165:, a giant triplane bomber was designed to use the Tiger but redesigned to use other engines when it became clear the Tiger would not be available soon enough. The only aircraft in which the Siddeley Tiger flew was the ill-fated prototype of the twin-engined
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with the advanced feature of an electric starter motor protected by a friction clutch. A reduction gear arrangement was provided for the propeller drive with a
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of which three were planned to be produced. Major problems with both the engines and this experimental bomber aircraft led to cancellation of the projects.
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of 0.559:1. The company claimed a power output of 600 hp (447 kW) but this was regarded as optimistic. Flight testing by a
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143:'The engines could never be persuaded to run simultaneously for any length of time'
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111:. Problems encountered during flight testing caused the project to be cancelled.
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The
Siddeley Tiger marked the end of the aero engine line started by
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Contemporary technical description of the engine with photographs.
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420:. Cambridge, England. Patrick Stephens Limited, 1989.
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and
Siddeley-Deasy. The name was later re-used for an
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Developed using two modified cylinder banks from the
434:. Marlborough, Wiltshire: Airlife Publishing, 2003.
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150:Lumsden – British Aero-Engines and Their Aircraft
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209:12-cylinder liquid-cooled inline piston engine
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8:
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123:, the Tiger was a liquid-cooled 60-degree
432:British Piston Engines and their Aircraft
455:"The Siddeley Aero Engines: The "Tiger""
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7:
467:(14): 431–433. 3 April 1919. No. 536
16:1920s British piston aircraft engine
748:Armstrong Siddeley aircraft engines
103:developed shortly after the end of
418:World Encyclopedia of Aero Engines
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36:
19:For the 1932 radial engine, see
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753:1920s aircraft piston engines
157:Application and cancellation
133:Royal Aircraft Establishment
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18:
44:
35:
30:
365:List of aircraft engines
21:Armstrong Siddeley Tiger
282:, 4 valves per cylinder
201:General characteristics
325:0.42 hp/lb (0.7 kW/kg)
187:Specifications (Tiger)
154:
115:Design and development
321:Power-to-weight ratio
167:Siddeley-Deasy Siniai
758:V12 aircraft engines
96:was an unsuccessful
402:Lumsden 2003, p.87.
388:Gunston 1989, p.18.
335:Related development
254:39.57 in (1,005 mm)
242:81.34 in (2,066 mm)
148:Frank T.Courtenay,
45:The Siddeley Tiger
512:Armstrong Siddeley
353:Rolls-Royce Condor
347:Comparable engines
236:2,657 in³ (43.5 L)
178:Armstrong Siddeley
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280:Overhead camshaft
263:1,400 lb (635 kg)
248:33.46 in (850 mm)
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430:Lumsden, Alec.
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316:600 hp (447 kW)
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301:Cooling system:
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227:7.1 in (180 mm)
218:6.3 in (160 mm)
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137:Frank Courtenay
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68:United Kingdom
64:National origin
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109:Siddeley-Deasy
94:Siddeley Tiger
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359:Related lists
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341:Siddeley Puma
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314:Power output:
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303:Liquid-cooled
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181:radial engine
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163:Tarrant Tabor
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121:Siddeley Puma
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73:Manufacturer
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57:inline engine
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681:Double Mamba
618:
574:Jaguar Major
515:aero engines
469:. Retrieved
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417:
410:Bibliography
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358:
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334:
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319:
313:
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294:
290:carburettors
286:Fuel system:
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232:Displacement
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135:test pilot,
118:
93:
91:
25:
619:Tiger (V12)
559:Genet Major
308:Performance
105:World War I
101:aero engine
742:Categories
669:Turboprops
589:Lynx Major
471:12 January
371:References
295:Fuel type:
275:Valvetrain
268:Components
259:Dry weight
125:V12 engine
83:First run
638:Turbojets
629:Wolfhound
549:Deerhound
529:Boarhound
192:Data from
174:Beardmore
717:Screamer
655:Sapphire
594:Mongoose
330:See also
146:—
722:Stentor
712:Snarler
604:Panther
579:Leopard
534:Cheetah
252:Height:
240:Length:
195:Lumsden
98:British
691:Python
614:Serval
569:Jaguar
544:Cougar
460:Flight
438:
424:
297:Petrol
246:Width:
223:Stroke
31:Tiger
727:Gamma
686:Mamba
660:Viper
645:Adder
599:Ounce
564:Hyena
554:Genet
539:Civet
376:Notes
288:Twin
207:Type:
129:ratio
86:1920
50:Type
707:Beta
609:Puma
584:Lynx
473:2011
436:ISBN
422:ISBN
214:Bore
161:The
92:The
676:ASP
650:ASX
107:by
54:V12
744::
465:XI
463:.
457:.
393:^
183:.
504:e
497:t
490:v
475:.
442:.
323::
277::
261::
234::
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216::
197:.
23:.
Text is available under the Creative Commons Attribution-ShareAlike License. Additional terms may apply.
