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HISTORIC AVIATION IN FOCUS – RADIAL ENGINES: A PERSONAL VIEW
Posted by Elliott Marsh | Jul 20, 2016 | Aviation History and Nostalgia, Feature, Vintage Aviation, Warbirds | 0 |
Richie Piper delves into the history of the radial engine and offers personal insight into the operation of radial engine vintage aeroplanes.
The Radial – I have to admit to having rather a passion for these smoke belching specialist aeronautical mechanical devices. The engine is always the heart of any aircraft but the radial seems even more than that, it defines the aircraft whether it be the profile to accommodate the frontal area, the invariable oil leaks (or marking its territory as we say!) or the way it starts in clouds of smoke and its distinctive sound.
T-28 Trojans © Darren Harbar Photography – www.darrenharbar.co.uk
A brief history
Through aviation history there have been two schools of thought on engine design, inline or circular, and there have been a whole raft of variations on these two themes. In the circular school, the rotary engine was the early standard where the crankshaft was bolted to the airframe and it was the engine that rotated, to which the propeller was fixed. This had many advantages including the engine itself acting as the flywheel, rather than having to add the mass of one, as well as the cooling effect of the engine spinning, even when on the ground. However, there were downsides including the gyroscopic effects on handling (Sopwith Camel trainee pilots were not allowed to turn right unless above 1,000 feet initially) and a limitation on the ultimate power of these designs. The Bentley BR2 (as used in the Sopwith Snipe) perhaps represents the pinnacle of rotary development, peaking at 245 bhp.
The inline engine favoured over 100 years ago by the Wright brothers, who designed and built their own, often had to be water-cooled because sufficient airflow could not be easily routed around the cylinders for that purpose. The horizontally opposed engines from the 1940s and ’50s managed to do away with the necessity of water cooling but as designers and operators know, baffle and cowling design is a bit of a black art to get front and rear cylinder temperatures even.
Detail on a radial engine © Huw Hopkins – Global Aviation Resource
Three aircraft, five radials – Staggerwing leads Beech 18 and C-47 Skytrain © Karl Drage – Global Aviation Resource
The Avro 504 was originally powered by a rotary engine but this modern day replica houses a radial power plant © Huw Hopkins – Global Aviation Resource
The successor to the rotary was the radial, where the engine is fixed and the propeller is driven by the crankshaft through the wonderful contrivance of the master rod and main journal, with each of the other slave con rods contributing to the whole endeavour. It is worth having a look at the animations that demonstrate this intriguing choreography of a seemingly illogical design. This in an instant resolved the handling issues and also removed the power limitations. There were other benefits such as the oil no longer being slung into the airstream and hence back onto the pilot. The lubricant, often being castor oil, was prone to cause digestive complications for the air crew! As most rotary engines tended to utilise a total loss lubrication system, oil consumption and hence flight limitations were also improved.
Although oil consumption was greatly improved over the rotary, usage and therefore the need for replenishment was a factor in some scenarios. The Skyraider’s patrol and loiter profiles, for example, meant that a very large oil tank of 36 gallons was required for its missions of up to ten hours and it was oil rather than fuel which could be the limiting factor. The piston airliners of the 1950s had flight engineers to not only manage the engines, frequently adjusting mixtures, but also to monitor oil usage and pump oil from a reserve tank to the appropriate engine.
The 1930s Westland Lysander © Darren Harbar Photography – http://www.darrenharbar.co.uk/
The design rules of the four-stroke cycle dictate that a radial engine must have an odd number of cylinders. Louis Bleriot made use of all 24hp of the three cylinder Anzani to cross the Channel in 1909, an example of which at the Shuttleworth Collection is thought to be the oldest airworthy aero engine in the world. Engines like the Warner Scarab and Kinner, popular in the boom in personal aircraft before World War Two, have five cylinders and produce up to 160 bhp whilst the seven cylinder Continentals and Lycomings often seen in Stearman produce around 220 bhp, giving rise to the aircraft’s curvature of the earth departure climb!
The ubiquitous Pratt and Witney Wasp produces up to 600 bhp from its nine pots and was my first introduction to radials in the Harvard. The ultimate nine cylinder radial is the Wright Cyclone (producing 1425 bhp) that had great success in the Flying Fortress and many crews owe their lives to the ability of this engine to sustain damage but keep running for hours. It was also eventually used in the T-28 trainer to good effect. This was conceived as a replacement trainer for the Harvard but equipped with a “low powered” radial of 800hp to give pilots experience of the slow response of the jet they were moving onto.
North American Harvard © Huw Hopkins – Global Aviation Resource
Posted by Elliott Marsh | Jul 20, 2016 | Aviation History and Nostalgia, Feature, Vintage Aviation, Warbirds | 0 |
Richie Piper delves into the history of the radial engine and offers personal insight into the operation of radial engine vintage aeroplanes.
The Radial – I have to admit to having rather a passion for these smoke belching specialist aeronautical mechanical devices. The engine is always the heart of any aircraft but the radial seems even more than that, it defines the aircraft whether it be the profile to accommodate the frontal area, the invariable oil leaks (or marking its territory as we say!) or the way it starts in clouds of smoke and its distinctive sound.
T-28 Trojans © Darren Harbar Photography – www.darrenharbar.co.uk
A brief history
Through aviation history there have been two schools of thought on engine design, inline or circular, and there have been a whole raft of variations on these two themes. In the circular school, the rotary engine was the early standard where the crankshaft was bolted to the airframe and it was the engine that rotated, to which the propeller was fixed. This had many advantages including the engine itself acting as the flywheel, rather than having to add the mass of one, as well as the cooling effect of the engine spinning, even when on the ground. However, there were downsides including the gyroscopic effects on handling (Sopwith Camel trainee pilots were not allowed to turn right unless above 1,000 feet initially) and a limitation on the ultimate power of these designs. The Bentley BR2 (as used in the Sopwith Snipe) perhaps represents the pinnacle of rotary development, peaking at 245 bhp.
The inline engine favoured over 100 years ago by the Wright brothers, who designed and built their own, often had to be water-cooled because sufficient airflow could not be easily routed around the cylinders for that purpose. The horizontally opposed engines from the 1940s and ’50s managed to do away with the necessity of water cooling but as designers and operators know, baffle and cowling design is a bit of a black art to get front and rear cylinder temperatures even.
Detail on a radial engine © Huw Hopkins – Global Aviation Resource
Three aircraft, five radials – Staggerwing leads Beech 18 and C-47 Skytrain © Karl Drage – Global Aviation Resource
The Avro 504 was originally powered by a rotary engine but this modern day replica houses a radial power plant © Huw Hopkins – Global Aviation Resource
The successor to the rotary was the radial, where the engine is fixed and the propeller is driven by the crankshaft through the wonderful contrivance of the master rod and main journal, with each of the other slave con rods contributing to the whole endeavour. It is worth having a look at the animations that demonstrate this intriguing choreography of a seemingly illogical design. This in an instant resolved the handling issues and also removed the power limitations. There were other benefits such as the oil no longer being slung into the airstream and hence back onto the pilot. The lubricant, often being castor oil, was prone to cause digestive complications for the air crew! As most rotary engines tended to utilise a total loss lubrication system, oil consumption and hence flight limitations were also improved.
Although oil consumption was greatly improved over the rotary, usage and therefore the need for replenishment was a factor in some scenarios. The Skyraider’s patrol and loiter profiles, for example, meant that a very large oil tank of 36 gallons was required for its missions of up to ten hours and it was oil rather than fuel which could be the limiting factor. The piston airliners of the 1950s had flight engineers to not only manage the engines, frequently adjusting mixtures, but also to monitor oil usage and pump oil from a reserve tank to the appropriate engine.
The 1930s Westland Lysander © Darren Harbar Photography – http://www.darrenharbar.co.uk/
The design rules of the four-stroke cycle dictate that a radial engine must have an odd number of cylinders. Louis Bleriot made use of all 24hp of the three cylinder Anzani to cross the Channel in 1909, an example of which at the Shuttleworth Collection is thought to be the oldest airworthy aero engine in the world. Engines like the Warner Scarab and Kinner, popular in the boom in personal aircraft before World War Two, have five cylinders and produce up to 160 bhp whilst the seven cylinder Continentals and Lycomings often seen in Stearman produce around 220 bhp, giving rise to the aircraft’s curvature of the earth departure climb!
The ubiquitous Pratt and Witney Wasp produces up to 600 bhp from its nine pots and was my first introduction to radials in the Harvard. The ultimate nine cylinder radial is the Wright Cyclone (producing 1425 bhp) that had great success in the Flying Fortress and many crews owe their lives to the ability of this engine to sustain damage but keep running for hours. It was also eventually used in the T-28 trainer to good effect. This was conceived as a replacement trainer for the Harvard but equipped with a “low powered” radial of 800hp to give pilots experience of the slow response of the jet they were moving onto.
North American Harvard © Huw Hopkins – Global Aviation Resource