Rolls-Royce Eagle
The Rolls-Royce Eagle was the first aircraft engine to be developed by Rolls-Royce Limited. Introduced in 1915 to meet British military requirements during World War I, it was used to power the Handley Page Type O bombers and a number of other military aircraft.
The Eagle was the first engine to make a non-stop trans-Atlantic crossing by aeroplane when two Eagles powered the converted Vickers Vimy bomber on the transatlantic flight of Alcock and Brown in June 1919.
Background
At the outbreak of World War I in August 1914, the Royal Aircraft Factory asked Rolls-Royce to develop a new air-cooled engine. Despite initial reluctance, they agreed, on condition that it be cooled by water rather than by air, which was the company's area of expertise.Design and development
Development of the new 20 litre engine was led by Henry Royce from his home in Kent. Based initially on the 7.4 litre 40/50 Rolls-Royce Silver Ghost engine, and drawing also on the design of a 7.2 litre Daimler DF80 aero engine used in a 1913 Grand Prix Mercedes that had been acquired, the power was increased by doubling the number of cylinders to twelve and increasing their stroke to, although their bore remained at of the 40/50. The engine was also run faster, and an epicyclic reduction gear was designed to keep the propeller speed below 1,100 rpm. To reduce inertia and improve performance the valvetrain design was changed from sidevalves to a SOHC design, closely following the original "side-slot" rocker arm design philosophy used on the contemporary German Mercedes D.I, Mercedes D.II and Mercedes D.III straight-six aviation powerplants.The engineering department of the Royal Naval Air Service played a key role in the success of the engine by directing the car designer W.O. Bentley, who had enlisted in the Royal Navy, to place his expertise in the design of aluminium pistons at the service of Rolls-Royce. This gave significant weight saving to the Eagle and contributed to its excellent performance.
On 3 January 1915 the Admiralty ordered twenty-five of the new engines. The Eagle first ran on a test bed at Rolls-Royce's Derby works in February 1915, producing at 1,600 rpm. This was quickly increased to 1,800, then in August 1915 to 2,000 rpm where it produced. After further testing, it was decided to approve the engine for production at 1,800 rpm and ; 1,900 rpm was allowed for short periods. The engine first flew on a Handley Page O/100 bomber in December 1915, the first flight of a Rolls-Royce aero engine.
The Eagle was developed further during 1916 and 1917, with power being progressively increased from to, followed by, and then, and finally by February 1918 by which time eight Eagle variants had been produced. Throughout World War I Rolls-Royce struggled to build Eagles in the quantities required by the War Office, but the company resisted pressure to license other manufacturers to produce it. The fears of Rolls-Royce that the engine's much admired quality would be compromised by other manufacturers is often given as an explanation for this resistance, but the commercial terms sought by Rolls-Royce for licence production were so restrictive that other manufacturers - apart from Brazil Straker - refused to accept them. When the Ministry of Munitions took over coordination of aircraft production in 1917, Sir William Weir declined to intervene in the company's commercial strategy, even though success of the engine owed much to the technology transfer directed by the RNAS. He preferred to support untested engines using cast aluminium components like the Siddeley Puma and the Sunbeam Arab, believing them to be better suited to mass production, in comparison to the intricate machining required to build the Eagle and its smaller cousin the Falcon.
After the War, a Mark IX version of the Eagle was developed for civilian use. Production continued until 1928, and in total 4,681 Eagle engines were built.
Time between overhaul for later Eagles was around 100–180 hours.
Variants
Note:;Eagle I
;Eagle II
;Eagle III
;Eagle IV
;Eagle V
;Eagle VI
;Eagle VII
;Eagle VIII
;Eagle IX
Applications
- Admiralty N.S.3 North Sea Airship
- Admiralty 23 Class Airship
- Airco DH.4
- Airco DH.9
- Airco DH.10 Amiens
- Airco DH.16
- ANEC III
- BAT F.K.26
- Blackburn Blackburd
- Curtiss H.12 Large America
- Curtiss-Wanamaker Triplane
- Dornier Do E
- Dornier Wal
- Fairey III
- Fairey Campania
- Felixstowe F.2
- Felixstowe F.3
- Felixstowe F.4
- Felixstowe F.5
- Fokker F.VII
- Grahame-White G.W.E.7
- Handasyde H.2
- Handley Page Type O
- Handley Page V/1500
- Handley Page Type W
- Hawker Horsley
- Porte Baby
- Porte Super Baby
- Martinsyde F.1
- Rohrbach Ro II
- Rohrbach Ro III
- Royal Aircraft Factory F.E.2
- Royal Aircraft Factory F.E.4
- Royal Aircraft Factory R.E.7
- Short Bomber
- Short N.1B Shirl
- Short Type 184
- Sopwith Atlantic
- Sopwith Wallaby
- Sopwith Tractor Triplane
- Supermarine Commercial Amphibian
- Supermarine Scarab
- Supermarine Sea Eagle
- Supermarine Swan
- Van Berkel W-B
- Vickers F.B.11
- Vickers Valparaiso
- Vickers Vernon
- Vickers Viking
- Vickers Vulcan
- Vickers Vulture
- Vickers Vimy
- Wight Converted Seaplane
Engines on display
Examples of the Rolls-Royce Eagle are on display at the:- Polish Aviation Museum, Kraków
- Science Museum, London
- Canada Aviation Museum
- South African National Museum of Military History, Johannesburg
- South African Air Force Museum, Port Elizabeth
An airworthy Fokker C.IV is powered by a Rolls-Royce Eagle VIII at the Owls Head Transportation Museum, Maine.