Lloyd C.II

Lloyd C.II–C.IV
Lloyd C.II
Role Reconnaissance aircraft
National origin Austria-Hungary
Manufacturer Ungarische Lloyd Flugzeug und Motorenfabrik AG / Magyar Lloyd Repülőgép és motorgyár Részvény-Társaság
First flight 1915
Primary user KuKLFT
Number built 100 × C.II
ca. 50 × C.III
ca. 40 × C.IV

The Lloyd C.II and its derivatives, the C.III and C.IV were reconnaissance aircraft produced in Austria-Hungary during the First World War.[1] They were based on the Lloyd company's pre-war C.I design, and like it, were conventional biplanes with swept-back wings.

Design and development

After the outbreak of World War I, the original aircraft was refined somewhat by Lloyd designers Wizina and von Melczer,[2] featuring a reduced wingspan and wing area but increased weight.[3] An 8 mm Schwarzlose machine gun was added on a semi-circular mount for an observer.[4]

Beginning in 1915, one hundred examples of this type were built – fifty by Lloyd at their plant in Aszód, and another fifty by WKF in Vienna.

Apart from their service with the Austro-Hungarian flying service, ten C.IIs saw service with Poland. These were captured in Malopolska in November 1918 and were used as trainers until being withdrawn from service in 1920.

A C.III shot down in Romania

The C.III was almost identical except for the use of a 120 kW (160 hp) Austro-Daimler engine, which increased the top speed to 133 km/h (83 mph).[3] Production again was by both Lloyd and WKF, with total production amounting to 50-60 machines.

The C.IV also used the Austro-Daimler engine, and small batches were produced by both Lloyd and WKF.[3]

Variants

  • C.II with Heiro engine and 14.00 m wingspan (100 built)
  • C.III with Austro-Daimler engine and 14.00 m wingspan (8 or 16 built by Lloyd, 43 by WKF)
  • C.IV with Austro-Daimler engine produced by Lloyd with 14.52 m (47 ft 8 in) wingspan (47 built, plus one converted)

Operators

 Austria-Hungary

Specifications (C.II)

Data from Grosz 2002, German & Austro-Hungarian Aircraft Manufacturers 1908 - 1918[5]

General characteristics

  • Crew: 2
  • Length: 8.8 m (28 ft 10 in)
  • Upper wingspan: 14.8 m (48 ft 7 in)
  • Lower wingspan: 13.8 m (45 ft 3 in)
  • Height: 3.15 m (10 ft 4 in)
  • Wing area: 38.0 m2 (409 sq ft)
  • Empty weight: 900 kg (1,984 lb)
  • Gross weight: 1,329 kg (2,930 lb)
  • Powerplant: 1 × Hiero (Mar) 6-cyl. water-cooled in-line piston engine, 108 kW (145 hp)

Performance

  • Maximum speed: 128 km/h (80 mph, 69 kn)
  • Range: 400 km (250 mi, 220 nmi)
  • Service ceiling: 3,000 m (9,800 ft)
  • Rate of climb: 5.6 m/s (1,100 ft/min)

Armament
One 8 mm (0.315 in) Schwarzlose machine gun in the observers position, mounted on a rail.

  • 90 kg (198 lb) of bombs

Notes

  1. ^ Taylor 1989, 581
  2. ^ Gunston 2003, 184
  3. ^ a b c Grosz 2002
  4. ^ Murphy 2005, 108
  5. ^ Treadwell, Terry C. (2010). German & Austro-Hungarian Aircraft Manufacturers 1908 - 1918. Stroud: Amberley Publishing. pp. 268–271. ISBN 978-1-4456-0102-1.

References

  • Grosz, Peter M. (2002). Austro-Hungarian Army Aircraft of World War One. Colorado: Flying Machine Press.
  • Gunston, Bill (1993). World Encyclopedia of Aircraft Manufacturers. Annapolis: Naval Institute Press.
  • Murphy, Justin D. (2005). Military Aircraft: Origins to 1918. Santa Barbara: ABC-Clio.
  • Taylor, Michael J. H. (1989). Jane's Encyclopedia of Aviation. London: Studio Editions.
  • Treadwell, Terry C. (2010). German & Austro-Hungarian Aircraft Manufacturers 1908 - 1918. Stroud: Amberley Publishing. pp. 268–271. ISBN 978-1-4456-0102-1.
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