Napier Dagger

Dagger
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 an outgrowth of the earlier Napier Rapier.

Design and development

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 there were problems with cooling, maintenance, manufacturing, and weight. These problems weren't solved during the Dagger's lifetime and went unresolved well into its successor the Napier Sabre's lifetime. 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 also found an application in the experimental Martin-Baker MB 2 fighter.

Variants

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

Dagger powered Hawker Hector

Note:

• Fairey Battle testbed only
• Handley Page Hereford
• Hawker Hart
• Hawker Hector
• Martin-Baker MB 2

Engines on display

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

Specifications (Napier Dagger III MS)

Data from Lumsden

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

• Valvetrain: One inlet and one exhaust valve per cylinder
• Supercharger: Single-speed centrifugal type supercharger, 5.04:1 reduction
• Fuel system: Napier-Claudel-Hobson carburettor
• Fuel type: 87 Octane petrol
• Cooling system: Air-cooled
• Reduction gear: Spur, 2.69:1

Performance

• Power output:
  
  • 725 hp (541 kW) at 3,500 rpm for takeoff
  • 794 hp (592 kW) at 4,000 rpm at 5,000 ft (1,520 m)
• Specific power: 0.77 hp/in³ (35.13 kW/l)
• Compression ratio: 7.75:1
• Specific fuel consumption: 0.43 lb/(hp•h) (261 g/(kW•h))
• Oil consumption: 0.18-0.35 oz/(hp•h) (7-13 g/(kW•h))
• Power-to-weight ratio: 0.62 hp/lb (1.02 kW/kg)

See also

Related development

• Napier Rapier
• Napier Sabre
  

Comparable engines

• Fairey Monarch
  

Related lists

• List of aircraft engines
  

References

Bibliography

• 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. http://www.flightglobal.com/pdfarchive/view/1938/1938%20-%203053.html?. 

External links

• Napier Dagger at oldengine.org