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Bristol Ten-seater

From Wikipedia, the free encyclopedia
British biplanes

Ten-seater/Brandon
General information
TypeTransport
ManufacturerBristol Aeroplane Company
Designer
Number built3
History
Introduction date1922
First flight21 June 1921
Retired1926

TheBristol Ten-seater andBristol Brandon wereBritish single-enginebiplane transport aircraft built by theBristol Aeroplane Company in the early 1920s. Only three were built, two of which were used as civil transports and one of which (the Bristol Brandon) served with theRoyal Air Force.

Design and development

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In 1919 and 1920,Frank Barnwell, chief designer of theBristol Aeroplane Company, considered designs for a commercial transport aircraft, ranging from single-engine, three-seat aircraft to four-engine aircraft carrying ten passengers, none of which were built. Early in 1921, theBritish government decided to provide subsidies for approved airlines, so Bristol's management authorised Barnwell to proceed with a design for a single-engined transport aircraft. It was intended to be powered by aBristol Jupiter engine, but this had not yet been type-approved, so the initialprototype was fitted with aNapier Lion engine instead.[1]

The Lion-engined prototype, theBristol Type 62, orBristol Ten-seater, with the registrationG-EAWY first flew on 21 June 1921.[2] The Ten-seater was a large, two-baybiplane, with a cabin for nine passengers and a forwardcockpit for the single pilot.[3]

Ten-seater in 1921

The second aircraft, theBristol Type 75 was powered by the preferred Jupiter engine, which was mounted forward of a fireproof bulkhead, with the entire engine installation (or "power-egg") capable of being swung open like a gate to allow easy access to the rear of the engine. The Type 75 was designed to accommodate eight passengers and two crew. This aircraft, registeredG-EBEV, first flew in July 1922.[2] A third aircraft, theBristol Type 79 was ordered by the Air Council to meet a requirement (Specification 32/22) for a single-engined ambulance landplane for theRoyal Air Force. It was fitted with wings of greaterchord, and had accommodation for three stretchers and an attendant or two stretchers and four sitting patients.[4]

Operational history

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The Type 62 had itsCertificate of Airworthiness awarded on 14 February 1922[5] and was transferred toInstone Air Line for service on itsLondon-to-Paris route, carrying both passengers and cargo. It was later transferred toHandley Page Transport Ltd.[3]

The Type 75 received its Certificate of Airworthiness on 16 July 1924.[6] By this time, Instone Air Lines had merged with the other three subsidised British airlines to formImperial Airways. Imperial had a policy of using only multi-engine aircraft for passenger flights, so the Type 75 was converted into a freighter to carry 1,800 lb (820 kg) of cargo, going into service on the London-Cologne route on 22 July 1924,[2] continuing in service until 1926.

The Type 79 first flew on 19 March 1924 and was delivered to the RAF, who named the aircraft theBristol Brandon in 1925. It was overweight at full load and did not go into overseas service, being used as an ambulance atRAF Halton together with theAvro Andover.[7]

Variants

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Bristol Type 62
First aircraft, powered by 450 hp (340 kW)Napier Lion engine.[8]
Bristol Type 75
Second aircraft, powered by 425 hp ( kW)Bristol Jupiter IV engine.[9]
Bristol Type 79
Third aircraft built as a military transport and air ambulance aircraft for the RAF. Powered by Bristol Jupiter IV engine.

Operators

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 United Kingdom

Specifications (Type 75)

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Bristol Ten Seater 2-view .drawing from L'Aéronautique July 1921

Data fromBristol Aircraft Since 1910.[10]

General characteristics

  • Crew: 2
  • Capacity: 8 passengers / 1,800 lb (816 kg) payload
  • Length: 40 ft 6 in (12.34 m)
  • Wingspan: 56 ft 0 in (17.07 m)
  • Height: 11 ft 0 in (3.35 m)
  • Wing area: 700 sq ft (65 m2)
  • Empty weight: 4,000 lb (1,814 kg)
  • Gross weight: 6,755 lb (3,064 kg)
  • Powerplant: 1 ×Bristol Jupiter IV 8-cylinder air-cooled radial piston engine, 425 hp (317 kW)
  • Propellers: 2-bladed fixed-pitch propeller

Performance

  • Maximum speed: 110 mph (180 km/h, 96 kn)
  • Endurance: 5 hours 30 minutes
  • Service ceiling: 8,500 ft (2,600 m)
  • Wing loading: 9.65 lb/sq ft (47.1 kg/m2)
  • Power/mass: 0.063 hp/lb (0.104 kW/kg)

See also

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Aircraft of comparable role, configuration, and era

References

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Citations

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  1. ^Barnes 1964, pp.156–157.
  2. ^abcBarnes 1964, p.157.
  3. ^ab"Bristol 75 Ten Seater". Imperial Airways. Archived from the original on 15 August 2016. Retrieved2 August 2018.
  4. ^Barnes 1964, p.158.
  5. ^Jackson 1974, p.307.
  6. ^Jackson 1974, p.308.
  7. ^"Type 79 – Ambulance". Aviation Archive. Retrieved29 October 2015.
  8. ^"Bristol Ten-Seater"Flight, 19 November 1921, bottom of page – early photo fitted with Napier Lion engine and double main landing gear; next page shows interior of aircraft
  9. ^"The Bristol 10-Seater Commercial Aeroplane"FLIGHT, 19 January 1922
  10. ^Barnes 1964, p.159.

Bibliography

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  • Barnes, C.H. (1964).Bristol Aircraft Since 1910 (First ed.). London: Putnam.
  • Jackson, A.J. (1974).British Civil Aircraft since 1919 Volume 1. London: Putnam.ISBN 0-370-10006-9.

External links

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