Inflexible
Role Experimental Transport
Manufacturer Beardmore
Designer Dr Rohrbach[1]/W.S Shackleton
First flight 5 March 1928
Introduction 1928
Retired 1930
Status Retired
Primary user Royal Air Force
Number built 1

The Beardmore Inflexible, also known as the Rohrbach Ro VI, was a three-engined all-metal prototype transport aircraft built by William Beardmore and Company at Dalmuir, Scotland.

Design and development

Beardmore Inflexible photo published in Flight magazine, April 1928

William Beardmore and Company had acquired a licence for the use of the Rohrbach principle for stressed-skin construction. Using these principles and drawings supplied by Rohrbach for the RoVI, the Beardmore company built a massive all-metal three-engined transport, the Beardmore Inflexible.

The aircraft was built in sections at Dalmuir between 1925 and 1927 which were shipped by sea to Felixstowe and from there delivered by road to the Aeroplane & Armament Experimental Establishment (A&AEE) at Martlesham Heath Airfield where it first flew on 5 March 1928.[2] It appeared at the Hendon RAF Display later in the year. The aircraft was structurally advanced for its time and had good flying qualities. It was also a very large aircraft for the time, having a wingspan of 157 ft (48 m) - around 16 ft (4.9 m) greater than the Boeing B-29 Superfortress heavy bomber of World War II. However, with an all up weight of 37,000 lb (17,000 kg) it was underpowered and, with no interest forthcoming from the RAF for a production contract, the aircraft was dismantled at Martlesham Heath in 1930. It was then examined for the effects of corrosion on light-alloy stressed skin structures.

One of the aircraft's wheels survives, and is on exhibit in the Science Museum, London.

Operators

 United Kingdom

Specifications

Data from Air Enthusiast International [2]

General characteristics

  • Length: 75 ft 6 in (23.01 m)
  • Wingspan: 157 ft 6 in (48.01 m)
  • Height: 21 ft 2 in (6.45 m)
  • Wing area: 1,967 sq ft (182.7 m2)
  • Empty weight: 24,301 lb (11,023 kg)
  • Max takeoff weight: 37,000 lb (16,783 kg)
  • Powerplant: 3 × Rolls-Royce Condor II V12 piston engine, 650 hp (480 kW) each

Performance

  • Maximum speed: 109 mph (175 km/h, 95 kn)
  • Service ceiling: 9,350 ft (2,850 m) [3]
  • Rate of climb: 436 ft/min (2.21 m/s) at 2,000 ft (610 m)[3]

See also

Related development

Aircraft of comparable role, configuration, and era

Related lists

References

Notes

  1. ↑ Flight 5 July 1928 p539 "although the design staff at Dalmuir, headed by Mr. W. S. Shackleton...naturally did a large amount of the detail work."
  2. 1 2 Air Enthusiast International March 1974, p.145.
  3. 1 2 Jarrett Aeroplane Monthly March 1990, p. 142

Bibliography

  • "The Beardmore Inflexible". Flight. 5 April 1928. pp. 225–226. Archived from the original on 21 October 2012.{{cite magazine}}: CS1 maint: unfit URL (link)
  • The Illustrated Encyclopedia of Aircraft (Part Work 1982-1985). Orbis Publishing.
  • Jackson, A. J. (1973). British Civil Aircraft since 1919. Vol. 1. London: Putnam. ISBN 978-0370100067.
  • Jarrett, Philip (March 1990). "Beardmore's heavy metal monsters – Part 2". Aeroplane Monthly. Vol. 18, no. 3. pp. 136–142. ISSN 0143-7240.
  • "Plane Facts". Air Enthusiast International. Vol. 6, no. 3. Bromley, UK: Fine Scroll. March 1974. p. 145.
  • Taylor, Michael J. H. (1989). Jane's Encyclopedia of Aviation. London: Studio Editions. p. 123. ISBN 978-0517103166.
Wikimedia Commons has media related to Beardmore Inflexible.
  • Film clip of the Inflexible taxiing and taking off at the Norwich Air Display, May 1929; Pathé News online archive.
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