26:
123:
engine, the cylinders were cast separately from iron and then machined. They were grouped together to a single block, joined at their cooling jackets by means of flanges and bolts. The conjoined cylinder block incorporated a single intake duct running through the water jackets, fed by a single
140:
on the left side of the engine, with the camshaft being driven from the crankshaft by spur gears at the control end. The magneto also was located at the control end of the engine to the right, driven from the crankshaft via an intermediate spur gear.
144:
The crankshaft was supported by three intermediate and two outer plain bearings, with two additional thrust ball bearings at the propeller end. Lubrication was pressure fed, with an oil pump feeding oil to the crankshaft bearings.
116:. It had a bore and stroke of 140 mm × 150 mm (5.51 in × 5.91 in) and was rated at 80 / 100 hp (60 / 75 kW) with a normal speed of 1,200 rpm.
148:
In 1912 the engine was also produced as a six-cylinder with the same cylinder dimensions, rated at 100 / 130 hp (75 / 97 kW).
484:
166:(1912), 100–130 hp (75–97 kW), 160 kg (353 lb), 140 mm × 150 mm (5.5 in × 5.9 in) bore and stroke
160:(1911), 80–100 hp (60–75 kW), 130 kg (287 lb), 140 mm × 150 mm (5.5 in × 5.9 in) bore and stroke
548:
553:
477:
279:
394:
Airplane Engine
Encyclopedia: An Alphabetically Arranged Compilation Of All Available Data On The World's Airplane Engines
346:
Illustrirte
Mittheilungen des Oberrheinischen Vereins für Luftschiffahrt, issue 16/1911, p. 38, advertisement
470:
324:
44:
128:
which was installed at the control end. There were two overhead valves per cylinder, which were operated via
398:
255:
25:
504:
41:
232:
109:
212:
517:
512:
451:
425:
312:
120:
496:
402:
203:
89:
47:
424:(in German). I. Jahrgang 1912/13 (2). Berlin: Verlag für Fachliteratur G.m.b.H.: 96–101.
392:
444:
Illustrirte
Mittheilungen des Oberrheinischen Vereins für Luftschiffahrt, Jahrgang 1911
542:
194:
251:
439:
417:
462:
493:
125:
113:
93:
69:
267:
245:
221:
133:
92:
from 1911 was a four-cylinder, water cooled inline engine built by the German
455:
406:
429:
137:
129:
263:
59:
259:
466:
440:"Gustav Otto Flugmaschinen-Werke München (advertisement)"
503:
190:four-cylinder, water-cooled in-line piston engine
33:Aeromotor Gustav Otto 80/100 hp aircraft engine
373:
371:
369:
367:
365:
363:
361:
478:
8:
485:
471:
463:
342:
340:
163:Otto A.G.O. 100/130 hp six-cylinder
157:Otto A.G.O. 80/100 hp four-cylinder
108:) 80/100 hp engine was designed by
336:
171:Specifications (Otto A.G.O. 80/100 hp)
15:
7:
14:
217:9.24 L (564 cu in)
418:"Die Flugmotorern auf der "ALA""
24:
297:80–100 hp (60–75 kW)
114:Gustav Otto Flugmaschinenwerke
94:Gustav Otto Flugmaschinenwerke
70:Gustav Otto Flugmaschinenwerke
1:
549:1910s aircraft piston engines
416:Quittner, Victor (May 1912).
397:. Otterbein Press. pp.
570:
450:(16): 38. August 9, 1911.
391:Angle, Glenn Dale (1921).
377:Quittner, 1912, pp. 96-101
258:per cylinder actuated via
208:150 mm (5.91 in)
199:140 mm (5.51 in)
87:Otto A.G.O. 80/100 hp
254:in the engine block, two
226:130 kg (287 lb)
32:
23:
18:
325:List of aircraft engines
355:Angle 1921, pp. 372-373
182:General characteristics
100:Design and development
19:Otto A.G.O. 80/100 hp
554:Otto aircraft engines
106:Aeromotor Gustav Otto
119:As with the smaller
307:Related development
536:
535:
313:Otto A.G.O. 50 hp
121:Otto A.G.O. 50 hp
104:The Otto A.G.O. (
83:
82:
561:
497:aircraft engines
487:
480:
473:
464:
459:
433:
410:
378:
375:
356:
353:
347:
344:
56:
28:
16:
569:
568:
564:
563:
562:
560:
559:
558:
539:
538:
537:
532:
499:
491:
438:
415:
390:
387:
382:
381:
376:
359:
354:
350:
345:
338:
333:
304:
291:
273:Cooling system:
256:overhead valves
241:
184:
173:
154:
112:in 1911 at the
102:
90:aircraft engine
55:National origin
54:
12:
11:
5:
567:
565:
557:
556:
551:
541:
540:
534:
533:
531:
530:
525:
520:
515:
509:
507:
505:Piston engines
501:
500:
492:
490:
489:
482:
475:
467:
461:
460:
435:
434:
412:
411:
386:
383:
380:
379:
357:
348:
335:
334:
332:
329:
328:
327:
316:
315:
303:
300:
299:
298:
290:
287:
286:
285:
280:Reduction gear
276:
270:
260:roller tappets
240:
237:
236:
235:
233:Hans Geisenhof
227:
218:
209:
200:
191:
183:
180:
172:
169:
168:
167:
164:
161:
158:
153:
150:
110:Hans Geisenhof
101:
98:
81:
80:
77:
73:
72:
67:
63:
62:
57:
51:
50:
39:
35:
34:
30:
29:
21:
20:
13:
10:
9:
6:
4:
3:
2:
566:
555:
552:
550:
547:
546:
544:
529:
526:
524:
521:
519:
516:
514:
511:
510:
508:
506:
502:
498:
495:
494:Otto (A.G.O.)
488:
483:
481:
476:
474:
469:
468:
465:
457:
453:
449:
446:(in German).
445:
441:
437:
436:
431:
427:
423:
419:
414:
413:
408:
404:
400:
396:
395:
389:
388:
384:
374:
372:
370:
368:
366:
364:
362:
358:
352:
349:
343:
341:
337:
330:
326:
323:
322:
321:
320:
319:Related lists
314:
311:
310:
309:
308:
301:
296:
295:Power output:
293:
292:
288:
283:
281:
277:
274:
271:
269:
265:
261:
257:
253:
249:
247:
243:
242:
238:
234:
231:
228:
225:
223:
219:
216:
214:
210:
207:
205:
201:
198:
196:
192:
189:
186:
185:
181:
179:
177:
170:
165:
162:
159:
156:
155:
151:
149:
146:
142:
139:
135:
131:
127:
122:
117:
115:
111:
107:
99:
97:
95:
91:
88:
78:
75:
74:
71:
68:
66:Manufacturer
65:
64:
61:
58:
53:
52:
49:
46:
43:
40:
37:
36:
31:
27:
22:
17:
527:
522:
447:
443:
422:Der Oelmotor
421:
393:
385:Bibliography
351:
318:
317:
306:
305:
294:
284:Direct-drive
278:
275:Water-cooled
272:
244:
229:
220:
213:Displacement
211:
202:
193:
187:
175:
174:
147:
143:
118:
105:
103:
86:
84:
289:Performance
268:rocker arms
134:rocker arms
126:carburettor
48:aero engine
543:Categories
528:100/130 hp
331:References
246:Valvetrain
239:Components
222:Dry weight
76:First run
523:80/100 hp
407:23525261M
230:Designer:
176:Data from
136:from the
456:19872940
302:See also
264:pushrods
252:camshaft
178:Quittner
152:Variants
138:camshaft
130:pushrods
430:2449244
399:372-373
79:c.1911
60:Germany
454:
428:
405:
204:Stroke
45:inline
42:Piston
518:70 hp
513:50 hp
188:Type:
38:Type
452:OCLC
426:OCLC
266:and
250:one
195:Bore
132:and
85:The
545::
448:15
442:.
420:.
403:OL
401:.
360:^
339:^
262:,
96:.
486:e
479:t
472:v
458:.
432:.
409:.
282::
248::
224::
215::
206::
197::
Text is available under the Creative Commons Attribution-ShareAlike License. Additional terms may apply.
