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Bristol Brownie

The Bristol Type 91 Brownie was a light sports aircraft produced in the United Kingdom by the Bristol Aeroplane Company in 1924. It was a low-wing cantilever monoplane aircraft of conventional configuration with fixed tailskid undercarriage. The pilot and passenger sat in tandem open cockpits. It won the £1,000 pound prize for second place at the Lympne light aircraft trials in October 1924.

Type 91 Brownie
Role Sports aircraft
Manufacturer Bristol Aeroplane Company
Designer Frank Barnwell
First flight 6 August 1924
Number built 3

Design edit

Bristol had not built an aircraft to compete in the 1923 Lympne light aircraft trials, which had been for aircraft with engines of 750 cc or less, making use of Bristol's Cherub engine impossible. The rules were changed for the 1924 trials, permitting engines of up to 1,100 cc to be used, and accordingly Frank Barnwell started design work on a competitor early in 1924. He produced studies for alternative wood and metal aircraft, and after consideration of these the Board of Bristol Aircraft authorised the production of two aircraft on 4 February, adding a third on 5 May. All three aircraft had a similar fuselage, made of wire-braced high-tensile steel tubing, but for experimental purposes three different wing designs were produced: a 34 ft 7in (10.54m) span wooden wing and two different metal wings, one of 36 ft 7 in (11.15 m) span of all-steel construction, the other, intended for high-speed use, of 30 ft 7 in (9.32 m) span with combined steel and duralumin construction. To satisfy the rules of the competition the wings had to be readily detachable and the aircraft fitted with dual controls.

The three aircraft were registered G-EBJK, G-EBJL and G-EBJM on 14 July, and immediately named Jack, Jill and Jim. G-EBJK, fitted with the wooden wings, was the first flown, on 6 Aug piloted by Cyril Uwins. It performed and handled so well that a second flight was immediately made by Frank Barnwell, followed by a third by Uwins and Barnwell together. G-EBJL, which had the large metal wings fitted, first flew on 22 September and G-EBJM, completed as a single-seater with a long-range tank and the smaller metal wings, followed on 4 September.

All took part in the trials, which took place between 27 September and 4 October. Uwins, flying 'JK, winning second prize in the main trials. 'JL, to be flown by T.W. Campbell, was withdrawn because of aileron flutter, and Campbell in 'JM won third place in the Grosvenor Cup race, averaging over 70 mph.

Development edit

After the Lympne trials 'JK and 'JL were delivered to Martlesham Heath for evaluation as a primary trainer, but did not impress the Air Ministry enough for any development to be funded by them.

G-EBJK was returned to Filton for modifications in December 1925. It was fitted with the newly developed 36 hp Cherub III mounted slightly lower in the fuselage, and the top longerons were curved down more to improve the view from the rear cockpit. The fuel tank was enlarged and it was fitted with new metal wings giving it a span of 37 ft 7 in (11.45 m). This was designated Type 91A.

After further trials at Martlesham it was again returned to Filton, where the engine mounting was further lowered and a Fairey-Reed duralmin propeller fitted. Additionally, a curved decking was added to the rear fuselage, and it was fitted with an enlarged horn-balanced rudder and a new undercarriage using rubber shock absorbers. This was designated Type 91 B, or Brownie II. In this form the aircraft took place in the 1926 Lympne trials, where Uwins won the third place prize of £500.

Specifications (Brownie I, wooden wing) edit

 
Bristol Brownie 3-view drawing from NACA-TM-289

Data from Bristol Aircraft Since 1910[1]

General characteristics

  • Crew: 1
  • Capacity: 1 passenger
  • Length: 26 ft 3 in (8.00 m)
  • Wingspan: 34 ft 7 in (10.54 m)
  • Height: 6 ft 6 in (1.98 m)
  • Wing area: 204 sq ft (19.0 m2)
  • Empty weight: 500 lb (227 kg)
  • Gross weight: 870 lb (395 kg)
  • Powerplant: 1 × Bristol Cherub I 2-cylinder air-cooled horizontally-opposed piston engine, 32 hp (24 kW)
  • Propellers: 2-bladed fixed-pitch propeller

Performance

  • Maximum speed: 70 mph (110 km/h, 61 kn)
  • Range: 100 mi (160 km, 87 nmi)

See also edit

Aircraft of comparable role, configuration, and era Most British manufacturers produced aircraft to take part in the Lympne trials, and there are therefore a number of directly comparable aircraft, including:

References edit

Citations edit

  1. ^ Barnes 1964, p.193.

Bibliography edit

  • Barnes, C.H. (1964). Bristol Aircraft Since 1910 (First ed.). London: Putnam. ISBN 0-85177-823-2.
  • Taylor, Michael J. H. (1989). Jane's Encyclopedia of Aviation. London: Studio Editions. p. 206. ISBN 9781851703241.

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The Bristol Type 91 Brownie was a light sports aircraft produced in the United Kingdom by the Bristol Aeroplane Company in 1924 It was a low wing cantilever monoplane aircraft of conventional configuration with fixed tailskid undercarriage The pilot and passenger sat in tandem open cockpits It won the 1 000 pound prize for second place at the Lympne light aircraft trials in October 1924 Type 91 Brownie Role Sports aircraft Manufacturer Bristol Aeroplane Company Designer Frank Barnwell First flight 6 August 1924 Number built 3 Contents 1 Design 2 Development 3 Specifications Brownie I wooden wing 4 See also 5 References 5 1 Citations 5 2 BibliographyDesign editBristol had not built an aircraft to compete in the 1923 Lympne light aircraft trials which had been for aircraft with engines of 750 cc or less making use of Bristol s Cherub engine impossible The rules were changed for the 1924 trials permitting engines of up to 1 100 cc to be used and accordingly Frank Barnwell started design work on a competitor early in 1924 He produced studies for alternative wood and metal aircraft and after consideration of these the Board of Bristol Aircraft authorised the production of two aircraft on 4 February adding a third on 5 May All three aircraft had a similar fuselage made of wire braced high tensile steel tubing but for experimental purposes three different wing designs were produced a 34 ft 7in 10 54m span wooden wing and two different metal wings one of 36 ft 7 in 11 15 m span of all steel construction the other intended for high speed use of 30 ft 7 in 9 32 m span with combined steel and duralumin construction To satisfy the rules of the competition the wings had to be readily detachable and the aircraft fitted with dual controls The three aircraft were registered G EBJK G EBJL and G EBJM on 14 July and immediately named Jack Jill and Jim G EBJK fitted with the wooden wings was the first flown on 6 Aug piloted by Cyril Uwins It performed and handled so well that a second flight was immediately made by Frank Barnwell followed by a third by Uwins and Barnwell together G EBJL which had the large metal wings fitted first flew on 22 September and G EBJM completed as a single seater with a long range tank and the smaller metal wings followed on 4 September All took part in the trials which took place between 27 September and 4 October Uwins flying JK winning second prize in the main trials JL to be flown by T W Campbell was withdrawn because of aileron flutter and Campbell in JM won third place in the Grosvenor Cup race averaging over 70 mph Development editAfter the Lympne trials JK and JL were delivered to Martlesham Heath for evaluation as a primary trainer but did not impress the Air Ministry enough for any development to be funded by them G EBJK was returned to Filton for modifications in December 1925 It was fitted with the newly developed 36 hp Cherub III mounted slightly lower in the fuselage and the top longerons were curved down more to improve the view from the rear cockpit The fuel tank was enlarged and it was fitted with new metal wings giving it a span of 37 ft 7 in 11 45 m This was designated Type 91A After further trials at Martlesham it was again returned to Filton where the engine mounting was further lowered and a Fairey Reed duralmin propeller fitted Additionally a curved decking was added to the rear fuselage and it was fitted with an enlarged horn balanced rudder and a new undercarriage using rubber shock absorbers This was designated Type 91 B or Brownie II In this form the aircraft took place in the 1926 Lympne trials where Uwins won the third place prize of 500 Specifications Brownie I wooden wing edit nbsp Bristol Brownie 3 view drawing from NACA TM 289 Data from Bristol Aircraft Since 1910 1 General characteristicsCrew 1 Capacity 1 passenger Length 26 ft 3 in 8 00 m Wingspan 34 ft 7 in 10 54 m Height 6 ft 6 in 1 98 m Wing area 204 sq ft 19 0 m2 Empty weight 500 lb 227 kg Gross weight 870 lb 395 kg Powerplant 1 Bristol Cherub I 2 cylinder air cooled horizontally opposed piston engine 32 hp 24 kW Propellers 2 bladed fixed pitch propeller Performance Maximum speed 70 mph 110 km h 61 kn Range 100 mi 160 km 87 nmi See also editAircraft of comparable role configuration and era Most British manufacturers produced aircraft to take part in the Lympne trials and there are therefore a number of directly comparable aircraft including Avro Avis Beardmore Wee Bee De Havilland Humming Bird English Electric Wren Gloster Gannet Gnosspelius Gull Hawker Cygnet Parnall Pixie Supermarine Sparrow Vickers Vagabond Westland WoodpigeonReferences edit nbsp Wikimedia Commons has media related to Bristol Brownie Citations edit Barnes 1964 p 193 Bibliography edit Barnes C H 1964 Bristol Aircraft Since 1910 First ed London Putnam ISBN 0 85177 823 2 Taylor Michael J H 1989 Jane s Encyclopedia of Aviation London Studio Editions p 206 ISBN 9781851703241 Retrieved from https en wikipedia org w index php title Bristol Brownie amp oldid 1068081771, wikipedia, wiki, book, books, library,

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