200675.html ''Flight'' magazine, 22 May 1919 - Flightglobal.com] |
<!--Dead link*[http://www.flightglobal.com/pdfarchive/view/1919/1919%20-%200675.html ''Flight'' magazine, 22 May 1919 - Flightglobal.com]--> |
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*[http://www.flightglobal.com/pdfarchive/view/1960/1960%20-%200208.html ''Flight'' magazine, 12 February 1960 - Flightglobal.com] |
<!--Dead link*[http://www.flightglobal.com/pdfarchive/view/1960/1960%20-%200208.html ''Flight'' magazine, 12 February 1960 - Flightglobal.com]--> |
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* |
* {{cite web |title=World War I late ventures - Cosmos Mercury |url=http://www.aviationarchive.org.uk/stories/pages.php?enum=GE122&pnum=13&maxp=15 |website=Aviationarchive.org |access-date=20 December 2020 |archive-url=https://web.archive.org/web/20110611232905/http://www.aviationarchive.org.uk/stories/pages.php?enum=GE122&pnum=13&maxp=15 |archive-date=11 June 2011}} |
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{{Cosmos aeroengines}} |
{{Cosmos aeroengines}} |
Revision as of 10:04, 20 December 2020
Mercury | |
---|---|
The Cosmos Mercury | |
Type | Radial aero engine |
Manufacturer | Cosmos Engineering Brazil Straker |
Designer | Roy Fedden |
First run | July Template:Avyear |
Major applications | Bristol Scout F |
- For the 1926 nine-cylinder radial engine see Bristol Mercury
The Cosmos Mercury was a fourteen-cylinder twin-row air-cooled radial aeroengine. Designed by Roy Fedden of Cosmos Engineering, it was built in the United Kingdom in 1917. It produced 347 horsepower (259 kW). It did not enter production; a large order was cancelled due to the Armistice.
Design and development
Built at Bristol by Brazil-Straker under the direction of Roy Fedden, the Mercury featured an unusual crankshaft and connecting rod arrangement that dispensed with the more normal design of a single master rod linking to individual rods for each cylinder. It was said to run well without vibration and set an unofficial time to climb record while fitted to a Bristol 21A Scout F.1, the aircraft achieving 10,000 ft (3,000 m) in 5.4 minutes and 20,000 ft (6,000 m) in 16.25 minutes.[1]
An Admiralty order for 200 engines was placed in 1917 but was later cancelled by Lord Weir due to the end of World War I, it is also stated that Lord Weir had a preference for the ABC Dragonfly.[2]
The name was re-used by Fedden for the later nine-cylinder Bristol Mercury radial engine.
Applications
Specifications (Mercury)
Data from British Piston Engines and their Aircraft[1], Jane's All the World's Aircraft 1919[3]
General characteristics
- Type: 14-cylinder air-cooled two-row radial engine
- Bore: 4.375 in (111 mm)
- Stroke: 5.8 in (147 mm)
- Displacement: 1,223 cu in (20.0 L)
- Diameter: 41.625 in (1,057 mm)
- Dry weight: 582 lb (264 kg) including synchronisation gear
- Designer: Roy Fedden
Components
- Valvetrain: 2 valves per cylinder, poppet valve
- Fuel type: Petrol
- Cooling system: Air-cooled
- 2x M.L. 7-cylinder magnetoes delivering sparks through a 14-cylinder Remy distributor with coil.
Performance
- Power output:
- Maximum 347 hp (259 kW) at 2,000 rpm at sea level
- Normal 315 hp (235 kW) at 1,800 rpm at sea level
- Compression ratio: 5.3:1
See also
Comparable engines
Related lists
References
Notes
Bibliography
- Gunston, Bill (1989). World Encyclopaedia of Aero Engines (2nd ed.). Cambridge, England: Patrick Stephens Limited. p. 44. ISBN 978-1-85260-163-8.
- Lumsden, Alec (2003). British Piston Engines and their Aircraft. Marlborough, Wiltshire: Airlife Publishing. p. 92. ISBN 978-1-85310-294-3.
- Grey, C.G., ed. (1969). Jane's All the World's Aircraft 1919 (Facsimile ed.). London: David & Charles Limited. pp. 63b – 65b. ISBN 07153-4647-4.
- "The Cosmos Aero Engines". Flight. XI (27): 869–871. July 3, 1919. No. 549.
External links
- "World War I late ventures - Cosmos Mercury". Aviationarchive.org. Archived from the original on 11 June 2011. Retrieved 20 December 2020.