请输入您要查询的百科知识:

 

词条 Latécoère 611
释义

  1. Development and design

  2. Operational history

  3. Variants

  4. Operators

  5. Specifications (Latécoère 611)

  6. See also

  7. References

  8. External links

name = Latécoère 611image = caption =

}}{{Infobox Aircraft Type

type = Flying Boatmanufacturer = Latécoèredesigner = first flight = 8 March 1939introduced = 1940introduction= retired = 1947status = primary user = French Navymore users = produced = number built = 1unit cost =developed from = variants with their own articles =
}}

The Latécoère 611 was a French four-engined maritime reconnaissance flying boat of the Second World War. Although only a single prototype was completed, this served throughout the war, being used by both the Vichy French and Free French navies.

Development and design

In May 1935, the French Navy issued a specification for a long-range flying boat to replace the obsolete Breguet 521. To meet this requirement, Latécoère designed the Latécoère 611. This was a cantilever monoplane powered by four Gnome-Rhone 14N radial engines and fitted with a twin tail. It was also fitted with stabilising floats that retracted into the outer engine nacelles. The prototype was assembled at Biscarrosse, and first flew on 8 March 1939.[1]

Although it was intended that the aircraft be armed with a 25 mm cannon in a dorsal turret, this was unavailable, and was replaced by one carrying two 7.5 mm Darne machine guns, with a further four machine guns firing through portholes and two in a retractable tail position. In December 1939 the French Navy placed an order for twelve of a modified version, the Latécoère 612, which was to be powered by four Pratt & Whitney R-1830 radial engines. These aircraft, however, were never delivered.

Operational history

The prototype Latécoère 611 was delivered to the French Navy on 12 April 1940[1] and named Achenar, being flown to North Africa in June 1940 and subsequently disarmed under the terms of the Armistice. After being damaged in a collision with another flying boat, it eventually entered full service with the Vichy French Navy on 15 October 1941, operating with Escadrille 4E at Port Lyautey and Dakar.[1]

In November 1942, following the Allied Invasion of North Africa, Escadrille 4E switched sides and joined the Free French, carrying out anti-submarine patrols over the South Atlantic, later (October 1943) being enlarged to form Flotille 7F, which continued to fly the Latécoère 611 alongside Short Sunderlands. The Latécoère was re-armed in 1944, with the dorsal turret being fitted with two 50 cal. Browning machine guns and a similar gun being fitted in the tail.[1]

The sole Latécoère 611 was finally retired from service as a transport in 1947.[2]

Variants

Latécoère 610

Design studies for a military flying boat to have been powered by 4x {{convert|1000|hp|kW|abbr=on}} Hispano-Suiza 14AA-02 / Hispano-Suiza 14AA-03 engines, (left and right handed rotation).

Latécoère 611

Prototype – powered by four Gnome-Rhône 14N-30 / Gnome-Rhône 14N-31 engines, (left and right handed rotation), given the name Achernar. One built.

Latécoère 612

Proposed production version – powered by four Pratt & Whitney R-1830 engines, (twelve ordered but unbuilt).

Operators

{{FRA}}
  • French Navy

Specifications (Latécoère 611)

{{Aircraft specs
|ref=Warplanes of the Second World War, Volume Five, Flying Boats [1]
|prime units?=met


|genhide=
|crew=7
|capacity=
|length m=27.06
|length ft=
|length in=
|length note=
|span m=40.56
|span ft=
|span in=
|span note=
|upper span m=
|upper span ft=
|upper span in=
|upper span note=
|mid span m=
|mid span ft=
|mid span in=
|mid span note=
|lower span m=
|lower span ft=
|lower span in=
|lower span note=
|swept m=
|swept ft=
|swept in=
|swept note=
|dia m=
|dia ft=
|dia in=
|dia note=
|width m=
|width ft=
|width in=
|width note=
|height m=7.65
|height ft=
|height in=
|height note=
|wing area sqm=195.1
|wing area sqft=
|wing area note=
|swept area sqm=
|swept area sqft=
|swept area note=
|volume m3=
|volume ft3=
|volume note=
|aspect ratio=
|airfoil=
|empty weight kg=16,034
|empty weight lb=
|empty weight note=
|gross weight kg=26,555
|gross weight lb=
|gross weight note=
|max takeoff weight kg=31,065
|max takeoff weight lb=
|max takeoff weight note=
|fuel capacity=
|lift kg=
|lift lb=
|lift note=
|more general=


|eng1 number=2
|eng1 name=Gnome-Rhône 14N-30
|eng1 type=14 cyl. air-cooled radial engine
|eng1 kw=735
|eng1 hp=
|eng1 shp=
|eng1 kn=
|eng1 lbf=
|eng1 note=
|power original=
|thrust original=
|eng1 kn-ab=
|eng1 lbf-ab=
|eng2 number=2
|eng2 name= Gnome-Rhône 14N-31
|eng2 type=14 cyl. air-cooled radial engine
|eng2 kw=735
|eng2 hp=
|eng2 shp=
|eng2 kn=
|eng2 lbf=
|eng2 note=
|eng2 kn-ab=
|eng2 lbf-ab=
|eng3 number=
|eng3 name=
|eng3 type=
|eng3 kw=
|eng3 hp=
|eng3 shp=
|eng3 kn=
|eng3 lbf=
|eng3 note=
|eng3 kn-ab=
|eng3 lbf-ab=
|more power=
|prop blade number=
|prop name=
|prop dia m=
|prop dia ft=
|prop dia in=
|prop dia note=
|rot number=
|rot dia m=
|rot dia ft=
|rot dia in=
|rot area sqm=
|rot area sqft=
|rot area note=


|perfhide=
|max speed kmh=349
|max speed mph=
|max speed kts=
|max speed note=
|max speed mach=
|cruise speed kmh=180
|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=4,250
|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=32 hours
|ceiling m=
|ceiling ft=
|ceiling note=
|g limits=
|roll rate=
|glide ratio=
|climb rate ms=
|climb rate ftmin=
|climb rate note=
|time to altitude={{convert|2,000|m|ft|abbr=on}} in 10 minutes
|sink rate ms=
|sink rate ftmin=
|sink rate note=
|lift to drag=
|wing loading kg/m2=
|wing loading lb/sqft=
|wing loading note=
|disk loading kg/m2=
|disk loading lb/sqft=
|disk loading note=
|fuel consumption kg/km=
|fuel consumption lb/mi=
|power/mass=
|thrust/weight=
|more performance=


|guns=

  • 1× {{convert|25|mm|in|abbr=on}} CA mle 39 cannon in a dorsal turret
  • 2× {{convert|7.5|mm|in|abbr=on}} Darne machine guns in a tail position
  • 4× {{convert|7.5|mm|in|abbr=on}} Darne machine guns in beam positions

|bombs= up to {{convert|802|kg|lb|abbr=on}} of bombs, depth charges, or torpedoes
|rockets=
|missiles=
|hardpoints=
|hardpoint capacity=
|hardpoint rockets=
|hardpoint missiles=
|hardpoint bombs=
|hardpoint other=
|avionics=
}}

See also

{{aircontent
|related=
|similar aircraft=
  • Blohm & Voss BV 222
  • Kawanishi H8K
  • Lioré et Olivier LeO H-246
  • Martin PBM Mariner
  • Potez-CAMS 141
  • Short Sunderland

|lists=
  • List of aircraft of the French Air Force during World War II
  • List of aircraft of World War II
  • List of seaplanes and amphibious aircraft

|see also=
}}

References

1. ^{{cite book |last= Green |first=William |title=Warplanes of the Second World War, Volume Five, Flying Boats |year= 1968|publisher= Macdonald|location=London|pages= 27–29 |isbn=0 356 01449 5 }}
2. ^{{cite web |url= http://www.netmarine.net/aero/bases/stmandrier/histoire/histoire04.htm|title= Histoire de la BAN Saint-Mandrier|accessdate=2007-08-14 |language=French}}

External links

{{commons category|Latécoère}}
  • aviafrance.com
{{Latécoère aircraft}}{{DEFAULTSORT:Latecoere 611}}

6 : French military reconnaissance aircraft 1930–1939|Flying boats|Four-engined tractor aircraft|High-wing aircraft|Aircraft first flown in 1939|Four-engined piston aircraft

随便看

 

开放百科全书收录14589846条英语、德语、日语等多语种百科知识,基本涵盖了大多数领域的百科知识,是一部内容自由、开放的电子版国际百科全书。

 

Copyright © 2023 OENC.NET All Rights Reserved
京ICP备2021023879号 更新时间:2024/11/12 8:01:27