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词条 Heinkel HD 20
释义

  1. Design and development

  2. Operational history

  3. Specifications

  4. References

name=Heinkel HD 20 image=Heinkel HD-20 left front Aero Digest December 1926.jpg caption=

}}{{Infobox Aircraft Type

type=Three seat photographic survey and mapping aircraft national origin=Germany manufacturer=Heinkel Flugzeugwerke designer= first flight=c.1926 introduced= retired= status= primary user= more users= produced= number built=At least one program cost= unit cost= developed from= variants with their own articles=
}}

The Heinkel HD 20 was a twin engine, three seat German biplane built in 1926 for civil survey work.

Design and development

The Heinkel HD 20 was one of the early products of post-World War I aircraft companies after the Allies aviation ban was lifted.[1] HD stood for {{lang-de|Heinkel Doppeldecker}} or Heinkel biplane.

The HD.20 had unswept wings of mixed construction with wooden spars, two in the upper wing and one in the lower, and steel ribs; they were fabric covered. Both wings had constant chord over the inner section and semi-elliptical outer panels. The upper wing was considerably the larger, with 45% greater overall span and 17% greater chord over the inner panels. The wings were mounted with slight and equal dihedral and considerable stagger. Only the upper wings carried the long span, narrow chord ailerons. The lower wings were mounted directly onto the lower fuselage structure and the upper wing centre-section was joined to the upper fuselage with a pair of steel inverted V-struts on each side and a central parallel pair arranged transversely. It was a single bay biplane with V-form interplane struts leaning outward strongly from the lower wing below the engines to the upper wings at about 55% span.

It was powered by two {{convert|200|hp|kW|abbr=on|order=flip}} Wright R-790 Whirlwind

nine cylinder radial engines, mounted in streamlined cowlings with the cylinder heads protruding for cooling. They were fed from fuel tanks in the upper wing; oil tanks were in the cowlings. Each engine was bolted to a frame formed of the interplane struts, a nearly horizontal V-strut to the upper fuselage and an N-form strut from the lower wing to the upper fuselage.[1]

The square cross-section fuselage was formed with steel tubes and covered with fabric, with a light, rounded, wooden upper decking. There were three open cockpits: one in the nose, another under the upper wing and the last, from which it was flown, just behind the upper trailing edge which had a shallow, rounded cut-out to aid the pilot's forward view. The tail surfaces were conventional and straight-edged, with angled leading edges and unswept trailing edges. The tailplane, mounted on the upper fuselage, was braced from below to the fuselage with a single strut on each side. Both the rudder and elevators were balanced; the latter were separate, their inner corners cut away for deflections of the deep rudder.[1]

The HD.20 had a conventional tailskid undercarriage. Each mainwheel was mounted on a group of three struts, two to the lower fuselage longeron at points on the wing leading edge and at mid-chord and the third to the upper longeron. There was a solid rubber shock absorber in each hub. The wheels could be replaced with floats.[1]

Operational history

Rather little is known about the history of the HD 20. From the January 1927 date of the Les Ailles article[1] the first flight was probably in later 1926. The number built is also not known. One (D-1157), which appears on a reconstructed civil register, was owned by the Epro advertising agency and was destroyed on 21 November 1929.[6] The HD.20 is also mentioned as a photographic survey aircraft in a 1930 review of the topic, though it does not show the camera positions.

Specifications

{{Aircraft specs
|ref=Les Ailes, 6 January 1927[1]
|prime units?=met


|genhide=
|crew=Three
|length m=9.45
|length note=
|upper span m=12.80
|upper span note=
|mid span m=
|lower span m=8.80
|lower span note=
|height m=3.52
|height note=
|wing area sqm=39.80
|wing area note=
|aspect ratio=
|airfoil=
|empty weight kg=1315
|empty weight note=
|gross weight kg=1965
|gross weight note=
|max takeoff weight kg=
|max takeoff weight lb=
|max takeoff weight note=
|fuel capacity={{convert|340|l|Impgal USgal|abbr=on}}
|more general=


|eng1 number=2
|eng1 name=Wright R-790 Whirlwind
|eng1 type=9-cylinder radial
|eng1 hp=200
|eng1 note=
|power original=
|more power=
|prop blade number=2
|prop name=metal, Reed Propellers
|prop dia m=
|prop dia ft=
|prop dia in=
|prop dia note=


|perfhide=
|max speed kmh=195
|max speed note= at {{convert|500|m|ft|abbr=on}}
|cruise speed kmh=180
|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=85
|minimum control speed note=
|range km=
|range miles=
|range nmi=
|range note=
|endurance=4.5 hr
|ceiling m=6000
|ceiling ft=
|ceiling note=
|g limits=
|roll rate=
|glide ratio=
|climb rate ms=
|climb rate ftmin=
|climb rate note=
|time to altitude=35 min to {{convert|5000|m|ft|abbr=on}}
|sink rate ms=
|sink rate ftmin=
|sink rate note=
|lift to drag=
|wing loading kg/m2=
|wing loading lb/sqft=
|wing loading note=
|fuel consumption kg/km=
|fuel consumption lb/mi=
|power/mass=
|more performance=
}}

References

{{Commons category}}
1. ^{{cite journal|date=6 January 1927 |title=L'Avion de 'Travail' Heinkel|journal=Les Ailes|issue=290|pages=3 |url=http://gallica.bnf.fr/ark:/12148/bpt6k65683225/f3}}
2. ^{{cite web |url=http://www.airhistory.org.uk/gy/reg_D-.html|title=Golden Years of Aviation |author= |date= |work= |publisher= |accessdate=2 November 2015}}
[1][2]
}}{{Heinkel aircraft}}

2 : German civil aircraft 1920–1929|Heinkel aircraft

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