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Bristol Titan

The Bristol Titan was a British five-cylinder air-cooled radial engine, designed and built by the Bristol Aeroplane Company in the late 1920s. It had the same size cylinders as the earlier Bristol Mercury engine, 5.75 in × 6.5 in (146 mm × 165 mm) (displacing 844 cu in (13.83 L)), and produced between 200–240 hp (150–180 kW). Later versions of the Bristol Titan also used a Farman-style reduction gear produced by Gnome-Rhône.

Titan
The Bristol Titan
Type Piston aero engine
Manufacturer Bristol Aeroplane Company
Designer Roy Fedden
First run c.1928
Major applications Avro 504N
Bristol Primary Trainer

Design and development

The engine was designed as a five-cylinder radial, to use as many parts of the Bristol Jupiter as possible. Cylinders, pistons, articulated connecting rods, crankshaft and other minor parts were interchangeable with the Jupiter.[1]

The major significance of the Titan was that it was licensed to Gnome-Rhône and became the pattern for the Gnome-Rhône 5B and 5K. In 1927 Gnome-Rhône was looking for ways out of its licence agreement with Bristol for the Jupiter engine of 1920 and began to produce the Gnome-Rhône 5B and 5K without royalties.

Gnome-Rhône was not satisfied with simply producing Bristol designs under licence, and started a major design effort based around the mechanics of the Titan engine. The results were introduced in 1927 as the K-series, spanning the 260 hp (190 kW) Gnome-Rhône 5K Titan, the seven-cylinder 370 hp (280 kW) Gnome-Rhône 7K Titan Major, and the nine-cylinder 550 hp (410 kW) Gnome-Rhône 9K Mistral. With the introduction of the K-series, Gnome-Rhône finally ended royalty payments to Bristol, the Gnome-Rhône 5K being built in much greater numbers than the original Bristol Titan. By 1930 they had delivered 6,000 Jupiters, Mistrals and Titans, making them the largest engine company in France.

Variants

Titan I
(1928) - 205 hp (153 kW)
Titan IIF
Modified valve gear.
Titan II (Special)
Titan IV
(1928) - 205 hp (153 kW), 0.5:1 reduction gear from Bristol Jupiter.
Gnome et Rhône 5B
Gnome et Rhône 5Ba
Gnome et Rhône 5Bc
Gnome et Rhône 5K Titan
licence-built Titan II, 230 hp (170 kW)
Gnome et Rhône 7K Titan Major
enlarged seven-cylinder Titan with many detail improvements, produced by Gnome-Rhône without licence.

Applications

Specifications (Titan I)

Data from Lumsden.[2]

General characteristics

Components

  • Valvetrain: Overhead valve, 4 valves per cylinder
  • Cooling system: Air-cooled
  • Reduction gear: None, direct drive, left hand tractor

Performance

See also

Related development

Comparable engines

Related lists

References

Notes

  1. ^ Flight International 5 July 1928
  2. ^ Lumsden 2003, p.102.

Bibliography

  • Lumsden, Alec. British Piston Engines and their Aircraft. Marlborough, Wiltshire: Airlife Publishing, 2003. ISBN 1-85310-294-6.

bristol, titan, this, article, needs, additional, citations, verification, please, help, improve, this, article, adding, citations, reliable, sources, unsourced, material, challenged, removed, find, sources, news, newspapers, books, scholar, jstor, april, 2018. This article needs additional citations for verification Please help improve this article by adding citations to reliable sources Unsourced material may be challenged and removed Find sources Bristol Titan news newspapers books scholar JSTOR April 2018 Learn how and when to remove this template message The Bristol Titan was a British five cylinder air cooled radial engine designed and built by the Bristol Aeroplane Company in the late 1920s It had the same size cylinders as the earlier Bristol Mercury engine 5 75 in 6 5 in 146 mm 165 mm displacing 844 cu in 13 83 L and produced between 200 240 hp 150 180 kW Later versions of the Bristol Titan also used a Farman style reduction gear produced by Gnome Rhone TitanThe Bristol TitanType Piston aero engineManufacturer Bristol Aeroplane CompanyDesigner Roy FeddenFirst run c 1928Major applications Avro 504NBristol Primary Trainer Contents 1 Design and development 2 Variants 3 Applications 4 Specifications Titan I 4 1 General characteristics 4 2 Components 4 3 Performance 5 See also 6 References 6 1 Notes 6 2 BibliographyDesign and development EditThe engine was designed as a five cylinder radial to use as many parts of the Bristol Jupiter as possible Cylinders pistons articulated connecting rods crankshaft and other minor parts were interchangeable with the Jupiter 1 The major significance of the Titan was that it was licensed to Gnome Rhone and became the pattern for the Gnome Rhone 5B and 5K In 1927 Gnome Rhone was looking for ways out of its licence agreement with Bristol for the Jupiter engine of 1920 and began to produce the Gnome Rhone 5B and 5K without royalties Gnome Rhone was not satisfied with simply producing Bristol designs under licence and started a major design effort based around the mechanics of the Titan engine The results were introduced in 1927 as the K series spanning the 260 hp 190 kW Gnome Rhone 5K Titan the seven cylinder 370 hp 280 kW Gnome Rhone 7K Titan Major and the nine cylinder 550 hp 410 kW Gnome Rhone 9K Mistral With the introduction of the K series Gnome Rhone finally ended royalty payments to Bristol the Gnome Rhone 5K being built in much greater numbers than the original Bristol Titan By 1930 they had delivered 6 000 Jupiters Mistrals and Titans making them the largest engine company in France Variants EditTitan I 1928 205 hp 153 kW Titan IIF Modified valve gear Titan II Special Titan IV 1928 205 hp 153 kW 0 5 1 reduction gear from Bristol Jupiter Gnome et Rhone 5B Gnome et Rhone 5Ba Gnome et Rhone 5Bc Gnome et Rhone 5K Titan licence built Titan II 230 hp 170 kW Gnome et Rhone 7K Titan Major enlarged seven cylinder Titan with many detail improvements produced by Gnome Rhone without licence Applications EditAvro 504N Bristol Primary Trainer Bristol Type 110ASpecifications Titan I EditData from Lumsden 2 General characteristics Type five cylinder air cooled radial engine Bore 5 75 in 146 mm Stroke 6 5 in 165 mm Displacement 844 in 13 8 L Diameter 48 4 in 1229 3 mm Dry weight 500 lb 227 kg Components Valvetrain Overhead valve 4 valves per cylinder Cooling system Air cooled Reduction gear None direct drive left hand tractorPerformance Power output 210 hp 157 kW at 1 800 rpm Specific power 0 25 hp in 11 4 kW L Compression ratio 5 1 Power to weight ratio 0 42 hp lb 0 7 kW kg See also EditRelated development Bristol Mercury Bristol NeptuneComparable engines Armstrong Siddeley MongooseRelated lists List of aircraft enginesReferences EditNotes Edit Flight International 5 July 1928 Lumsden 2003 p 102 Bibliography Edit Lumsden Alec British Piston Engines and their Aircraft Marlborough Wiltshire Airlife Publishing 2003 ISBN 1 85310 294 6 Retrieved from https en wikipedia org w index php title Bristol Titan amp oldid 1125790012, wikipedia, wiki, book, books, library,

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