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词条 Supermarine Swan
释义

  1. Design and development

  2. Operators

  3. Specifications

  4. See also

  5. References

{{Use dmy dates|date=November 2017}}{{Use British English|date=November 2017}}
name = Swanimage = Supermarine Swan.jpgcaption = Prototype (N175) with landing gear at Woolston, Southampton.

}}{{Infobox Aircraft Type

type = Flying boatmanufacturer = Supermarinedesigner = R. J. Mitchellfirst flight = 25 March 1924introduced = 1926retired = 1927status =primary user = Imperial Airwaysmore users = Marine Aircraft Experimental Establishmentproduced = number built = 1unit cost =developed from =variants with their own articles = Supermarine Southampton
}}

The Supermarine Swan was a 1920s British experimental amphibian aircraft built by Supermarine at Woolston. Only one was built and it was used for a passenger service between England and France.

Design and development

The Swan was designed by R. J. Mitchell, chief designer at Supermarine as an experimental wooden twin-engined biplane amphibian aircraft, in parallel with the Supermarine Scylla design for a replacement for the Royal Air Force's Felixstowe F5s.[1]

First flown on 25 March 1924 (as serial N175), the Swan was powered by two 350 hp (261 kW) Rolls-Royce Eagle IX engines. It was re-engined with two 450 hp (336 kW) Napier Lion engines and had the landing gear removed for evaluation at the Marine Aircraft Experimental Establishment in August 1924. In 1926, it was registered G-EBJY and loaned to Imperial Airways as a flying boat with accommodation for 10 passengers until it was scrapped in 1927.

Operators

{{UK}}
  • Marine Aircraft Experimental Establishment
  • Imperial Airways

Specifications

{{Aircraft specs
|ref=[2][3][4]
|prime units?= met


|genhide=
|crew= 2
|capacity= 10 passengers, or 1352 kg (2982 lbs.) of cargo
|length m= 14.78
|length ft=
|length in=
|span m= 20.93
|span ft=
|span in=
|height m= 5.57
|height ft=
|height in=
|wing area sqm= 117.6
|wing area sqft=
|empty weight kg=
|empty weight lb= 10114
|gross weight kg=
|gross weight lb= 13710
|fuel capacity=


|eng1 number= 2
|eng1 name= Napier Lion IIB
|eng1 type= inline piston
|eng1 kw= 336
|eng1 hp=
|eng1 shp=
|prop blade number=
|prop name=
|prop dia m=
|prop dia ft=
|prop dia in=


|perfhide=
|max speed kmh= 175
|max speed mph=
|max speed kts=
|cruise speed kmh=
|cruise speed mph= 92
|cruise speed kts=
|stall speed kmh=
|stall speed mph= 45
|stall speed kts=
|stall speed note=
|range km=
|range miles= 300
|range nmi=
|ceiling m= 3110
|ceiling ft=
|climb rate ms=
|climb rate ftmin= 510
|wing loading kg/m2=
|wing loading lb/sqft= 10.78
|wing loading note=
|more performance=
|avionics=
}}

See also

{{Aircontent
|related =
  • Supermarine Scylla
  • Supermarine Southampton

|similar aircraft =
  • Felixstowe F.5
  • English Electric Kingston
  • Hiro H1H
  • Naval Aircraft Factory PN

|lists =
  • List of seaplanes and amphibious aircraft

|see also =
}}

References

{{commons category|Supermarine}}
1. ^Andrews and Morgan 1987, p.87
2. ^Andrews and Morgan 1987, p.95.
3. ^{{cite web |url=https://www.flightglobal.com/pdfarchive/view/1926/1926%20-%200213.html |last1=Simmonds|first1=O.E.|title=Development of Civil Aircraft|journal=Flight|date=25 March 1926|volume=XVIII|issue=12|pages=180-182|accessdate=21 December 2016|ref=Flight}}
4. ^{{cite journal|journal=Air Pictorial and Air Reserve Gazette|volume=18|issue=9|title=}}
  • {{cite book |last= Andrews |first= C.N. |author2=Morgan, E.B. |title=Supermarine Aircraft since 1914|edition= Second |year=1987 |publisher=Putnam |location=London |isbn=0-85177-800-3 }}
  • A.J. Jackson, British Civil Aircraft since 1919 Volume 3, 1974, Putnam, London, {{ISBN|0-370-10014-X}}, Page 315
{{Supermarine aircraft}}

5 : British military reconnaissance aircraft 1920–1929|Amphibious aircraft|Supermarine aircraft|Aircraft first flown in 1924|Twin piston-engined tractor aircraft

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