请输入您要查询的百科知识:

 

词条 Siemens-Schuckert DDr.I
释义

  1. Design and development

  2. Specifications

  3. References

name=DDr.1 image=Siemens D Dr I.jpg caption=

}}{{Infobox Aircraft Type

type=Triplane fighter aircraft national origin=Germany manufacturer=Siemens-Schuckert designer= first flight=9 November 1917 introduced= retired= status= primary user= more users= produced= number built=1 program cost= unit cost= developed from= variants with their own articles=
}}

The Siemens-Schuckert DDr.I was a World War I German twin engine, push-pull configuration triplane fighter aircraft. Only one was built, crashing on its first flight.

Design and development

The unusual DDr.I was one of the first aircraft to have two engines on the same centre line, one in tractor configuration and the other a pusher, an arrangement usually known as tandem push-pull. It was a triplane with constant chord, straight edged, square tipped wings of equal span and marked stagger. These were divided into two bays by pairs of near-parallel interplane struts. The upper wing was braced over the fuselage with a pair of N-form struts, leaning inward from the upper fuselage to common mountings on the wing centre line. The middle wing of the triplane was positioned at shoulder height on the fuselage and the lower wing passed unbraced below. There were short span ailerons on each wing.[2]

The smoothly faired and contoured short fuselage of the DDr.I positioned the open pilot's cockpit between two {{convert|110|hp|kW|abbr=on|0}} Siemens-Halske Sh.I nine cylinder rotary engines, one with a two blade tractor propeller and the other driving a four blade pusher turning just aft of the lower wing trailing edge. The empennage was mounted on four longitudinal, tubular outrigger beams, braced with vertical and transverse members. There were no fixed rear surfaces; the single piece, constant chord elevator reached between the two upper beams and a pair of similarly shaped rudder went from the upper to the lower beams, hinged further aft than the elevator but with their lower ends on a hinged frame that moved with it. The DDr.I had a fixed conventional undercarriage, with its mainwheels on a single axle mounted on wide spread V-struts attached to the lower fuselage at the lower corner points of each engine's firewall.[2]

Engine control problems and a lack of stability experienced in the first flight, made on 9 November 1917, led to a crash; the aircraft was not rebuilt and plans for a more powerful version, the DDr.II, powered by two {{convert|160|hp|kW|abbr=on|0}}, Siemens-Halske Sh.III eleven cylinder rotary engines were abandoned.[2]

Specifications

{{Aircraft specs
|ref=German Aircraft of the First World War
|prime units?=met


|genhide=
|crew=One
|length m=5.8
|length note=
|span m=10.9
|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=
|height m=
|height ft=
|height in=
|height note=
|wing area sqm=30
|wing area note=
|aspect ratio=
|airfoil=
|empty weight kg=680
|empty weight note=
|gross weight kg=910
|gross weight note=
|max takeoff weight kg=
|max takeoff weight lb=
|max takeoff weight note=
|fuel capacity=
|more general=


|eng1 number=2
|eng1 name=Siemens-Halske Sh.1
|eng1 type=9-cylinder rotary
|eng1 hp=110
|eng1 note=
|power original=
|more power=
|prop blade number=2/4
|prop name=; the tractor propeller had two blades and the pusher four.
|prop dia m=
|prop dia ft=
|prop dia in=
|prop dia note=


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


|guns=2×7.9 mm (0.311 in) calibre LMG 08/15 (Spandau) synchronised machine guns
}}{{aircontent
|see also=
|related=
|similar aircraft=
|lists=
}}

References

1. ^{{cite book |last=Green |first=William |first2= Gordon|last2= Swanborough |title=The Complete Book of Fighters |date=1994|publisher=Salamander Books|location=Godalming, UK|isbn=1-85833-777-1|page=530}}
[1]
}}{{Siemens-Schuckert aircraft}}

6 : Triplanes|Twin-engined push-pull aircraft|German fighter aircraft 1910–1919|Siemens-Schuckert aircraft|Aircraft first flown in 1917|Rotary-engined 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:2024/9/30 18:35:17