Napier Dagger

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Dagger
NapierDagger.JPG
Napier Dagger at the Royal Air Force Museum, London
Type Piston aero-engine
Manufacturer Napier & Son
First run 1934
Major applications Handley Page Hereford
Hawker Hector

The Napier Dagger was a 24-cylinder H-pattern (or H-Block) air-cooled engine designed by Frank Halford and built by Napier before WWII. It was a development of the earlier Napier Rapier.[1]

Design and development[edit]

The H-Block has a compact layout, as it essentially consists of two vertically opposed inline engines lying side-by-side and driving side-by-side crankshafts. Another advantage is that since the cylinders are opposed, the motion in one is balanced by the opposite motion in the one on the opposite side, leading to very smooth running. The Dagger was remarkable for its fast rotation, running at up to 4,000 rpm but unlike the later Napier Sabre, it had conventional poppet valves.

Although considered a masterpiece of engine design by Frank Halford, there were problems with cooling, maintenance, manufacturing and weight, which were not solved during the Dagger's lifetime and went unresolved well into it the lifetime of the Napier Sabre, it's successor. The Dagger powered the Hawker Hector army co-operation aircraft and the Handley Page Hereford, a variant of the Hampden bomber. The operational usefulness of the Hector was restricted by engine cooling problems, which made it unsuitable for operations in the tropics and the Hereford was found to be unsuitable for combat, because its Dagger VIII engines were noisy and unreliable. The Dagger was also used in the experimental Martin-Baker MB 2 fighter.

Variants[edit]

Napier-Halford Dagger I

1934 - 650 hp.

Dagger II

1938 - 755 hp

Dagger IIIM

1938 - 725 hp

Dagger VIII

1938 - 955 hp, intermediate altitude supercharger, initially known as E.108

Applications[edit]

Dagger powered Hawker Hector

Note:[2]

Engines on display[edit]

A preserved Napier Dagger is on display at the Royal Air Force Museum London.

Specifications (Napier Dagger III MS)[edit]

Data from Lumsden[3]

General characteristics

  • Type: Twenty-four-cylinder supercharged air-cooled H engine
  • Bore: 3.813 in (96.8 mm)
  • Stroke: 3.75 in (95.25 mm)
  • Displacement: 1,027 in³ (16.8 L)
  • Length: 80 in (2,032 mm)
  • Width: 22.5 in (584 mm)
  • Height: 45.125 in (1,146 mm)
  • Dry weight: 1,358 lb (616 kg)

Components

Performance

See also[edit]

Related development
Comparable engines
Related lists

References[edit]

Notes[edit]

  1. ^ Gunston 1989, p.105.
  2. ^ Some of these aircraft were test beds only.
  3. ^ Lumsden 2003, p.174.

Bibliography[edit]

  • Gunston, Bill. World Encyclopedia of Aero Engines. Cambridge, England. Patrick Stephens Limited, 1989. ISBN 1-85260-163-9
  • Lumsden, Alec. British Piston Engines and their Aircraft. Marlborough, Wiltshire: Airlife Publishing, 2003. ISBN 1-85310-294-6.
  • "Britain's aero engines". archive at flightglobal.com. 3 November 1938. 

External links[edit]