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Armstrong Siddeley Panther Aero-Engines

Panther

By 1929, the Jaguar engine was underpowered compared to the competition. To address this situation, the engine's bore was increased to 5.25 inches, which raised the displacement to 27.3 litres. The prototype was known as the Jaguar Major, whilst all production units were named as Panthers.

 

The Panther variants were available as geared or ungeared units, with aspiration options including a plain fan, a geared fan that provided a mild supercharging effect, and a full supercharger.

HE132 Panther IV.jpg
Panther Mk IV 
Armstrong Siddeley Panther.jpg
Panther Mk X
Armstrong Siddeley  Panther XIA Aero Engine.jpg
Panther Mk XIA 
Some examples of Panther powered aircraft are shown below.
armstrong-whitworth Starling.jpg

AW Starling Panther IIA

Avro_627 Mailplane credit Tim mason.jpg
Avro_627 Panther IIA     Credit Tim Mason
Hawket Fury Panther IIIA Noewegian Air Force.jpg

Hawker Fury Panther IIIA

Supamarine Air Yacht 3 Panther IIA.jpg
Supermarine Air Yacht Panther IIA engines
AWXVI Powered by Armstrong Siddeley Panther III.jpg
AW XVI  Panther III
Fairey Gordon Panther IIA Credit IWM
Fairey Gordon powered by Armstrong Siddeley Panther IIA.jpg

Leading Particulars of Panther Engines

 

Engine Type    14-cylinder, two-row air-cooled, radial aero-engine

Bore                  5.25 inch     (133.4mm)                 
Stroke               5.50 inch     (139.7mm)
Volume             1666 cu. in. (27.3 litre)

Tractor Drive    Geared Epicyclic

Variants

Jaguar Major Mk I, 1929 prototype of the Panther engine

 

MK II

     1929 605hp (445kW), Plain Fan, Compression ratio 5:1

Mk IIA

     1930 605hp (445kW), Geared Fan, Compression ratio 5:1

Mk III

     1931 560hp (412kW), Supercharged, Compression ratio 5:1

Mk IIIA

     1931 502hp (369kW), Supercharged, Compression ratio 5:1

Mk VI

     1930 560hp (212kW), Geared Fan, Compression ratio 5.2:1

Mk VIA

     1932 560hp (412kW), Geared Fan, Compression ratio 5.2:1

Mk VII

     1934 565hp (416kW), Supercharged.Compression ratio 5.1:1

Mk IXA

     1934 580hp  (427kW), Geared Fan.Compression ratio 6.35:1

Mk X

     1934 700hp  (515kW), Geared Fan.Compression ratio 6.35:1

Mk XI

     1936 600hp  (441kW), Geared Fan.Compression ratio 6.35:1

Note: The plain fan had no supercharging effect; the geared fan gave a mild supercharging effect.

armstrong-whitworth scimitar credit Redit jpeg.jpg
AW Scimitar Panther VII  Credit Redit
Wapiti P613 with Armstrong Sidderley Panther engine. credir SAAF.jpg
Westland Wapiti Panther II       Credit SAAF
AW Atlas powered by Armstrong Siddeley Panther IIA.jpg
AW Atlas Panther IIA
Panther IV.jpg
Panther IV
 Panther IV
Armstrong Siddeley Panther IV.jpg
Panther IV reduced.jpg
Panther IV
Farey Seal IIIF Powered by  Panther Panther Mk IIA with peruvian Air Corps.jpg
Peruvian Air Corps Farey Seal Panther IIA
Balckburn Ripon IIF with Panther engine.jpg
Finish Air Force Blackburn Ripon Panther IIA

Power Curve for a Panther IIA

Power curve rated at 3000ft from A. & A.A.E Martlesham, Report M617 dated 24.1.1933. Boost rated -.625 lb/sq. in. 

RPM             2,300         2,200        2,100        2,000        1,900      1,800

BHP                605            579           554           529           501         469

BOOST          zero                          -.625 lb


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