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Curtiss-Reid Rambler

The Reid Rambler, later known under the Curtiss-Reid brand after Reid was purchased by Curtiss, was a biplane trainer/sport aircraft built in Canada in the early 1930s and used in small numbers as a trainer aircraft by the Royal Canadian Air Force.

Rambler
Role Sportsplane
Manufacturer Reid, Curtiss-Reid
Designer Wilfrid T. Reid
First flight 22 September 1928
Primary user Royal Canadian Air Force
Number built 45[1]

Design and development edit

In 1928, Wilfrid Thomas Reid set up his own company in Montreal after working as an engineer for Canadian Vickers. His first design was a light aircraft that was intended to exploit a Canadian government programme to support the development of flying clubs. The Reid Rambler was primarily intended to be a training aircraft. The Rambler was a largely conventional sesquiplane design with wings braced with Warren trusses and which could be folded backwards for transport or storage. The fuselage was of fabric-covered steel tube construction and the pilot and a single passenger sat in tandem, open cockpits.[2]

The prototype (registration G-CAVO) was first flown at the Cartierville Airport on 23 September 1928 by Martin Berlyn. The test flight was nearly a disaster because the ailerons seized, leaving Berlyn with a dangerous approach and landing. A modification of the aileron control linkage rectified the problem. The Rambler continued to be developed, and in 1931, an improved version, the Rambler III, was flown with the more powerful Gipsy III engine. John C. Webster flew the MK III prototype in the British King's Cup Race that year.[2]

Operational history edit

In December 1928, the Curtiss Aeroplane & Motor Company purchased the Reid Aircraft Company and renamed it The Curtiss-Reid Aircraft Company. The new firm assumed control of the existing Rambler project and established a production line. A number of alterations were made to the production series including replacing the original ailerons with Frise-style ailerons, introducing an unbalanced rudder along with changes to the engine cowling, exhaust system and tailskid, and adding a head rest.[2]

Although it was intended principally for civilian use, the Royal Canadian Air Force (RCAF) evaluated the aircraft as a basic training aircraft. Although the RCAF employed many other ab-initio aircraft including the ubiquitous de Havilland Moth, senior military staff elected to purchase a small number of the Ramblers.[2]

Curtiss-Reid Ramblers enjoyed a relatively productive and lengthy career both in civilian and military use lasting well into the Second World War era.[2]

Variants edit

Data from:Canadian aircraft since 1909[2]

Rambler Mk.I
Powered by an 83–100 hp (62–75 kW) de Havilland Gipsy I
Rambler Mk.II
Powered by a 105–115 hp (78–86 kW) Cirrus Hermes II
Rambler Mk.III
Powered by a 120 hp (89 kW) de Havilland Gipsy III

Specifications (Rambler Mk.I) edit

Data from Jane's all the World's Aircraft 1931,[3] Canadian aircraft since 1909[2]

General characteristics

  • Crew: 2
  • Length: 22 ft 6 in (6.86 m) *Length folded: 22 ft 6 in (6.86 m)
  • Upper wingspan: 33 ft (10 m)
  • Lower wingspan: 22 ft 5 in (6.83 m)
  • Width: 11 ft 1 in (3.38 m)
  • Height: 8 ft (2.4 m)
  • Wing area: 238 sq ft (22.1 m2)
  • Empty weight: 1,000 lb (454 kg)
  • Gross weight: 1,650 lb (748 kg)
  • Fuel capacity: 20 imp gal (24 US gal; 91 L)
  • Powerplant: 1 × de Havilland Gipsy I 4-cylinder up-right in-line air-cooled piston engine, 90 hp (67 kW)
  • Propellers: 2-bladed fixed-pitch metal propeller

Performance

  • Maximum speed: 102 mph (164 km/h, 89 kn) at sea level
97 mph (84 kn; 156 km/h) at 5,000 ft (1,500 m)
  • Cruise speed: 90 mph (140 km/h, 78 kn)
  • Stall speed: 38 mph (61 km/h, 33 kn)
  • Range: 315 mi (507 km, 274 nmi) cruising range
  • Endurance: 3.5 hours
  • Service ceiling: 12,000 ft (3,700 m) ; 14,000 ft (4,300 m) Absolute ceiling
  • Rate of climb: 750 ft/min (3.8 m/s)
  • Wing loading: 6.075 lb/sq ft (29.66 kg/m2)
  • Power/mass: 16.5 lb/hp (10.0 kg/kW)

References edit

  1. ^ Molson, Kenneth M.; Taylor, H.A. (1982). Canadian aircraft since 1909. Stittsville, Ontario: Canada's Wings. p. 473. ISBN 0-920002-11-0.
  2. ^ a b c d e f g Molson, Kenneth M.; Taylor, H.A. (1982). Canadian aircraft since 1909. Stittsville, Ontario: Canada's Wings. pp. 236–242. ISBN 0-920002-11-0.
  3. ^ Grey, C.G., ed. (1931). Jane's all the World's Aircraft 1931. London: Sampson Low, Marston & company, ltd. pp. 84c–85c.

Further reading edit

  • Taylor, Michael J.H. (1989). Jane's Encyclopaedia of Aviation. London: Studio Editions. p. 288. ISBN 978-0-517-69186-1.

External links edit

  • . Archived from the original on 15 August 2011. Retrieved 29 December 2018.
  • rcaf.com Curtiss-Reid Rambler
  • Canadian Aviation Heritage Centre - Curtiss-Reid Rambler
  • Flightglobal Archive - Curtiss-Reid Rambler

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The Reid Rambler later known under the Curtiss Reid brand after Reid was purchased by Curtiss was a biplane trainer sport aircraft built in Canada in the early 1930s and used in small numbers as a trainer aircraft by the Royal Canadian Air Force RamblerRole SportsplaneManufacturer Reid Curtiss ReidDesigner Wilfrid T ReidFirst flight 22 September 1928Primary user Royal Canadian Air ForceNumber built 45 1 Contents 1 Design and development 2 Operational history 3 Variants 4 Specifications Rambler Mk I 5 References 6 Further reading 7 External linksDesign and development editIn 1928 Wilfrid Thomas Reid set up his own company in Montreal after working as an engineer for Canadian Vickers His first design was a light aircraft that was intended to exploit a Canadian government programme to support the development of flying clubs The Reid Rambler was primarily intended to be a training aircraft The Rambler was a largely conventional sesquiplane design with wings braced with Warren trusses and which could be folded backwards for transport or storage The fuselage was of fabric covered steel tube construction and the pilot and a single passenger sat in tandem open cockpits 2 The prototype registration G CAVO was first flown at the Cartierville Airport on 23 September 1928 by Martin Berlyn The test flight was nearly a disaster because the ailerons seized leaving Berlyn with a dangerous approach and landing A modification of the aileron control linkage rectified the problem The Rambler continued to be developed and in 1931 an improved version the Rambler III was flown with the more powerful Gipsy III engine John C Webster flew the MK III prototype in the British King s Cup Race that year 2 Operational history editIn December 1928 the Curtiss Aeroplane amp Motor Company purchased the Reid Aircraft Company and renamed it The Curtiss Reid Aircraft Company The new firm assumed control of the existing Rambler project and established a production line A number of alterations were made to the production series including replacing the original ailerons with Frise style ailerons introducing an unbalanced rudder along with changes to the engine cowling exhaust system and tailskid and adding a head rest 2 Although it was intended principally for civilian use the Royal Canadian Air Force RCAF evaluated the aircraft as a basic training aircraft Although the RCAF employed many other ab initio aircraft including the ubiquitous de Havilland Moth senior military staff elected to purchase a small number of the Ramblers 2 Curtiss Reid Ramblers enjoyed a relatively productive and lengthy career both in civilian and military use lasting well into the Second World War era 2 Variants editData from Canadian aircraft since 1909 2 Rambler Mk I Powered by an 83 100 hp 62 75 kW de Havilland Gipsy I Rambler Mk II Powered by a 105 115 hp 78 86 kW Cirrus Hermes II Rambler Mk III Powered by a 120 hp 89 kW de Havilland Gipsy IIISpecifications Rambler Mk I editData from Jane s all the World s Aircraft 1931 3 Canadian aircraft since 1909 2 General characteristicsCrew 2 Length 22 ft 6 in 6 86 m Length folded 22 ft 6 in 6 86 m Upper wingspan 33 ft 10 m Lower wingspan 22 ft 5 in 6 83 m Width 11 ft 1 in 3 38 m Height 8 ft 2 4 m Wing area 238 sq ft 22 1 m2 Empty weight 1 000 lb 454 kg Gross weight 1 650 lb 748 kg Fuel capacity 20 imp gal 24 US gal 91 L Powerplant 1 de Havilland Gipsy I 4 cylinder up right in line air cooled piston engine 90 hp 67 kW Propellers 2 bladed fixed pitch metal propellerPerformance Maximum speed 102 mph 164 km h 89 kn at sea level97 mph 84 kn 156 km h at 5 000 ft 1 500 m dd dd dd dd dd Cruise speed 90 mph 140 km h 78 kn Stall speed 38 mph 61 km h 33 kn Range 315 mi 507 km 274 nmi cruising range Endurance 3 5 hours Service ceiling 12 000 ft 3 700 m 14 000 ft 4 300 m Absolute ceiling Rate of climb 750 ft min 3 8 m s Wing loading 6 075 lb sq ft 29 66 kg m2 Power mass 16 5 lb hp 10 0 kg kW References edit Molson Kenneth M Taylor H A 1982 Canadian aircraft since 1909 Stittsville Ontario Canada s Wings p 473 ISBN 0 920002 11 0 a b c d e f g Molson Kenneth M Taylor H A 1982 Canadian aircraft since 1909 Stittsville Ontario Canada s Wings pp 236 242 ISBN 0 920002 11 0 Grey C G ed 1931 Jane s all the World s Aircraft 1931 London Sampson Low Marston amp company ltd pp 84c 85c Further reading editTaylor Michael J H 1989 Jane s Encyclopaedia of Aviation London Studio Editions p 288 ISBN 978 0 517 69186 1 External links edit nbsp Wikimedia Commons has media related to Curtiss Reid Rambler CurtissReidRambler Archived from the original on 15 August 2011 Retrieved 29 December 2018 rcaf com Curtiss Reid Rambler Canadian Aviation Heritage Centre Curtiss Reid Rambler Flightglobal Archive Curtiss Reid Rambler Retrieved from https en wikipedia org w index php title Curtiss Reid Rambler amp oldid 1212049848, wikipedia, wiki, book, books, library,

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