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词条 De Havilland Highclere
释义

  1. Development

  2. Operational history

  3. Unbuilt variants

  4. Specifications

  5. References

{{Use dmy dates|date=February 2018}}{{Use British English|date=February 2018}}
name=Highclere image=DH Highclere.jpg caption=

}}{{Infobox Aircraft Type

type=Airliner national origin=United Kingdom manufacturer=de Havilland Aircraft Co. Ltd. designer= first flight=18 June 1925 introduced= retired=1927 status= primary user= number built=1 developed from= variants with their own articles=
}}

The de Havilland DH.54 Highclere was a single-engined 15-passenger biplane airliner designed to replace the DH.34. Its development ended when Imperial Airways decided to use only multi-engined types.

Development

The DH.54 Highclere[1] was designed to Air Ministry specification 40/22 for a larger version of the very successful DH.34 and the two aircraft had much in common, both in construction and general layout. Compared with the DH.34, the Highclere's passenger complement increased from nine to twelve, its all-up weight by 56% and its wing area by 70%. They were both single-engined two-bay biplanes with fabric-covered wooden wings and with wooden-framed fuselages covered with thin plywood.[1]

Size apart, the wings of the Highclere differed[1] in having no stagger, no upper wing dihedral and in having a larger inter-wing gap, the upper wing now attached to the fuselage by cabane struts rather than directly to the upper fuselage. In response to criticism of the DH.34's high landing speed, full-span flaps were fitted. To reduce the hazards of ditching, the undercarriage could be jettisoned and the fuselage was made watertight. Passengers sat in four rows of seats, singles on the left and doubles on the right. A rearrangement of luggage space allowed room for toilets. The Highclere had balanced elevators. The weight increase required an increase in power, so the Highclere used a 650 hp (485 kW) Rolls-Royce Condor IIIA water-cooled inline engine which lengthened the nose and drove a four-bladed propeller of 14 ft (4.27 m) diameter.[1]

Operational history

The Highclere was first flown by H.S. Broad on 18 June 1925[5] and was soon carrying non-paying passengers and winning races.[1] Owned by the Air Ministry throughout its life, it went to RAF Martlesham Heath for successful airworthiness tests early in 1926, with the Certificate of Airworthiness awarded on 23 April 1926. By then, though Imperial Airways had decided no longer to transport passengers in single-engined types for safety reasons and the sole Highclere was transferred to RAE Farnborough on 7 March 1926 for experimental work. On 7 November 1926[2] it was loaned to Imperial Airways at Croydon Airport as a freighter and some thought was given to modifications to make the Highclere better fitted to this role,[1] but it was destroyed when a hangar collapsed in heavy snow at Croydon on 1 February 1927.

Unbuilt variants

DH.55

Unbuilt design for 12-seat transport powered by three 120 hp (90 kW) Airdisco engines.[3]

DH.57

Unbuilt derivative of DH.55 with three 230 hp (172 kW) Siddeley Puma engines.[3]

Specifications

{{aerospecs
|ref={{Harvnb|Jackson|1978|pages=212}}
|met or eng?=eng
|crew=two
|capacity=twelve
|length m=15.54
|length ft=51
|length in=0
|span m=20.78
|span ft=68
|span in=2
|swept m=
|swept ft=
|swept in=
|rot number=
|rot dia m=
|rot dia ft=
|rot dia in=
|dia m=
|dia ft=
|dia in=
|width m=
|width ft=
|width in=
|height m=4.64
|height ft=15
|height in=2½
|wing area sqm=93.27
|wing area sqft=1,004
|swept area sqm=
|swept area sqft=
|rot area sqm=
|rot area sqft=
|volume m3=
|volume ft3=
|aspect ratio=
|wing profile=
|empty weight kg=3,070
|empty weight lb=6,768
|gross weight kg=5,103
|gross weight lb=11,250
|lift kg=
|lift lb=
|eng1 number=1
|eng1 type=Rolls-Royce Condor IIIA
|eng1 kw=485
|eng1 hp=650
|eng1 kn=
|eng1 lbf=
|eng1 kn-ab=
|eng1 lbf-ab=
|eng2 number=
|eng2 type=
|eng2 kw=
|eng2 hp=
|eng2 kn=
|eng2 lbf=
|eng2 kn-ab=
|eng2 lbf-ab=
|max speed kmh=177
|max speed mph=110
|max speed mach=
|cruise speed kmh=161
|cruise speed mph=100
|stall speed kmh=
|stall speed mph=
|range km=644
|range miles=400
|endurance h=
|endurance min=
|ceiling m=
|ceiling ft=
|g limits=
|roll rate=
|glide ratio=
|climb rate ms=2.95
|climb rate ftmin=580
|sink rate ms=
|sink rate ftmin=
|armament1=
|armament2=
|armament3=
|armament4=
|armament5=
|armament6=
}}{{aircontent
|see also=
|related=
|similar aircraft=
|lists=
}}

References

{{commons category|De Havilland DH.54 Highclere}}
1. ^{{Harvnb|Jackson|1978|pages=210–2}}
2. ^{{harvnb|Jackson|1988|p=302}}
3. ^{{harvnb|Jackson|1987|p=519}}
  • {{cite book |title= de Havilland Aircraft since 1909|last= Jackson|first=A.J.| year=1978 |publisher=Putnam Publishing |location=London |isbn=0-370-30022-X|ref=harv }}
  • {{cite book|last=Jackson|first=A.J.|title=De Havilland Aircraft since 1909|publisher=Putnam|location=London|year=1987|edition=3rd|isbn=0-85177-802-X|ref=harv}}
  • {{cite book |title= British Civil Aircraft 1919-1972 vol II|last= Jackson|first=A.J.| year=1988 |publisher=Putnam Publishing |location=London |isbn=0-85177-813-5|ref=harv}}
{{refbegin}}{{refend}}{{de Havilland aircraft}}

2 : British airliners 1920–1929|De Havilland aircraft

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