An obturator ring was a type of piston ring used in World War I aero engines for improved sealing in the presence of cylinder distortion.

Purpose

The cylinders of rotary aircraft engines (engines with the crankshaft fixed to the airframe and rotating cylinders) suffered from uneven cylinder cooling as the side facing the direction of rotation received more cooling air which lead to thermal distortion. To keep weight down the cylinders on rotary engines had very thin-walls (1.5 mm)[1] and some had no cylinder liners. On engine types without cylinder liners, obturator rings, made of bronze in the early Gnome engines,[2] were fitted as these were soft enough to not damage cylinder walls and could flex to the shape of the cylinder. Wear on the rings was considerable. Engines needed to be overhauled about every 20 hours.[3] The reliability of Gnome engines license-built by The British Gnome and Le Rhone Engine Co. gave an overhaul life of about 80 hours mainly as a result using a special tool to roll the 'L' section obturator rings.[4]

Le Rhône and Bentley BR1/BR2 rotary engines used cylinder liners and were sealed using conventional piston rings rather than obturator rings.[5]

An 'L' section obturator ring is shown in Patent US 1378109A - "Obturator ring".[6]

See also

References

  1. ↑ The Rotary Aero Engine, Andrew Nahum 1987, ISBN 1 900747 12 X, p.40
  2. ↑ Aviation Engine Examiner, Major Victor W. Page, The Norman W. Henley Publishing Co., 2 West 45th Street, New York 1931, p.146
  3. ↑ The Rotary Aero Engine, Andrew Nahum 1987, ISBN 1 900747 12 X, p.40
  4. ↑ I Kept No Diary, Air Commodore F.R. Banks 1978, ISBN 0 9504543 9 7, p.63
  5. ↑ The Rotary Aero Engine, Andrew Nahum 1987, ISBN 1 900747 12 X, p.27
  6. ↑ https://patentimages.storage.googleapis.com/31/ba/4e/d0d1dff885aaff/US1378109.pdf


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