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词条 Avro Avis
释义

  1. Design and development

  2. Specifications

  3. See also

  4. References

     Notes  Bibliography 

  5. External links

{{Use dmy dates|date=May 2017}}{{Use British English|date=May 2017}}
name= Avro 562 Avis image= File:AAvis.jpg caption=

}}{{Infobox Aircraft Type

type=Light biplane national origin=United Kingdom manufacturer=Avro designer= first flight=1924 introduced= retired=1931 status= primary user= number built=1 developed from= variants with their own articles=
}}

The Avro 562 Avis was a two-seat light biplane designed and built by the A.V.Roe and Company Limited at Hamble for the 1924 Lympne Light Aeroplane Trials.

Design and development

The Avis was a single-bay unstaggered biplane with full-span ailerons on both upper and lower wings. It had a fixed landing gear with a tailskid and could be powered by a nose-mounted 32 hp Bristol Cherub II engine or a 35 hp Blackburne Thrush radial piston engine.[1] It had tandem open cockpits. First flown with the Thrush engine prior to the trials, it was refitted with the Cherub, and first flown with this engine by Bert Hinkler at Lympne on 30 September 1924. On the next day it won the Grosvenor Cup at a speed of 65.87 mph.[2]

For the 1926 trials it was re-engined with a 38 hp Blackburne Thrush, being eliminated after a forced landing. In 1927, it was re-engined again with a Bristol Cherub I and passed into private ownership until it was scrapped in 1931.[3]

Specifications

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|ref=Avro Aircraft since 1908.[4]
|met or eng?=eng
|crew=one (pilot)
|capacity=one (passenger)
|length m=7.32
|length ft= 24
|length in=0
|span m=9.17
|span ft=30
|span in=1
|swept m=
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|rot dia m=
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|width ft=
|width in=
|height m=2.74
|height ft=9
|height in=0
|wing area sqm=22.9
|wing area sqft=246
|swept area sqm=
|swept area sqft=
|rot area sqm=
|rot area sqft=
|volume m3=
|volume ft3=
|aspect ratio=
|empty weight kg=268
|empty weight lb=590
|gross weight kg=451
|gross weight lb=995
|lift kg=
|lift lb=
|eng1 number=1
|eng1 type=Blackburne Thrush three-cylinder air-cooled radial engine
|eng1 kw=26
|eng1 hp=35
|eng1 kn=
|eng1 lbf=
|eng1 kn-ab=
|eng1 lbf-ab=
|eng2 number=
|eng2 type=
|eng2 kw=
|eng2 hp=
|eng2 kn=
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|eng2 kn-ab=
|eng2 lbf-ab=
|max speed kmh=120
|max speed mph=75
|max speed mach=
|cruise speed kmh=
|cruise speed mph=
|range km=
|range miles=
|endurance h=
|endurance min=
|ceiling m=
|ceiling ft=
|glide ratio=
|climb rate ms=
|climb rate ftmin=
|sink rate ms=
|sink rate ftmin=
|armament1=
|armament2=
|armament3=
|armament4=
|armament5=
|armament6=
}}

See also

{{aircontent
|see also=
|related=
|similar aircraft=
  • Hawker Cygnet
  • Westland Widgeon

|lists=
}}

References

Notes

1. ^Jackson 1990, p. 222.
2. ^Jackson 1990, pp. 222–223.
3. ^Jackson 1990, p. 224.
4. ^Jackson 1990, p. 225.

Bibliography

{{Refbegin}}
  • Jackson, A.J. Avro Aircraft since 1908. London: Putnam Aeronautical Books 2nd edition, 1990. {{ISBN|0-85177-834-8}}.
  • Jackson, A.J. British Civil Aircraft since 1919, Volume 1. London: Putnam, 1974. {{ISBN|0-370-10006-9}}.
{{Refend}}

External links

{{commons category|Avro Avis}}
  • [https://web.archive.org/web/20070211094906/http://www.britishaircraft.co.uk/aircraftpage.php?ID=263 Avro Avis] – British Aircraft Directory
{{Avro aircraft}}

3 : British sport aircraft 1920–1929|Avro aircraft|Aircraft first flown in 1924

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