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词条 Gourdou-Leseurre GL-820 HY
释义

  1. Design and development

  2. Variants

  3. Specifications (GL-821 HY)

  4. References

{{short description|1930s French floatplane}}
name=GL-820 HY image= caption=

}}{{Infobox aircraft type

type=Shipborne reconnaissance / torpedo floatplane national origin=France manufacturer=Gourdou-Leseurre designer= first flight=
GL-820 HY 10 May 1935
GL-821 HY 28 January 1936

GL-821 HY 02 5 October 1937

introduced= retired= status= primary user= more users= produced= number built=

1x GL-820 HY

1 x GL-821 HY

1 x GL-821 HY 02

program cost= unit cost= developed from= variants with their own articles=
}}

The Gourdou-Leseurre GL-820 HY family of four-seat single-engined floatplanes were designed and built in France during the latter half of the 1930s by Gourdou-Leseurre. The GL-820 HY and GL-821 HY 02 were shipborne reconnaissance / obeservation aircraft, while the sole GL-821 HY was built as a torpedo carrier.

Design and development

The Gl-820 and GL-821 were low-wing monoplane floatplanes with four tandem open cockpits, (the Cockpits on the GL-821 HY 02 were enclosed). The wings, tailplanes and floats were all supported by a system of streamlined struts.

Variants

GL-820 HY
The initial reconnaissance aircraft prototype, powered by a {{cvt|730|hp}} Hispano-Suiza 9Vb driving a two-bladed fixed-pitch wooden propeller.[1]
GL-821 HY
The second aircraft built as a torpedo carrier, powered by a {{cvt|750|hp}} Gnome & Rhône 9Kfr.[2]
GL-821 HY 02
The third aircraft, powered by a {{cvt|750|hp}} Gnome & Rhône 9Kfr driving a three-bladed metal propeller.[3]

Specifications (GL-821 HY)

{{Aircraft specs
|ref=Aviafrance : Gourdou Leseurre GL-821 HY[2], Gourdou Leseurre GL-821 HY 02[3], Gourdou Leseurre GL-820 HY[1]
|prime units?=met


|crew=4
|length m=11
|span m=16
|height m=5.2
|wing area sqm=44
|aspect ratio=
|airfoil=
|empty weight kg=1950
|gross weight kg=3200
|max takeoff weight kg=
|fuel capacity=
|more general=


|eng1 number=1
|eng1 name=Gnome & Rhône 9Kfr
|eng1 type=9-cylinder air-cooled radial piston engine
|eng1 hp=750
|eng1 note=

GL-820 HY: 1 x {{cvt|730|hp}} Hispano-Suiza 9Vb 9-cylinder radial


|prop blade number=
|prop name=
|prop dia m=
|prop dia ft=
|prop dia in=
|prop dia note=


|max speed kmh=220
|max speed note=

Gl-820 HY: {{cvt|215|km/h|mph kn}}

Gl-821 HY 02: {{cvt|235|km/h|mph kn}}


|cruise speed kmh=
|stall speed kmh=
|never exceed speed kmh=
|range km=1000
|combat range km=
|ferry range km=
|endurance=
|ceiling m=7000
|g limits=
|roll rate=
|climb rate ms=
|time to altitude=
|wing loading kg/m2=
|fuel consumption kg/km=
|power/mass=
|more performance=


|guns= 1 × fixed forward firing {{cvt|7.5|mm|3}} Darne machine gun in the starboard wing; 2x {{cvt|7.75|mm|3}} Lewis guns on a flexible mount in the rearmost cockpit
|bombs= {{cvt|300|kg}} of bombs (GL-820 HY and GL-821 HY 02) or one torpedo (GL-821 HY)
}}

References

1. ^{{cite web |last1=Parmentier |first1=Bruno |title=Gourdou Leseurre GL-820 HY |url=https://www.aviafrance.com/aviafrance1.php?ID=9313&ID_CONSTRUCTEUR=582&ANNEE=0&ID_MISSION=0&MOTCLEF= |website=Aviafrance |accessdate=1 February 2019 |location=Paris |language=fr |date=29 April 2003}}
2. ^{{cite web |last1=Parmentier |first1=Bruno |title=Gourdou Leseurre GL-821 HY |url=https://www.aviafrance.com/aviafrance1.php?ID=9314&ID_CONSTRUCTEUR=582&ANNEE=0&ID_MISSION=0&MOTCLEF= |website=Aviafrance |accessdate=1 February 2019 |location=Paris |language=fr |date=5 August 2001}}
3. ^{{cite web |last1=Parmentier |first1=Bruno |title=Gourdou Leseurre GL-821 HY 02 |url=https://www.aviafrance.com/aviafrance1.php?ID=9313&ID_CONSTRUCTEUR=582&ANNEE=0&ID_MISSION=0&MOTCLEF= |website=Aviafrance |accessdate=1 February 2019 |location=Paris |language=fr |date=29 April 2003}}
{{Gourdou-Leseurre aircraft}}

2 : French military reconnaissance aircraft 1930–1939|Gourdou-Leseurre aircraft

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