Canadian Vickers Vancouver: Difference between revisions
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{|{{Infobox |
{|{{Infobox aircraft begin |
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|name=Vancouver |
|name=Vancouver |
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|image=Canadian Vickers Vancouver ExCC.jpg |
|image=Canadian Vickers Vancouver ExCC.jpg |
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|caption= |
|caption= |
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}}{{Infobox |
}}{{Infobox aircraft type |
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|type=Transport/patrol flying boat |
|type=Transport/[[Maritime patrol aircraft|patrol flying boat]] |
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|manufacturer=[[Canadian Vickers Limited|Canadian Vickers]] |
|manufacturer=[[Canadian Vickers Limited|Canadian Vickers]] |
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|designer= |
|designer= |
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|introduced= |
|introduced= |
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|retired=1940 |
|retired=1940 |
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|status=out of service |
|status=out of service, cancelled |
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|primary user=[[RCAF]] |
|primary user=[[RCAF]] |
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|more users= |
|more users= |
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The '''Canadian Vickers Vancouver''' was a |
The '''Canadian Vickers Vancouver''' was a Canadian transport/patrol [[flying boat]] of the 1930s built by [[Canadian Vickers Limited|Canadian Vickers]]. |
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It was a twin-engine, equal-span [[biplane]]. The hull was of metal and the rest of the structure of fabric-covered wood. |
It was a twin-engine, equal-span [[biplane]]. The hull was of metal and the rest of the structure of fabric-covered wood. |
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==Development== |
==Development== |
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The '''Vancouver''' was developed as a replacement for the [[Canadian Vickers Varuna|Varuna]] in response to a [[Royal Canadian Air Force]] requirement for a flying boat to transport men and equipment to forest fires. The main difference from the '''Varuna''' was a duralumin hull and more powerful engines. The two flight crew were located in two tandem open cockpits, forward of the wing. The main cabin could accommodate a firefighting team of six men and all the required equipment. Five aircraft were delivered to the |
The '''Vancouver''' was developed as a replacement for the [[Canadian Vickers Varuna|Varuna]] in response to a [[Royal Canadian Air Force]] requirement for a flying boat to transport men and equipment to forest fires. The main difference from the '''Varuna''' was a duralumin hull and more powerful engines. The two flight crew were located in two tandem open cockpits, forward of the wing. The main cabin could accommodate a firefighting team of six men and all the required equipment. Five aircraft were delivered to the Royal Canadian Air Force, one was later converted into a coastal patrol aircraft.<ref name="Molson">{{cite book |last1=Molson |first1=K.M.|last2=Taylor |first2=H.A. |title=Canadian aircraft since 1909 |date=1982 |publisher=Canada's Wings |location=Stittsville, Ont. |isbn=0-920002-11-0 |edition=1. publ. |pages=198–202}}</ref> |
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==Design== --> |
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==Operational history== |
==Operational history== |
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After the outbreak of the [[World War II|Second World War]], Vancouvers served with 4 Squadron, RCAF at [[Jericho Beach Air Station]] until withdrawn from service in 1940. After a brief period of service in training duties, they were finally withdrawn and struck off in 1940. |
After the outbreak of the [[World War II|Second World War]], Vancouvers served with 4 Squadron, RCAF at [[Jericho Beach Air Station]] until withdrawn from service in 1940. After a brief period of service in training duties, they were finally withdrawn and struck off in 1940. |
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None of the aircraft saw service after 1940, one private offer to acquire was denied.<ref>http://www.rwrwalker.ca/RCAF_901_950_detailed.htm</ref> |
None of the aircraft saw service after 1940, one private offer to acquire was denied.<ref name="RWRwalker">{{cite web |last1=Walker |first1=R.W.R. |title=RCAF 901 to 950 |url=http://www.rwrwalker.ca/RCAF_901_950_detailed.htm |website=www.rwrwalker.ca |access-date=29 December 2018 |date=2005}}</ref> |
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==Variants== |
==Variants== |
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''Data from:''Canadian Aircraft since 1909<ref name="Molson"/> |
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* '''Vancouver I''' - prototype with [[Armstrong Siddeley Lynx|Armstrong Siddeley Lynx IV]] engines, one built. |
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* '''Vancouver |
* '''Vancouver I''' – prototype with [[Armstrong Siddeley Lynx|Armstrong Siddeley Lynx IV]] engines, one built. |
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* '''Vancouver |
* '''Vancouver IA''' – designation of prototype after installation of [[Armstrong Siddeley Lynx|Armstrong Siddeley Lynx IVC]] engines. |
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* '''Vancouver II''' – production transport version with [[Armstrong Siddeley Lynx IVC]] (three aircraft) or [[Wright J-6 Whirlwind]] (two aircraft) engines, five built. |
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* '''Vancouver IIS/S''' – conversion of three Lynx-powered Vancouver IIs to "service standard" with three Lewis gun cockpits for coastal patrol, powered by [[Armstrong Siddeley Serval IV]] engines. |
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* '''Vancouver IIS/W''' – "service standard" conversion of two [[Wright J-6 Whirlwind]] powered Vancouver IIs. |
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==Operator== |
==Operator== |
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;{{flag|Canada|1921}}: [[Royal Canadian Air Force]] |
;{{flag|Canada|1921}}: [[Royal Canadian Air Force]] |
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**[[No. 4 Squadron RCAF]] |
**[[No. 4 Squadron RCAF]] 1939-1940 |
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==Specifications (Vancouver IIS) == |
==Specifications (Vancouver IIS/W) == |
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{{Aircraft specs |
{{Aircraft specs |
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|ref=<!--dead linkRCAF.com<ref>{{cite web |url=http://www.rcaf.com/aircraft/patrol/vancouver/index.php?name=Vickers%20Vancouver |title=RCAF.com }}</ref>,--> Canadian aircraft since 1909,<ref name="Molson"/> Jane's all the World's Aircraft 1931<ref name=JAWA1931>{{cite book |title=Jane's all the World's Aircraft 1931 |editor1-last=Grey |editor1-first=C.G. |year=1931 |publisher=Sampson Low, Marston & company, ltd |location=London |pages=83c–84c}}</ref> |
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|ref=RCAF.com<ref>{{cite web |
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|prime units?=imp |
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|url=http://www.rcaf.com/aircraft/patrol/vancouver/index.php?name=Vickers%20Vancouver |
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|title=RCAF.com |
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|last= |
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|first= |
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|date= |
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|accessdate= |
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|work= |
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|publisher=}}</ref><!-- for giving the reference for the data --> |
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|prime units?=kts<!-- imp or kts first for US aircraft, and UK aircraft pre-metrification, met(ric) first for all others. You MUST choose a format, or no specifications will show --> |
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<!-- |
<!-- |
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General characteristics |
General characteristics |
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--> |
--> |
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|crew=9 (2 crew in civil versions) |
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|genhide= |
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|capacity=(7 pax in civil versions) |
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|length ft=37 |
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|crew=two (nine in military Vancouvers) |
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|length in=6 |
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|capacity=7 pax |
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|length m= |
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|length ft=38 |
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|length in=3 |
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|length note= |
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|span m=16.76 |
|span m=16.76 |
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|span ft= |
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|span in= |
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|span note= |
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|upper span m= |
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|upper span ft= |
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|upper span in= |
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|upper span note= |
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|mid span m= |
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|mid span ft= |
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|mid span in= |
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|mid span note= |
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|lower span m= |
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|lower span ft= |
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|lower span in= |
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|lower span note= |
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|swept m=<!-- swing-wings --> |
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|swept ft=<!-- swing-wings --> |
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|swept in=<!-- swing-wings --> |
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|swept note= |
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|dia m=<!-- airships etc --> |
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|dia ft=<!-- airships etc --> |
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|dia in=<!-- airships etc --> |
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|dia note= |
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|width m=<!-- if applicable --> |
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|width ft=<!-- if applicable --> |
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|width in=<!-- if applicable --> |
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|width note= |
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|height m=4.75 |
|height m=4.75 |
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|wing area sqft=772 |
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|height ft= |
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|height in= |
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|height note= |
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|wing area sqm=76.08 |
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|wing area sqft= |
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|wing area note= |
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|swept area sqm=<!-- swing-wings --> |
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|swept area sqft=<!-- swing-wings --> |
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|swept area note= |
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|volume m3=<!-- lighter-than-air --> |
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|volume ft3=<!-- lighter-than-air --> |
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|volume note= |
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|aspect ratio=<!-- give where relevant eg sailplanes --> |
|aspect ratio=<!-- give where relevant eg sailplanes --> |
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|airfoil= |
|airfoil=[[Clark Y]] |
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|empty weight kg= |
|empty weight kg=2340 |
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|gross weight kg=3450 |
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|empty weight note= |
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|gross weight kg=4,540 |
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|gross weight lb= |
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|gross weight note= |
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|max takeoff weight kg= |
|max takeoff weight kg= |
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|max takeoff weight lb= |
|max takeoff weight lb= |
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|max takeoff weight note= |
|max takeoff weight note= |
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|fuel capacity= |
|fuel capacity= |
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|lift kg=<!-- lighter-than-air --> |
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|lift lb=<!-- lighter-than-air --> |
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|lift note= |
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|more general= |
|more general= |
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<!-- |
<!-- |
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--> |
--> |
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|eng1 number=2 |
|eng1 number=2 |
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|eng1 name=[[ |
|eng1 name=[[Wright J-6 Whirlwind]] |
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|eng1 type= |
|eng1 type=9-cyl. air-cooled radial piston engine |
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|eng1 |
|eng1 hp=300 |
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|eng1 hp=310<!-- prop engines --> |
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|eng1 kn=<!-- jet/rocket engines --> |
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|eng1 lbf=<!-- jet/rocket engines --> |
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|eng1 note= |
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|power original= |
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|thrust original= |
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|eng1 kn-ab=<!-- afterburners --> |
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|eng1 lbf-ab=<!-- afterburners --> |
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|prop blade number=2 |
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|prop name=Standard steel fixed-pitch propellers |
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|eng2 name= |
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|eng2 type= |
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|eng2 kw=<!-- prop engines --> |
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|eng2 hp=<!-- prop engines --> |
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|eng2 kn=<!-- jet/rocket engines --> |
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|eng2 lbf=<!-- jet/rocket engines --> |
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|eng2 note= |
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|eng2 kn-ab=<!-- afterburners --> |
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|eng2 lbf-ab=<!-- afterburners --> |
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|eng3 number= |
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|eng3 name= |
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|eng3 type= |
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|eng3 kw=<!-- prop engines --> |
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|eng3 hp=<!-- prop engines --> |
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|eng3 kn=<!-- jet/rocket engines --> |
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|eng3 lbf=<!-- jet/rocket engines --> |
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|eng3 note= |
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|eng3 kn-ab=<!-- afterburners --> |
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|eng3 lbf-ab=<!-- afterburners --> |
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|more power= |
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|prop blade number=<!-- propeller aircraft --> |
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|prop name= |
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|prop dia m=<!-- propeller aircraft --> |
|prop dia m=<!-- propeller aircraft --> |
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|prop dia ft=<!-- propeller aircraft --> |
|prop dia ft=<!-- propeller aircraft --> |
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|prop dia in=<!-- propeller aircraft --> |
|prop dia in=<!-- propeller aircraft --> |
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|prop note= |
|prop note= |
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|rot number=<!-- helicopters --> |
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|rot dia m=<!-- helicopters --> |
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|rot dia ft=<!-- helicopters --> |
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|rot dia in=<!-- helicopters --> |
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|rot area sqm=<!-- helicopters --> |
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|rot area sqft=<!-- helicopters --> |
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|rot area note= |
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<!-- |
<!-- |
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Performance |
Performance |
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--> |
--> |
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|perfhide= |
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|max speed kmh=151 |
|max speed kmh=151 |
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|max speed mph= |
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|max speed kts= |
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|max speed note= |
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|max speed mach=<!-- supersonic aircraft --> |
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|cruise speed kmh=138 |
|cruise speed kmh=138 |
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|cruise speed mph= |
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|cruise speed kts= |
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|cruise speed note= |
|cruise speed note= |
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*'''Alighting speed:''' {{cvt|45|mph|kn km/h}} |
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|stall speed kmh=<!-- aerobatic --> |
|stall speed kmh=<!-- aerobatic --> |
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|stall speed mph=<!-- aerobatic --> |
|stall speed mph=<!-- aerobatic --> |
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|ferry range note= |
|ferry range note= |
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|endurance=<!-- if range unknown --> |
|endurance=<!-- if range unknown --> |
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|ceiling |
|ceiling ft= 15000 |
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|ceiling |
|ceiling note=plus |
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|ceiling note= |
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|g limits=<!-- aerobatic --> |
|g limits=<!-- aerobatic --> |
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|roll rate=<!-- aerobatic --> |
|roll rate=<!-- aerobatic --> |
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|glide ratio=<!-- sailplanes --> |
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|climb rate ms= |
|climb rate ms= |
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|climb rate ftmin= |
|climb rate ftmin=565 |
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|climb rate note= |
|climb rate note= |
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|time to altitude= |
|time to altitude= |
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|sink rate ms=<!-- sailplanes --> |
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|sink rate ftmin=<!-- sailplanes --> |
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|sink rate note= |
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|lift to drag= |
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|wing loading kg/m2= |
|wing loading kg/m2= |
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|wing loading lb/sqft= |
|wing loading lb/sqft= |
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|wing loading note= |
|wing loading note= |
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|disk loading kg/m2= |
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|disk loading lb/sqft= |
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|disk loading note= |
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|power/mass= |
|power/mass= |
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|thrust/weight= |
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|more performance= |
|more performance= |
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Armament |
Armament |
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--> |
--> |
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|guns= 3 x {{cvt|0.303|in|2}} [[Lewis Gun]]s (military Vancouvers only) |
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|bombs= {{cvt|1000|lb}} of bombs (military Vancouvers only) |
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|bombs= 1,000lb (450 kg) of bombs (military Vancouvers only) |
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|rockets= |
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|missiles= |
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|hardpoints= |
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|hardpoint capacity= |
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|hardpoint rockets= |
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|hardpoint missiles= |
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|hardpoint bombs= |
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|hardpoint other= |
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|other armament= |
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|avionics= |
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}} |
}} |
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==See also== |
==See also== |
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{{Portal|Aviation| |
{{Portal|Aviation|Canada}} |
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{{aircontent |
{{aircontent |
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|related=<!-- related developments --> |
|related=<!-- related developments --> |
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|similar aircraft=<!-- similar or comparable aircraft --> |
|similar aircraft=<!-- similar or comparable aircraft --> |
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|sequence=<!-- designation sequence, if appropriate --> |
|sequence=<!-- designation sequence, if appropriate --> |
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|lists= |
|lists= |
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* [[List of aircraft of World War II]] |
* [[List of aircraft of World War II]] |
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* [[List of |
* [[List of flying boats and floatplanes]] |
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* [[List of |
* [[List of interwar military aircraft]] |
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|see also=<!-- other relevant information --> |
|see also=<!-- other relevant information --> |
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}} |
}} |
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{{Canadian Vickers aircraft}} |
{{Canadian Vickers aircraft}} |
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{{Aircraft manufactured in Canada}} |
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[[Category:Canadian patrol aircraft |
[[Category:1920s Canadian patrol aircraft]] |
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[[Category:Canadian Vickers aircraft|Vancouver]] |
[[Category:Canadian Vickers aircraft|Vancouver]] |
||
[[Category:Biplanes]] |
[[Category:Biplanes]] |
||
[[Category:Twin-engined tractor aircraft]] |
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[[Category:Aircraft first flown in 1929]] |
[[Category:Aircraft first flown in 1929]] |
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[[Category:Twin piston-engined tractor aircraft]] |
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Latest revision as of 20:20, 15 February 2024
| Vancouver | |
|---|---|
| |
| Role | Transport/patrol flying boat |
| Manufacturer | Canadian Vickers |
| First flight | 1929 |
| Retired | 1940 |
| Status | out of service, cancelled |
| Primary user | RCAF |
| Produced | 6 |
The Canadian Vickers Vancouver was a Canadian transport/patrol flying boat of the 1930s built by Canadian Vickers.
It was a twin-engine, equal-span biplane. The hull was of metal and the rest of the structure of fabric-covered wood.
Development[edit]
The Vancouver was developed as a replacement for the Varuna in response to a Royal Canadian Air Force requirement for a flying boat to transport men and equipment to forest fires. The main difference from the Varuna was a duralumin hull and more powerful engines. The two flight crew were located in two tandem open cockpits, forward of the wing. The main cabin could accommodate a firefighting team of six men and all the required equipment. Five aircraft were delivered to the Royal Canadian Air Force, one was later converted into a coastal patrol aircraft.[1]
Operational history[edit]
In the mid-1930s, the Vancouvers were modified as coastal patrol aircraft by the installation of machine guns and bombs.
After the outbreak of the Second World War, Vancouvers served with 4 Squadron, RCAF at Jericho Beach Air Station until withdrawn from service in 1940. After a brief period of service in training duties, they were finally withdrawn and struck off in 1940.
None of the aircraft saw service after 1940, one private offer to acquire was denied.[2]
Variants[edit]
Data from:Canadian Aircraft since 1909[1]
- Vancouver I – prototype with Armstrong Siddeley Lynx IV engines, one built.
- Vancouver IA – designation of prototype after installation of Armstrong Siddeley Lynx IVC engines.
- Vancouver II – production transport version with Armstrong Siddeley Lynx IVC (three aircraft) or Wright J-6 Whirlwind (two aircraft) engines, five built.
- Vancouver IIS/S – conversion of three Lynx-powered Vancouver IIs to "service standard" with three Lewis gun cockpits for coastal patrol, powered by Armstrong Siddeley Serval IV engines.
- Vancouver IIS/W – "service standard" conversion of two Wright J-6 Whirlwind powered Vancouver IIs.
Operator[edit]
- No. 4 Squadron RCAF 1939-1940
Specifications (Vancouver IIS/W)[edit]
Data from Canadian aircraft since 1909,[1] Jane's all the World's Aircraft 1931[3]
General characteristics
- Crew: 9 (2 crew in civil versions)
- Capacity: (7 pax in civil versions)
- Length: 37 ft 6 in (11.43 m)
- Wingspan: 55 ft 0 in (16.76 m)
- Height: 15 ft 7 in (4.75 m)
- Wing area: 772 sq ft (71.7 m2)
- Airfoil: Clark Y
- Empty weight: 5,159 lb (2,340 kg)
- Gross weight: 7,606 lb (3,450 kg)
- Powerplant: 2 × Wright J-6 Whirlwind 9-cyl. air-cooled radial piston engine, 300 hp (220 kW) each
- Propellers: 2-bladed Standard steel fixed-pitch propellers
Performance
- Maximum speed: 94 mph (151 km/h, 82 kn)
- Cruise speed: 86 mph (138 km/h, 75 kn) *Alighting speed: 45 mph (39 kn; 72 km/h)
- Service ceiling: 15,000 ft (4,600 m) plus
- Rate of climb: 565 ft/min (2.87 m/s)
Armament
- Guns: 3 x 0.303 in (7.70 mm) Lewis Guns (military Vancouvers only)
- Bombs: 1,000 lb (450 kg) of bombs (military Vancouvers only)
See also[edit]
Related lists
- List of aircraft of World War II
- List of flying boats and floatplanes
- List of interwar military aircraft
References[edit]
Wikimedia Commons has media related to Canadian Vickers Vancouver.
- ^ a b c Molson, K.M.; Taylor, H.A. (1982). Canadian aircraft since 1909 (1. publ. ed.). Stittsville, Ont.: Canada's Wings. pp. 198–202. ISBN 0-920002-11-0.
- ^ Walker, R.W.R. (2005). "RCAF 901 to 950". www.rwrwalker.ca. Retrieved 29 December 2018.
- ^ Grey, C.G., ed. (1931). Jane's all the World's Aircraft 1931. London: Sampson Low, Marston & company, ltd. pp. 83c–84c.