Clerget aircraft engines

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Template:Short description

File:Clerget 9B.jpg
Preserved Clerget 9B rotary engine on display at the Pima Air & Space Museum

Clerget is the name given to aircraft engines designed by the French engineer Pierre Clerget(fr) in the first half of the 20th century. From 1912, Clerget focused his efforts on developing a series of rotary aircraft engines, which were widely used in French and British aircraft during World War I. More than 30,000 Clerget rotary engines were manufactured in France by Clerget-Blin and in Great Britain by Gwynnes Limited they were used on such aircraft as the Sopwith Camel and Vickers Gunbus.

In the 1920s Pierre Clerget turned his attention to diesel radial engines and finally produced a H-16 engine before he died in 1943.

Early Clerget engines

The first Clerget aero engine to enter series production was the 50 hp model of 1910. The engine was a water cooled inline-4 with aluminum pistons which produced Template:Convert (Template:Convert when hot) for a weight of Template:Convert. The engine was used on several pioneering aircraft including the Coandă-1910 and the first Etrich Taube. Clerget also designed a second larger inline-4 producing Template:Convert. Both these engines were manufactured by Clément-Bayard.[1]Template:Rp

In October 1910, at the Paris Air Show, Clément-Bayard showcased the powerful 200 hp Clerget water cooled V8 aero engine.[1]Template:Rp The engine weighed Template:Convert which gave a power to weight ratio of only Template:Cvt,[2] considered remarkable for its time period.[3] The engine featured a form of variable valve timing, utilising a camshaft that could be adjusted axially to engage different cam profiles. This allowed the opening period of the intake and exhaust valves to be optimised during flight.[1]Template:Rp[2] In 1912, a single 200 hp Clerget engine was fitted to the giant Voisin Icare Aero-Yacht.[1]Template:Rp

Early Clerget engine types

File:200 hp Clerget.jpg
200 hp Clerget aircraft engine displayed at the London Science Museum
50 hp Clerget
(1910) Template:Convert, inline 4
100 hp Clerget
(1910) Template:Convert, inline 4
200 hp Clerget
(1910) Template:Convert, V8

Early Clerget engines on display

Rotary engine development (spark ignition)

File:Clerget 9 engine, cylinder head and valve rockers.jpg
Cylinder head of a Clerget 9J, showing the two valve rockers and the induction pipe from the rear of the engine

From 1912, Pierre Clerget devoted himself to the design of rotary engines. Clerget's designs were successful, initially with the sports aircraft market and then with military customers. More than 30,000 Clerget rotary engine were built during World War I.[1]Template:Rp

What distinguished the Clerget rotary engine from its rivals (Gnome and Le Rhône) was that the Clerget had normal intake and exhaust valves unlike the Gnome, and the connecting rod arrangement was much simpler than the Le Rhone. A source of failure among the Clerget engines were the special-purpose piston rings, called obturator rings. These were located below the gudgeon or wrist pin, to block heat transfer from the combustion area to the lower part of the cylinder and overcome their subsequent distortion. These rings were often made from brass and only had a lifespan of a few hours. The Clerget engines were considered reliable but they cost more per unit to produce than their rivals. Unlike other contemporary rotaries in which the ignition system was either switched on or off to provide a rudimentary form of engine speed control, the Clerget featured a throttle.

The Bentley BR1 and Bentley BR2 rotaries were designed as improvements of the Clerget, while sharing some of the earlier engine's distinctive design features.

Design features

The Clerget rotary engines were air-cooled with either seven, nine or eleven cylinders. They were fitted with a double thrust ball race, which enabled them to be used either as a pusher or as a tractor engine.

The engines worked on a four-stroke cycle. The chief points of difference from other rotary engines were:

  • The connecting rods had a tubular section.
  • The inlet and exhaust valves were mechanically operated by means of separate cams, tappets and rocker arms.

The direction of rotation was counter (anti)-clockwise as seen from the propeller-end of the engine. Like many other rotary engines of the period they were made chiefly of steel, for strength and lightness.

Rotary engine types

Clerget 7Y
(1912) Template:Cvt, seven-cylinder.
Clerget 7Z
(1913) Template:Cvt, seven-cylinder.
Clerget 9A
(1913) Template:Cvt, nine-cylinder derivative of 7Z. (designation reused for radial)
Clerget 9B
(1915) Template:Cvt, nine-cylinder. (designation reused for radial)
Clerget 9Bf
(1915) Template:Cvt, nine-cylinder long stroke version of the Clerget 9B. The most numerous British production engine with 2,350 units being built.
Clerget 9J
(1917) Template:Cvt, nine-cylinder. Redesigned with aluminium pistons, tubular connecting rods and revised valve gear.
Clerget 9Z
(1915) Template:Cvt, nine-cylinder.
Clerget 11Eb
(1918) Template:Cvt, 11-cylinder, single-row engine.

Rotary engines on display

Operational rotary engines

The Shuttleworth Collection based at Old Warden Aerodrome in the UK, operate an airworthy late production Sopwith Triplane (G-BOCK)[6] fitted with an original 9B as well as an airworthy late production Sopwith Camel (G-BZSC)[7] fitted with an original long-stroke 9Bf. These aircraft can be seen displaying at home air displays through the summer months.

Radial 'X' engines

Clerget 16X

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A 420 hp (310 kW) 16-cylinder, four-row X engine.

Diesel radial engines

File:Clerget 14 F.jpg
A Clerget 14F diesel aircraft engine preserved at the Conservatoire de l'Air et de l'Espace d’Aquitaine

In the 1920s Pierre Clerget designed static diesel radial engines, the earliest were based on his rotary designs.

Clerget 9A
(1929) 100 hp (75 kW) nine-cylinder, single row radial engine.[8]
Clerget 9B
Clerget 9C
Produced under licence by Hispano-Suiza as the Hispano-Suiza 9T
Clerget 14F-01
(1937) 14-cylinder, two-row radial engine, flown in a Potez 25 biplane.
Clerget 14F-02
Clerget 14Fcs

16H engine

Clerget's final engine design was a V-16 designated Clerget 16H and known as the Type Transatlantique. It developed 2,000 hp (1,500 kW) through the use of four Rateau turbochargers.

See also

References

Template:Reflist

  • "Air Board" Technical Notes issued by Controller Technical Department for persons holding an official position in His Majesty's Service dated 1918
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External links

Template:Sister project

Template:Clerget aeroengines

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  6. The Shuttleworth Collection - Sopwith Triplane Retrieved: 21 August 2018
  7. The Shuttleworth Collection - Sopwith Camel Retrieved: 21 August 2018
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