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词条 Dyle et Bacalan DB-10
释义

  1. Design

  2. Operational history

  3. Specifications

  4. References

  5. External links

name=DB-10 image=Dyle et Bacalan DB-10 right front photo NACA Aircraft Circular No.27.jpg caption=

}}{{Infobox Aircraft Type

type=Heavy night bomber national origin=France manufacturer=Dyle et Bacalan, Bordeaux designer= first flight=1926 introduced= retired= status= primary user= more users= produced= number built=1 program cost= unit cost= developed from= variants with their own articles=
}}

The Dyle et Bacalan DB-10 was a heavy night bomber, designed in France and flown in 1926. It was a twin engine, high wing, metal frame monoplane, distinguished by a very thick centre section wing which formed the forward fuselage and housed the engines.

Design

In 1925 the well-established naval ship builders Société Anonyme de Travaux Dyle et Bacalan, based in Bordeaux, developed an aircraft manufacturing interest. Their first production was a high wing, twin engine heavy bomber, the DB-10. Like their later aircraft, the DB-10 was structurally an all-metal machine. In most respects the DB-10 was a conventional design for its day but it had one feature, a very thick wing centre section blended into the fuselage, which was also to become a characteristic of later Dyle et Bacalan aircraft.

At the front of the DB-10 the thick aerofoil centre section stretched unbroken between the engines, which were mounted upon it. Beyond the engines outer wings of normal thickness and constant chord, significantly thinner and narrower than the inboard section, were each supported by a pair of parallel struts to the lower edge of the centre section. Wing spars and struts were made of steel tubing, with duralumin ribs. A conventional, rectangular section, fuselage with duralumin longerons emerged from the centre section as the thick aerofoil thinned, carrying a tailplane on its upper surface, braced from below. It also carried a single fin and a deep rudder, which moved in a cut-out between the elevators. All surfaces, except those housing the uncowled Gnome-built Bristol Jupiter radial engines, were fabric. The DB-10 had a fixed, conventional undercarriage with each single, partly cowled, mainwheel mounted on a parallel pair of V-shaped struts behind the engines. The outer pair of struts was fixed close to the lower ends of the wing struts, at the edge of the thick aerofoil. A tailwheel was mounted at the rear of the fuselage, just in front of the rudder.[2][3]

The thick centre section enclosed vertical bomb racks as well as fuel tanks.[2] Open cockpits for the crew were built on top of it, starting with a navigator/bombardier's or gunner's position at the extreme leading edge. Immediately behind but stepped above it was the pilot's cockpit, with another cockpit just aft where the raised crew housing ended. There was a separate dorsal gunner's position, fitted with a gun ring, on the fuselage proper.[3]

Operational history

The DB-10 was entered into the 1926 French government BN3 competition for a new three man night bomber, held at Villacoublay where it flew against such aircraft as the Amiot 122, the Farman F.123, the Latécoère 19 and the eventual winner the Lioré et Olivier LéO 20. Only one DB-10 was built, though the company persisted with the thick wing idea in its later DB-70 transport aircraft.

Specifications

{{Aircraft specs
|ref=Flight December 1926[2], Air International:Plane Facts: The French "Burnelli"[1], Aviafrance:Dyle et Bacalan DB-10[3], Jane's all the World's Aircraft 1928[2]
|prime units?=met


|crew=3/4
|length m=13.60
|span m=25
|height m=3.80
|wing area sqm=93.0
|aspect ratio=
|airfoil=
|empty weight kg=3150
|gross weight kg=5600
|max takeoff weight kg=
|max takeoff weight lb=
|max takeoff weight note=
|fuel capacity=
|more general=


|eng1 number=2
|eng1 name=Gnome et Rhône 9A Jupiter
|eng1 type=9-cylinder radial
|eng1 hp=480
|prop blade number=2
|prop name=fixed pitch wooden propellers
|prop dia m=
|prop dia ft=
|prop dia in=
|prop note=


|max speed kmh=195
|max speed note=at sea level

{{cvt|173|km/h|mph kn}} at {{cvt|4000|m}}


|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=
|ceiling m=5500
|g limits=
|roll rate=
|climb rate ms=
|climb rate ftmin=
|climb rate note=
|time to altitude=
|wing loading kg/m2=60.1
|power/mass={{cvt|0.0685|hp/lb|kW/kg|order=flip}}
|more performance=


|guns= 2× {{cvt|7.7|mm|3}} Lewis guns in nose gunner's position
|bombs= {{cvt|1300|kg}} bombs in internal bomb bay
}}

References

{{Commons category}}
1. ^{{cite magazine|title=Plane Facts: The French "Burnelli"|magazine=Air International|issue=August 1976|page=94}}
2. ^{{cite book |title=Jane's all the World's Aircraft 1928 |editor1-last=Grey |editor1-first=C.G. |year=1928 |publisher=Sampson Low, Marston & company, ltd |location=London |pages=98c}}
3. ^{{cite magazine |last= |first= |authorlink= |coauthors= |year= |month= |title=Dyle et Bacalan|magazine= Flight|volume= |issue=2 December 1926 |page=778 |id= |url= http://www.flightglobal.com/pdfarchive/view/1926/1926%20-%200878.html |accessdate= |quote= }}
4. ^{{cite web |url=http://www.aviafrance.com/dyle-et-bacalan-db-10-aviation-france-4849.htm |title=Dyle et Bacalan DB-10 |author= |date= |work= |publisher= |accessdate=2010-12-27}}
[3][4]
}}

External links

  • [https://www.youtube.com/watch?v=TTGki_q8aO8 The Dyle et Bacalan DB-10 in flight]
{{Dyle et Bacalan aircraft}}{{DEFAULTSORT:Dyle Et Bacalan Db-10}}

4 : French bomber aircraft 1920–1929|Twin-engined tractor aircraft|High-wing aircraft|Dyle et Bacalan aircraft

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