26:
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The crankcase was made of aluminum and cast in separate upper and lower half parts, with the lower half having four mounting arms cast into it. Each cylinder pair was fixated to the crankcase by six bolts. The crankshaft was supported by two outer ball bearings and one intermediate plain bearing.
180:
on the left side of the engine. The intake valves were oriented to the center of each cylinder pair, and their intake ducts were conjoined within the casting into a single external port facing to the left side of the engine. The intake manifold was made of cast aluminum and a single
148:
The Argus 70 hp engine had a bore and stroke of 124 mm × 130 mm (4.9 in × 5.1 in) and was rated 70 hp (52 kW) at 1,250 rpm. The engine design evolved from the earlier
207:
In
October 1911 the engine has been evaluated in a French contest for aviation engines, where it produced on average 72.2 hp (53.8 kW) at 1,248 rpm. In 1912 the engine also competed the
168:
The engine cylinders were of cast iron, cast in pairs of two cylinders, with the cooling jackets integral in the casting. There were two overhead valves per cylinder, which were operated via
200:-magneto located at the control side of the engine, driven from the crankshaft via an intermediate spur gear. There was no oil pump installed and the lubrication was done solely by
825:
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204:. The coolant was circulated by a centrifugal water pump which was installed on the carburettor side and driven from the camshaft gear.
25:
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Airplane Engine
Encyclopedia: An Alphabetically Arranged Compilation Of All Available Data On The World's Airplane Engines
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The camshaft was driven from the crankshaft by spur gears at the control end. The engine had one or two
129:
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41:
594:"Concours de Moteurs d'aviation organisé au Laboratoire de l'A.C.F. par la Ligue Nationale Aérienne"
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aircraft engine contest, where it produced on average 72 hp (54 kW) at 1,342 rpm.
124:
and not As I) from 1911 was a four-cylinder, water cooled inline engine built by the German
821:
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113:
47:
518:(in German). II. Jahrgang 1913/14 (1). Berlin: Verlag für Fachliteratur G.m.b.H.: 24–36.
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engines with the same bore and stroke, with the main change being the use of
101:
33:
Argus (Aviatic-Rossel) 70 hp four-cylinder aircraft engine, intake side, 1911
500:
479:
813:
598:
Bulletin officiel de la
Commission technique de l'Automobile-club de France
523:
132:
and sold in France under the brand names 'Aviatik' and 'Aviatic-Rossel' by
512:"Der Wettbewerb um den Kaiserpreis für den besten deutschen Flugzeugmotor"
629:
177:
169:
162:
59:
182:
633:
495:(in German). Berlin: R. C. Schmidt & co. pp. 73, 188.
405:, 1911, pp. 18-20 (see also Krzyzan, Steinle; 1989, pp. 86-88)
161:. The engine can already be found in a 1911 brochure of the
128:
company. The engine also was license produced in France by
414:
Lumet, Ventou-Duclaux; 1911, p. 117, listed as 'Aviatic I'
829:
783:
670:
585:(1). Frankfurt am Main: Oskar Ursinus: 14–15. 1912.
828:. If you have a source, you can help Knowledge by
390:Angle, 1921, p. 49, listed as 'Type I with 70 hp'
253:four-cylinder, water-cooled in-line piston engine
592:Lumet, G.; Ventou-Duclaux, L. (October 1911).
645:
398:
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8:
575:"Die Flugmotore auf dem III. Pariser Salon"
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423:Laudahn, April 1913, p. 25, Engine no. 14a
824:article is missing some (or all) of its
553:Krzyzan, Marian; Steinle, Holger (1989).
600:(in French). 6e Année 1911 (63). Paris:
136:, the local sales representative of the
374:
15:
492:Motoren für Flugzeuge und Luftschiffe
7:
330:70 hp (52 kW) at 1,250 rpm
14:
280:6.28 L (383 cu in)
812:
24:
613:Friedrichshafen Aircraft of WW1
555:Die Jeannin-Stahltaube A.180/14
1:
849:1910s aircraft piston engines
470:. Otterbein Press. pp.
381:Flugsport 1/1912, pp. 14–15
870:
557:. Herford; Bonn: Mittler.
510:Laudahn, W. (April 1913).
464:Angle, Glenn Dale (1921).
196:per cylinder and a single
289:120 kg (265 lb)
271:130 mm (5.1 in)
262:124 mm (4.9 in)
32:
23:
18:
540:Automobil und Aviatik AG
441:Herris, 2016, p. 17
432:Herris, 2016, p. 15
363:List of aircraft engines
163:Automobil und Aviatik AG
138:Automobil und Aviatik AG
450:Huth, 1914, pp. 73, 188
245:General characteristics
183:Cudell-G.A.-carburettor
854:Argus aircraft engines
144:Design and development
611:Herris, Jack (2016).
489:Huth, Fritz (1914).
226:Friedrichshafen FF.8
221:Friedrichshafen FF.4
120:(in common with the
340:Related development
615:. Aeronaut Books.
130:Automobiles Rossel
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622:978-1-935881-35-3
542:. 1911. pp.
535:Aviatik-Flugzeuge
403:Aviatik-Flugzeuge
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126:Argus Motoren
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317:Water-cooled
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306:Cam-in-block
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276:Displacement
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215:Applications
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118:Argus Type I
117:
110:
108:
19:Argus 70 hp
830:adding them
346:Argus 50 hp
322:Performance
209:Kaiserpreis
194:spark plugs
174:rocker arms
159:side valves
157:instead of
151:Argus 50 hp
122:Argus 50 hp
90:Argus 50 hp
48:aero engine
843:Categories
705:140/150 hp
700:120/130 hp
369:References
351:Argus As I
301:Valvetrain
294:Components
285:Dry weight
102:Argus As I
76:First run
785:Pulse jet
579:Flugsport
480:23525261M
237:Data from
176:from the
501:11492610
335:See also
178:camshaft
170:pushrods
602:114–117
524:2449244
79:c.1911
60:Germany
798:As 044
793:As 014
775:As 413
770:As 412
765:As 411
760:As 410
755:As 402
750:As 401
720:As III
695:115 hp
690:110 hp
619:
561:
522:
499:
478:
267:Stroke
202:splash
116:, aka
45:inline
42:Piston
820:This
745:As 17
740:As 16
735:As 10
715:As II
685:70 hp
680:50 hp
661:Argus
544:18–20
251:Type:
198:Bosch
38:Type
730:As 8
725:As 5
710:As I
617:ISBN
559:ISBN
520:OCLC
497:OCLC
258:Bore
240:Huth
172:and
109:The
310:OHV
845::
596:.
583:IV
577:.
514:.
476:OL
474:.
472:49
395:^
308:,
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