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词条 Short S.41
释义

  1. Development and design

  2. Operational history

  3. Variants

  4. Operators

  5. Specifications (S.41 seaplane)

  6. See also

  7. Notes

  8. References

  9. External links

{{Use dmy dates|date=January 2017}}{{Use British English|date=January 2017}}
name=Short S.41 image=Charles Rumney Samson b322bdd7fb o.jpg caption=

}}{{Infobox Aircraft Type

type=Floatplane national origin=United Kingdom manufacturer=Short Brothers designer= first flight=2 April 1912 introduced= 1912 retired= status= primary user=Royal Naval Air Service more users= produced= number built=3 (S.41, S.51 and S.52) program cost= unit cost= developed from= Short S.36 variants with their own articles=
}}

The Short S.41 was a British single-engined biplane built for the Royal Naval Air Service in 1912. Capable of being operated either on wheels or floats, it was successful enough for a further two similar aircraft to be built, with the type remaining in use until the early years of the First World War.

Development and design

In 1912, the Short S.36 tractor biplane, built for Francis McClean, was loaned to the Royal Naval Air Service (RNAS) for use at its Naval Flying School. Impressed by the S.36, the RNAS ordered two similar tractor biplanes, capable of operating on either wheels or floats, the smaller Short S.45, like the S.36, powered by a 70 hp (52 kW) Gnome Lambda, and the larger Short S.41 powered by a 14-cylinder, twin-row 100 hp (75 kW) Gnome double Omega rotary engine.[1]

The S.41 was an unequal-span two bay tractor biplane with a slim rectangular section fuselage mounted between the wings.[2] It was first flown by Charles Rumney Samson on 2 April 1912 with a wheeled undercarriage, and shortly afterwards was fitted with floats, consisting of two main pontoons under the fuselage and smaller floats at the wingtips and tail, and was delivered to the Navy.[2]

Following the operational flights made during 1912, S.41 was returned to the factory for an overhaul and the fitting of folding wings, which were hinged so that they folded back horizontally alongside the fuselage, reducing storage space required for stowage aboard ship. At this time it was given the RNAS number "10". In November 1913 it underwent further modifications, being used to perfect a development of the folding mechanism which allowed the wings to be unfolded from the cockpit: at the same time new wings, similar in pattern to those of the Short Admiralty Type 81 were fitted.

The folding wing mechanism for shipborne aircraft had been designed by Horace Short, and was the subject of a series of patents[3]

Operational history

The S.41 was flown successfully at the Fleet Review at Weymouth on 8 May, being based on the Battleship HMS Hibernia.[4] It was also used by Samson to carry out survey flights of potential sites for seaplane stations, which led to the establishment of the seaplane station at Felixstowe,[5] and for early trials with use of radio from aircraft.[4]

The success of the S.41 was such that two similar aircraft, constructor's numbers S.51 and S.52,[6] also powered by the two-row Gnome, were ordered by the RNAS,[7] with serial numbers 20 and 21: These were first flown in April 1913.[8] These aircraft differed in detail from the first aircraft: the wing section was improved, double-acting ailerons were fitted and the overhanging section of the upper wing was braced by kingposts rather than struts.

Like 10, they were used for trials of airborne radio, as well as carrying out tests of beaching gear.[4] They remained in use at the start of the First World War, where, despite the unreliability of the twin-row Gnome,[9] they were used for anti-submarine patrols early in the war, 20 continuing in use from the seaplane station at Great Yarmouth until July 1915.[2][10]

Variants

A single aircraft, similar in design to the S.41 but slightly smaller, was built by Shorts and exhibited at the 1913 Aero Show at Olympia, London, featuring a number of refinements including manganese-steel tube interplane struts and provision for starting the engine from the cockpit. This had the Shorts manufacturer's number S.53, and was later bought by the Admiralty and given RNAS No. 42, thereby becoming known as the Admiralty Type 42. It was first flown as a seaplane but later fitted with a wheeled undercarriage: in this form it was one of the aircraft which were sent to Ostend at the outbreak of World War I: it was written off by Samson on 28 September 1914 when it crashed on takeoff due to engine failure.[11]

Operators

{{UK}}
  • Royal Naval Air Service

Specifications (S.41 seaplane)

{{Aircraft specs
|ref=Shorts Aircraft since 1900[12]
|prime units?=imp


|genhide=
|crew=two
|capacity=
|length m=
|length ft=39
|length in=
|length note=as seaplane: length as landplane 36 ft 6 in (11.15 m)
|span m=
|span ft=50
|span in=
|span note=
|upper span m=
|upper span ft=
|upper span in=
|upper span note=
|mid span m=
|mid span ft=
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|mid span note=
|lower span m=
|lower span ft=
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|height m=
|height ft=11
|height in=9
|height note=[13]
|wing area sqm=
|wing area sqft=450
|wing area note=
|volume note=
|aspect ratio=
|airfoil=
|empty weight kg=
|empty weight lb=1100
|empty weight note=
|gross weight kg=
|gross weight lb=1600
|gross weight note=
|max takeoff weight kg=
|max takeoff weight lb=
|max takeoff weight note=
|fuel capacity=
|more general=


|eng1 number=1
|eng1 name=Gnome Double Omega
|eng1 type=14-cylinder, two-row rotary engine
|eng1 kw=
|eng1 hp=100
|eng1 kn=
|eng1 lbf=
|eng1 note=
|power original=
|thrust original=
|eng1 kn-ab=
|eng1 lbf-ab=
|prop blade number=
|prop name=
|prop dia m=
|prop dia ft=
|prop dia in=
|prop note=


|perfhide=
|max speed kmh=
|max speed mph=60
|max speed kts=
|max speed note=
|max speed mach=
|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=
|combat range km=
|combat range miles=
|combat range nmi=
|combat range note=
|ferry range km=
|ferry range miles=
|ferry range nmi=
|ferry range note=
|endurance=5 hrs
|ceiling m=
|ceiling ft=
|ceiling note=
|g limits=
|roll rate=
|glide ratio=
|climb rate ms=
|climb rate ftmin=
|climb rate note=
|time to altitude=
|sink rate note=
|lift to drag=
|wing loading kg/m2
|wing loading lb/sqft=
|wing loading note=
|power/mass=
|thrust/weight=
|more performance=


|armament=
|guns=
|bombs=
|rockets=
|missiles=
|hardpoints=
|hardpoint capacity=
|hardpoint rockets=
|hardpoint missiles=
|hardpoint bombs=
|hardpoint other=
|avionics=
}}

See also

{{aircontent
|see also=
|related=
|similar aircraft=
|lists=
  • List of aircraft of the Royal Naval Air Service
  • List of seaplanes and amphibious aircraft

}}

Notes

1. ^Barnes 1967, pp. 79–80.
2. ^Barnes 1967, p.80.
3. ^Patents secured by Short Brothers including patents nos. 1792/13, 15727/13 and 28610/13, 5290/14, 20537/14 and 9276/15, see Barnes and James, pp. 92, 110
4. ^Bruce Flight 14 December 1956, p. 923.
5. ^Barnes 1967, p.82.
6. ^Barnes 1989, pp. 529.
7. ^Barnes 1967, p.83.
8. ^Barnes 1967, pp. 88–89.
9. ^Barnes 1967, p. 97.
10. ^Flight 14 December 1956, p. 924.
11. ^Barnes 1967
12. ^Barnes 1967, p.87.
13. ^Bruce 1957, pp. 472–473.

References

{{refbegin}}
  • Barnes, C.H. Shorts Aircraft since 1900. London:Putnam, 1967.
  • Bruce, J.M. "The Short Seaplanes:Historical Military Aircraft No. 14 Part I". Flight, 14 December 1956. pp. 921–926.
  • Bruce, J.M. British Aeroplanes 1914–18. London:Putnam, 1957.
{{refend}}

External links

{{commons category-inline|Short S.41}}{{Short Brothers aircraft}}

7 : British military reconnaissance aircraft 1910–1919|Floatplanes|Short Brothers aircraft|Biplanes|Rotary-engined aircraft|Single-engined tractor aircraft|Aircraft first flown in 1912

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