29:
766:
173:-magneto, which was driven from the camshaft spur gear. Lubrication was done by an oil pump mounted on the control end, directly driven by the camshaft. The oil was recirculated from the oil sump and sprayed onto the connecting rod ends, from where it was distributed further. Also, a centrifugal water pump was mounted directly to the crankshaft at the control end.
164:
The crankcase was made of aluminum and cast in separate upper and lower half parts, with the upper half having four mounting arms cast into it. Each cylinder pair was fixated to the crankcase by ten bolts. The crankshaft was supported by two outer ball bearings and one intermediate plain bearing.
156:
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
180:
contest for aviation engines, where it was rated down to the maximum allowed 115 hp (86 kW) by throttling it to 1,100 rpm. The engine suffered a piston fracture caused by a torn off valve disk. Since the replacement engine was not available, and the engine according to
168:
The camshaft was driven from the crankshaft by spur gears at the control end, with generally all gears on the control end having been encapsulated. The engine had two spark plugs per cylinder and a single
144:
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
777:
134:
It had a bore and stroke of 155 mm × 165 mm (6.1 in × 6.5 in) and was rated 140–150 hp (100–110 kW) at 1,250–1,300 rpm.
603:
553:
800:
137:
The general design of the engine was carried over from the preceding four-cylinder Argus engines, such as the 100 hp (75 kW)
572:
28:
177:
805:
596:
431:
Airplane Engine
Encyclopedia: An Alphabetically Arranged Compilation Of All Available Data On The World's Airplane Engines
589:
549:
332:
47:
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623:
44:
232:
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721:
706:
691:
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529:
506:
483:
460:
170:
736:
656:
651:
505:(in German). I. Jahrgang 1912/13 (12). Berlin: Verlag für Fachliteratur G.m.b.H.: 519–530.
773:
615:
439:
223:
104:
50:
528:(in German). II. Jahrgang 1913/14 (1). Berlin: Verlag für Fachliteratur G.m.b.H.: 24–36.
429:
482:(in German). I. Jahrgang 1912/13 (1). Berlin: Verlag für Fachliteratur G.m.b.H.: 39–47.
794:
612:
214:
182:
112:
72:
744:
716:
711:
671:
646:
641:
280:
521:
498:
475:
454:
111:(not As IV), was a four-cylinder, water cooled inline engine built by the German
701:
696:
686:
666:
636:
631:
681:
676:
661:
320:
275:
259:
149:
138:
92:
185:
was at disadvantage due to its power, it was retracted from the competition.
464:
443:
765:
533:
510:
487:
522:"Der Wettbewerb um den Kaiserpreis für den besten deutschen Flugzeugmotor"
499:"Der Wettbewerb um den Kaiserpreis für den besten deutschen Flugzeugmotor"
581:
153:
145:
124:
123:
The Argus 140/150 hp first can be found in a 1911 brochure of the
62:
158:
585:
459:(in German). Berlin: R. C. Schmidt & co. pp. 73, 188.
354:, 1911, pp. 18-20 (see also Krzyzan, Steinle; 1989, pp. 86-88)
36:
Argus 140/150 hp four-cylinder aircraft engine, intake side
781:
127:. In April 1912 it was also presented at the "ALA" (
735:
622:
176:In 1912, the engine has also been submitted to the
780:. If you have a source, you can help Knowledge by
210:four-cylinder, water-cooled in-line piston engine
374:
372:
370:
368:
366:
364:
362:
360:
597:
8:
760:
604:
590:
582:
396:Laudahn, March 1913, p.528, Engine No. 14c
387:Angle, 1921, p. 50-51, listed as 'Type IV'
776:article is missing some (or all) of its
563:Krzyzan, Marian; Steinle, Holger (1989).
344:
305:140 hp (100 kW) at 1,250 rpm
18:
456:Motoren für Flugzeuge und Luftschiffe
7:
129:Allgemeine Luftfahrzeug-Ausstellung
16:1910s German piston aircraft engine
237:12.45 L (760 cu in)
14:
764:
476:"Die Flugmotorern auf der "ALA""
27:
565:Die Jeannin-Stahltaube A.180/14
474:Quittner, Victor (April 1912).
405:Laudahn, April 1913, pp. 24–36
1:
801:1910s aircraft piston engines
434:. Otterbein Press. pp.
822:
567:. Herford; Bonn: Mittler.
520:Laudahn, W. (April 1913).
497:Laudahn, W. (March 1913).
428:Angle, Glenn Dale (1921).
255:726 mm (28.6 in)
249:495 mm (19.5 in)
243:1,220 mm (48 in)
264:190 kg (419 lb)
228:165 mm (6.5 in)
219:155 mm (6.1 in)
107:from 1911, also known as
35:
26:
21:
550:Automobil und Aviatik AG
333:List of aircraft engines
131:) exhibition in Berlin.
125:Automobil und Aviatik AG
414:Huth, 1914, pp. 73, 188
202:General characteristics
159:Cudell-G.A.-carburettor
806:Argus aircraft engines
119:Design and development
378:Quittner, 1912, p. 41
102:Argus 140/150 hp
453:Huth, Fritz (1914).
315:Related development
789:
788:
758:
757:
552:. 1911. pp.
545:Aviatik-Flugzeuge
352:Aviatik-Flugzeuge
98:
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22:Argus 140/150 hp
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327:Related lists
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303:Power output:
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113:Argus Motoren
110:
109:Argus Type IV
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73:Argus Motoren
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69:Manufacturer
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526:Der Oelmotor
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503:Der Oelmotor
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480:Der Oelmotor
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422:Bibliography
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292:Water-cooled
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281:Cam-in-block
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233:Displacement
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108:
101:
99:
782:adding them
297:Performance
178:Kaiserpreis
150:rocker arms
51:aero engine
795:Categories
657:140/150 hp
652:120/130 hp
339:References
321:Argus As I
276:Valvetrain
269:Components
260:Dry weight
139:Argus As I
93:Argus As I
79:First run
737:Pulse jet
444:23525261M
194:Data from
152:from the
115:company.
465:11492610
310:See also
154:camshaft
146:pushrods
534:2449244
511:2449244
488:2449244
253:Height:
241:Length:
82:c.1911
63:Germany
750:As 044
745:As 014
727:As 413
722:As 412
717:As 411
712:As 410
707:As 402
702:As 401
672:As III
647:115 hp
642:110 hp
571:
532:
509:
486:
463:
442:
247:Width:
224:Stroke
48:inline
45:Piston
772:This
697:As 17
692:As 16
687:As 10
667:As II
637:70 hp
632:50 hp
613:Argus
554:18–20
436:50-51
208:Type:
171:Bosch
41:Type
682:As 8
677:As 5
662:As I
569:ISBN
530:OCLC
507:OCLC
484:OCLC
461:OCLC
215:Bore
197:Huth
148:and
100:The
285:OHV
797::
524:.
501:.
478:.
440:OL
438:.
359:^
283:,
141:.
784:.
605:e
598:t
591:v
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513:.
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217::
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