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词条 Borel hydro-monoplane
释义

  1. Design and development

  2. Operational history

  3. Operators

  4. Specifications

  5. References

name = Borel hydro-monoplane image = File:Borel Marinha 2A.PNG caption = alt =

}}{{Infobox aircraft type

type = Seaplanenational origin = Francemanufacturer = Etablissements Boreldesigner = first flight = 1912introduced = retired = status = primary user = more users = produced = number built =program cost = unit cost = developed from = Morane-Borel monoplanevariants with their own articles =
}}

The Borel Hydro-monoplane was a French seaplane produced in 1912.

Design and development

The Borel hydro-monoplane, which was developed from the 1911 Morane-Borel monoplane, was a tractor monoplane powered by an 80 hp Gnome Lambda rotary engine. The rectangular section fuselage tapered to a vertical knife-edge at the rear: at the front the longerons on each side were curved inwards, meeting at the front engine bearer. A curved aluminium cowling covered the top of the engine, and the sides of the fuselage were covered with aluminium as far aft as the rear of the cockpit. The two seats were arranged in tandem, with the pilot sitting in front. Dual controls were fitted. Tail surfaces consisted of a narrow-chord fixed horizontal surface with a much broader elevator with horn balances hinged to the trailing edge and a balanced rudder which extended below the sternpost and carried a small float. The main undercarriage consisted of a pair of unstepped flat-bottomed floats. Lateral control was by wing warping.[1]

Operational history

An example was entered in the 1913 Schneider Trophy competition, but crashed during the elimination trials.[2]

Another example, flown by George Chemet, was the winner of the 1913 Paris-Deauville race.[3]

Operators

{{flag|Italy}}
  • Corpo Aeronautico Militare
{{UK}}
  • Royal Naval Air Service
  • Royal Flying Corps
{{BRA}}
  • Brazilian Naval Aviation
  • Military Police of Paraná State

Specifications

{{Aircraft specs
|ref= Flight, 26 July 1913, p. 814[4]
|prime units?=

met


|genhide=
|crew=one
|capacity=one passenger
|length m=
|length ft=27
|length in=6
|length note=
|span m=
|span ft=38
|span in=4
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|wing area sqm=
|wing area sqft=190
|wing area note=
|airfoil=
|empty weight kg=
|empty weight lb=
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|max takeoff weight note=
|fuel capacity=
|lift kg=
|lift lb=
|lift note=
|more general=


|eng1 number=1
|eng1 name=Gnome Lambda
|eng1 type=7-cylinder rotary engine
|eng1 kw=
|eng1 hp=80
|eng1 shp=
|eng1 note=
|power original=
|thrust original=
|prop blade number=2
|prop name=
|prop dia m=
|prop dia ft=8
|prop dia in=6
|prop dia note=


|perfhide=Y
|max speed kmh=
|max speed mph=
|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=
|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=
|ceiling m=
|ceiling ft=
|ceiling note=
|g limits=
|roll rate=
|glide ratio=
|climb rate ms=
|climb rate ftmin=
|climb rate note=
|time to altitude=
|lift to drag=
|wing loading kg/m2=
|wing loading lb/sqft=
|wing loading note=
|fuel consumption kg/km=
|fuel consumption lb/mi=
|power/mass=
|thrust/weight=
|more performance=
}}

References

1. ^{{cite journal|journal=Flight|url=http://www.flightglobal.com/pdfarchive/view/1913/1913%20-%200430.html|title=The Borel Hydro-Monoplane |date=19 July 1913|page=450}}
2. ^{{cite journal|journal=Flight|url=http://www.flightglobal.com/pdfarchive/view/1913/1913%20-%200787.html|title=The Monaco Meet|date=19 April 1913|pages=813–6}}
3. ^{{cite book|author=Stéphane Nicolaou|title=Flying Boats & Seaplanes: A History from 1905|page=30 |location=| publisher=MBI Publishing |year= 1998|isbn= 9780760306215}}
4. ^Flight, 26 July 1913, p. 814
{{Borel aircraft}}

6 : Floatplanes|Schneider Trophy|Single-engined tractor aircraft|Mid-wing aircraft|Aircraft first flown in 1912|Rotary-engined aircraft

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