29:
150:
combustion chamber, with the inlet valve situated below the exhaust valve. The inlet valve was operated directly from the camshaft via a tappet, whereas the exhaust valve was operated via a push rod and a rocker lever. The propeller was mounted directly on the camshaft, which was driven from the crankshaft via reduction gearing consisting of spur gears.
138:. The main changes in design included an increased angle between the two rows of six cylinders, now being placed at an 90° angle instead of 60° at the previous V-12. Another change was the increase of the displacement, with cylinder dimensions of 105 mm bore and 130 mm stroke. The engine was similar in construction to the
149:
A single camshaft was situated between the two rows of cylinders and operates the inlet and exhaust valves of both cylinder rows, with each valve operated by a separate cam on the camshaft. The inlet and exhaust valves sat vertically opposed in a lateral pocket of the cylinder head on the side of the
146:
cylinders was generated with a fan driven from the rear end of the crankshaft. The fan was blowing air into the sheet metal enclosed chamber between the two rows of cylinders, which then left the enclosure through the narrow spaces between the cylinders, passing through the cylinder's cooling-fins.
168:
Ignition was supplied by two magnetos, with each magneto separately serving one cylinder row. The two magnetos were mounted transversely on the top of camshaft on the propeller end. The drive shafts of the magnetos were joined together and driven from the camshaft via helical gears. Three types of
145:
The cylinders and cylinder heads were separate cast-iron pieces with cast fins for air-cooling. The cylinder head was tightened to the cylinder with a copper-asbestos washer, and then secured by a cross-shaped clamp which was bolted to the crankcase with four long studs. Airflow for cooling the
157:
The pistons, fitted with three cast iron rings, were made of steel and were connected to the crankshaft via master-and-slave connecting rods. The crankshaft had six throws and was supported by five plain intermediate bearings and two outer ball bearings.
153:
The lower part of the crankcase served as an oil reservoir. A pressurized oil lubrication system was fed by a gear pump located on the lowest point of the crankcase. The oil pump was driven over a vertical shaft from the camshaft via helical gears.
515:
206:
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878:
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Instructions sur le RĂ©glage et l'Entretien du Moteur d'Aviation 130 Chevaux Ă Ailettes Ă l'usage des MĂ©caniciens d'Escadrilles. pp. 25-34
162:
165:
42 DC dual carburetors were fitted on the engine, one on each side of the crankcase, with each dual carburetor feeding one cylinder row.
883:
597:
577:
Instructions sur le RĂ©glage et l'Entretien du Moteur d'Aviation 130 Chevaux Ă Ailettes Ă l'usage des MĂ©caniciens d'Escadrilles
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Instructions sur le RĂ©glage et l'Entretien du Moteur d'Aviation 130 Chevaux Ă Ailettes Ă l'usage des MĂ©caniciens d'Escadrilles
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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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Notice sur les
Carburateurs Zénith - Spéciaux aux Moteurs d'Aviation Renault, 1916, pp. 1-9
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306:
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magnetos were used, ranging from Bosch Z.U.6 and S.E.V. C.6 magnetos to
Lavallette magnetos.
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http://www.wwi-models.org/app/sbj/srch/Macn.php?action=uArchList&subjId=288
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Instructions sur le
Montage et le RĂ©glage des Moteurs Renault Type 130 Chevaux
565:
Instructions sur le
Montage et le RĂ©glage des Moteurs Renault Type 130 Chevaux
262:
516:
Notice sur les
Carburateurs Zénith - Spéciaux aux Moteurs d'Aviation Renault
488:
28:
613:
582:
134:
The
Renault 130 hp V-12 engine was a development from the earlier
123:
75:
65:
122:
is a twelve-cylinder, air cooled 90° vee engine built by the French
586:
212:
One 130 hp
Renault 12Dc engine has been on display at the
530:. Flying Machines Press. pp. 163–166, 222–232, 233–243.
240:
12-cylinder, 90-degree Vee, air-cooled in-line piston engine
205:
One 130 hp
Renault 12Db engine is preserved at the
573:. Lyon: A. Bordet & Cie. (Renault engine manual)
567:. Lyon: A. Bordet & Cie. (Renault engine manual)
142:V-8 engine, also having the same bore and stroke.
526:Davilla, Dr. James J.; Soltan, Arthur M. (2002).
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383:Manuel d'aviation. Fascicule 5, 1916, pp. 143-148
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503:. Paris: Berger-Levrault. 1916. pp.
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528:French aircraft of the First World War
519:. Société du carburateur Zénith. 1916.
302:138 hp (103 kW) at 1,800 rpm
18:
7:
16:1910s French piston aircraft engine
14:
27:
221:Specifications (Renault 130 hp)
38:Royal Air Force Museum, Cosford
500:Manuel d'aviation. Fascicule 5
1:
879:1910s aircraft piston engines
479:. Otterbein Press. pp.
258:130 mm (5.118 in)
249:105 mm (4.134 in)
905:
473:Angle, Glenn Dale (1921).
623:
579:. (Renault engine manual)
431:Davilla 2002, pp. 233-243
419:Davilla 2002, pp. 222-232
410:Davilla 2002, pp. 163-166
267:350 kg (772 lb)
35:
26:
21:
884:Renault aircraft engines
440:Renault 12Db, Brussels,
339:List of aircraft engines
117:Renault 130 hp V-12
452:Renault 12Dc, Cosford,
367:Angle 1921, pp. 414-415
232:General characteristics
214:Royal Air Force Museum
130:Design and development
36:Renault 130 hp at the
889:V12 aircraft engines
321:Related development
207:Brussels Air Museum
108:Renault 100hp V-12
83:Major applications
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307:Compression ratio
200:Preserved engines
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333:Related lists
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327:Renault 80 hp
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617:aero engines
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173:Applications
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688:265 hp V-12
683:200 hp V-12
678:190 hp V-12
668:120 hp V-12
663:100 hp V-12
294:Performance
216:in Cosford.
189:Farman F.40
179:Caudron R.4
136:100 hp V-12
96:Farman F.40
88:Caudron R.4
54:aero engine
873:Categories
537:1891268090
345:References
280:Air-cooled
272:Components
263:Dry weight
858:Bengali 6
853:Bengali 4
633:45 hp V-8
547:Renault.
489:23525261M
226:Data from
126:company.
316:See also
614:Renault
505:143-148
481:414-415
458:photo 2
454:photo 1
124:Renault
76:Renault
673:160 hp
534:
487:
254:Stroke
163:ZĂ©nith
66:France
51:inline
48:Piston
658:90 hp
350:Notes
289:0.5:1
238:Type:
228:Angle
44:Type
803:12Fe
532:ISBN
245:Bore
161:Two
115:The
848:18J
843:12T
838:12S
833:12R
828:12N
823:12M
818:12K
813:12J
808:12H
798:12F
793:12E
788:12D
783:12A
718:626
713:468
708:456
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698:446
693:438
875::
778:9P
773:9C
768:9A
763:8G
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753:8B
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733:6P
728:4P
723:4B
485:OL
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