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词条 Short Crusader
释义

  1. Background

  2. Design and development

  3. Operational history

  4. Operators

  5. Specifications

  6. See also

  7. References

  8. External links

{{Use dmy dates|date=January 2017}}{{Use British English|date=January 2017}}
name = Short Crusaderimage = Short Crusader A4.jpgcaption =

}}{{Infobox aircraft type

type = Racing seaplanenational origin = UKmanufacturer = Short Brothersdesigner = W A Bristowfirst flight = 4 May 1927introduction =retired = status = primary user = Royal Air Force, High Speed Flightmore users = produced = number built = 1program cost =unit cost =developed from =variants with their own articles =
}}

The Short Crusader also called the Short-Bristow Crusader[1] and Short-Bristol Crusader[2] was a British racing seaplane of the 1920s, built by Short Brothers to compete in the 1927 Schneider Trophy race.

Background

Although inline engines had a clear advantage for high-speed aircraft due to the smaller frontal area, Roy Fedden, the engineer in charge of aero-engine development at Bristol Aircraft, was unwilling to let the initiative in engine development pass to Rolls-Royce and Napier, and managed to obtain a contract for an uprated version of the Mercury nine-cylinder radial engine. The early production versions of this engine produced {{convert|420|hp|kW|abbr=on}}, but the uprated engine produced {{convert|960|hp|kW|abbr=on}} in bench-testing, although for flight purposes it was limited to an output of {{convert|810|hp|kW|abbr=on}}[3] The project for a racing aircraft using this engine was entrusted to Lieut.-Col. W. A. Bristow, a consultant aero-engineer, and W. G. Carter. Submitted to the Air Ministry in early 1926, the design was accepted and a contract for one prototype was awarded. Since it became apparent that the resources of a large aircraft manufacturer would be necessary, detail design and manufacture was assigned to Shorts, who had already been made responsible for the design and manufacture of the floats.

Design and development

The aircraft was a low-wing monoplane of mainly wooden construction. The wire-braced wings were of an unusual elliptical layout, with the maximum chord and thickness at mid-span on each side, tapering in towards the root. The two box-spars and the ribs were of spruce, covered with thin mahogany sheet overlaid with silk. The rear of the elliptical section fuselage was also wooden, being a monocoque construction with two layers of mahogany veneer applied over a frame of spruce formers and stringers. The forward section was built from steel tubing, covered with duralumin panels. The exposed cylinders were covered by streamlined helmets to minimise drag while admitting enough air to cool the engine, the helmet of the uppermost cylinder being continued back as a fairing which incorporated the windscreen and pilot's headrest. The twin floats, made of duralumin, were each carried on a pair of streamline section raked struts, braced by wires.[4]

Operational history

The aircraft was completed by 18 April 1927, fitted with a derated engine producing {{convert|650|hp|kW|abbr=on}} and wooden propeller for initial testing. Flight testing at Rochester had been prohibited by the Air Ministry, so after taxying trials it was dismantled and taken to Felixstowe, where the RAF High Speed Flight was then based.

Initial flight testing was made by Bert Hinkler, who asked Shorts to enlarge the aircraft's rudder area before he attempted to fly it. On 4 May Hinkler flew the aircraft for the first time, making a flight during which he achieved an average speed of {{convert |232|mph|kph|abbr=on}} over a measured mile. On landing Hinkler touched down first with the left- hand float, causing the aircraft to slew round, resulting in severe buckling of the float struts. Hinkler reported that the aircraft suffered from severe hunting at full throttle, admitting that he had been wrong about the rudder area. The main problem encountered was intake surging, which caused the engine to cut out intermittently.

After repairs, restoration of the rudder to the original size and some alterations to alleviate the intake problem, Hinkler made a second flight, after which the aircraft was formally accepted by the RAF, and RAF markings and serial number were painted on the tailfin. The first RAF pilot to fly it was Flt, Lieut. S.N. Webster, who reported its flight characteristics to be pleasant, although the engine still tended to cut out: this led to some alarming episodes when the aircraft was later flown by Flying Officer H.M. Schofield. During July a number of modifications were made: a new engine was fitted, together with a forged duralumin racing propeller, an additional fuel tank was fitted in the right-hand float to provide sufficient range to complete the Schneider course, high-temperature spark plugs were fitted and changes were made to the air inlets in a further attempt to cure the engine problems.

In mid August the Crusader was dismantled and shipped on HMS Eagle to Venice. Here it was fitted with the race engine, but since it was obviously slower than the other aircraft entered, it was intended to use it solely as a practice aircraft. On 11 September Schofield took off in the aircraft: since the aircraft with full fuel load was heavy on takeoff, he held the aircraft close to the water to build up speed. It is probable that the aircraft encountered a thermal caused by the hot weather, for suddenly the right wing lifted. Schofield attempted to correct this, but the control wires to the ailerons had been crossed during reassembly, so that the aileron movement was reversed. The aircraft continued the roll, and hit the water at a speed of {{convert|150|mph|abbr=on}}. The fuselage broke in half at the cockpit and Schofield was thrown clear, sustaining serious bruises but no broken bones. The aircraft sank into the lagoon and was recovered a week later, when examination of the wreckage clearly established the cause of the crash.[5]

Operators

{{UK}}
  • Royal Air Force
    • High Speed Flight RAF

Specifications

{{Aircraft specs
|ref=[6]
|prime units?= imp
|genhide=
|crew=one
|length m=
|length ft=25
|length in=
|length note=
|span m=
|span ft=26
|span in=6
|height m=
|height ft=
|height in=
|height note=
|wing area sqm=
|wing area sqft=120
|wing area note=
|airfoil=RAF 27 biconvex
|empty weight kg=
|empty weight lb=1938
|empty weight note=
|gross weight kg=
|gross weight lb=2712
|gross weight note=
|max takeoff weight kg=
|max takeoff weight lb=
|max takeoff weight note=
|fuel capacity=
|more general=


|eng1 number=1
|eng1 name=Bristol Mercury I
|eng1 type=9 cylinder air-coled radial
|eng1 kw=
|eng1 hp=810
|eng1 shp=
|eng1 kn=
|eng1 lbf=
|eng1 note=
|power original=
|prop blade number=2
|prop name=
|prop dia m=
|prop dia ft=
|prop dia in=
|prop dia note=


|perfhide=
|max speed kmh=
|max speed mph=270
|max speed kts=
|max speed note=
|cruise speed kmh=
|cruise speed mph=
|cruise speed kts=
|cruise speed note=
|stall speed kmh=
|stall speed mph=
|stall speed kts=
|stall speed note=
|never exceed speed kmh=
|never exceed speed mph=
|never exceed speed kts=
|never exceed speed note=
|minimum control speed kmh=
|minimum control speed mph=
|minimum control speed kts=
|minimum control speed note=
|range km=
|range miles=
|range nmi=
|range note=
|endurance=
|ceiling m=
|ceiling ft=
|ceiling note=
|climb rate ms=
|climb rate ftmin=
|climb rate note=
|time to altitude=
|wing loading kg/m2=
|wing loading lb/sqft=22.6
|wing loading note=
|fuel consumption kg/km=
|fuel consumption lb/mi=
|power/mass=
|thrust/weight=
|more performance=
}}

See also

{{Aircontent
|similar aircraft =
  • Supermarine S.5
  • Gloster IV
  • Macchi M.52

|lists=
  • List of aircraft of the RAF

|see also=
}}

References

1. ^Barnes, 1989, p.217
2. ^The Third British Schneider ChallengerFlight 18 August 1927
3. ^Barnes & James, p. 218
4. ^Barnes 1989 p.218-9
5. ^Barnes & James, p. 222
6. ^Barnes & James, p. 223
  • {{cite book | last = Barnes| first =C.H.|author2=James, D.N. | title =Shorts Aircraft since 1900| publisher =Putnam| year =1989| location =London| pages =560| isbn = 0-85177-819-4}}
  • http://www.airracinghistory.freeola.com/aircraft/Short%20Crusader.htm accessed 23 April 2008

External links

{{commons category|Short Brothers aircraft}}
  • Some Notes on the "Crusader"Flight International 18 August 1927
{{Short Brothers aircraft}}

7 : British sport aircraft 1920–1929|Schneider Trophy|Floatplanes|Short Brothers aircraft|Low-wing aircraft|Single-engined tractor aircraft|Aircraft first flown in 1927

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