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词条 Handley Page H.P.22
释义

  1. Development

  2. Specifications (H.P.22)

  3. References

     Notes  Bibliography 
{{Use dmy dates|date=January 2018}}{{Use British English|date=January 2018}}
name=H.P. 22 & 23 image= caption=

}}{{Infobox Aircraft Type

type=Light single-seat sport national origin=United Kingdom manufacturer=Handley Page designer=W.H.Sayers first flight=1923 introduced= retired= status= primary user= number built=3 developed from= variants with their own articles=
}}

The Handley Page H.P.22 and H.P.23 were single-seat sport monoplanes produced for the 1923 Lympne light aircraft trials. They were not successful.

Development

With prizes worth a total of £2,150, the Lympne light aircraft competition of October 1923 attracted 28 entries including the Avro 558, de Havilland Humming Bird and Gloster Gannet. Handley Page provided three contestants,[1] at that time without a company type letter but bearing the competition numbers 23, 25 and 26. These were designed by W.H Sayers, technical editor of The Aeroplane and owed much to a glider that he, along with Frank Courtney and Maurice Wright had designed and built for the glider competition held at Itford Hill the previous year. In the later 1920s, when Handley Page began using the familiar H.P. numbering system they retrospectively named the initially similar no.23 and 25 the H.P.22 and no.26 became the H.P.23.[2]

As originally completed, all three aircraft had much in common. They had almost constant chord wings that carried ailerons fitted with slots for low speed control. The fuselage was of square cross-section, with the underside tapering towards the tail. There was no fixed tailplane, only an elevator, and both types had a fixed triangular fin. On the H.P.22s this carried a rectangular, unbalanced rudder, but the H.P.23's rudder was rounded on the trailing edge and horn-balanced. The open cockpit was ahead of the wings and the undercarriage had two small wheels, mounted inboard on the fuselage on the H.P.22 and outboard on the H.P.23. The main differences between the two types came about because the H.P.23 was designed for the speed prizes rather than those for flight duration. It therefore had a much shorter span of 20 ft (6.1 m) compared with 36 ft 6 in (11.13 m) for the H.P.22. This wing had full span leading edge slots and camber changing flaps. Both types had their engine mounted on a pylon immediately ahead of the pilot. The H.P.22 used a 397 cc ABC flat-twin and the H.P.23 a 750 cc Blackburne V-twin, the latter requiring slight changes to the pylon and nose.[1][3]

No.23 proved impossible to get airborne, even when the little ABC was replaced with a 500 cc Douglas. No. 25 was therefore reworked: the wing was lowered to shoulder height with its incidence increased to 7°, the ABC engine was faired in and the cockpit faired over apart from two small viewing ports, giving a smooth nose profile.[1][4] Thus modified, with a lightweight pilot and bungee-cord takeoff assistance, allowed under the rules, no.25 took part in the competition though without success. The H.P.23 could not be completed in time for the competition. It was later bought by the Air Ministry and moved to Martlesham, though it never flew there.[1]

Specifications (H.P.22)

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|ref={{Harvnb|Barnes|James|1987|pages=444}}
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|crew=one
|capacity=
|length m=6.4
|length ft=21
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|span m=11.13
|span ft=36
|span in=6
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|rot dia in=
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|dia in=
|width m=
|width ft=
|width in=
|height m=
|height ft=
|height in=
|wing area sqm=14.9
|wing area sqft=161
|swept area sqm=
|swept area sqft=
|rot area sqm=
|rot area sqft=
|volume m3=
|volume ft3=
|aspect ratio=
|wing profile=
|empty weight kg=113
|empty weight lb=250
|gross weight kg=195
|gross weight lb=430
|lift kg=
|lift lb=
|eng1 number=1
|eng1 type=397 cc ABC
|eng1 kw=
|eng1 hp=unknown
|eng1 kn=
|eng1 lbf=
|eng1 kn-ab=
|eng1 lbf-ab=
|eng2 number=
|eng2 type=
|eng2 kw=
|eng2 hp=
|eng2 kn=
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|eng2 kn-ab=
|eng2 lbf-ab=
|perfhide=Y
|max speed kmh=
|max speed mph=
|max speed mach=
|cruise speed kmh=
|cruise speed mph=
|stall speed kmh=
|stall speed mph=
|range km=
|range miles=
|endurance h=
|endurance min=
|ceiling m=
|ceiling ft=
|g limits=
|roll rate=
|glide ratio=
|climb rate ms=
|climb rate ftmin=
|sink rate ms=
|sink rate ftmin=
|armament1=
|armament2=
|armament3=
|armament4=
|armament5=
|armament6=
}}{{aircontent
|see also=
|related=
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}}

References

Notes

1. ^{{Harvnb|Barnes|James|1987|pages=239–44}}
2. ^{{Harvnb|Barnes|James|1987|pages=599}}
3. ^Flight 11 October 1923 p.626
4. ^Flight 18 October 1923 p.640

Bibliography

{{refbegin}}
  • {{cite book |title= Handley Page Aircraft since 1907|last= Barnes|first=C.H. |last2=James|first2=D. N.|year=1987 |publisher=Putnam Publishing |location=London |isbn= 0-85177-803-8|ref=harv}}
{{refend}}{{Handley Page aircraft}}

3 : British sport aircraft 1920–1929|Handley Page aircraft|Aircraft first flown in 1923

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