351:
202:
262:
29:
320:. It was also to have had a two-stage three-speed supercharger, producing 2,350 hp (1,750 kW; 2,380 PS) at 3700 rpm for take-off. It would have weighed 1,055 kg (2,326 lb). There was no time to work this change into the production line before the war ended. Other experimental models included the
225:
The 213A (the main production series, with single-stage two-speed supercharging) first ran in 1940, but experienced lengthy delays before finally being declared "production quality" in 1943. Production was extremely slow to ramp up, in order to avoid delays in the existing Jumo 211 production. By the
212:
After redesigning the engine block to a smaller external size to suit the increased cooling power – while keeping the same 150 mm x 165 mm bore/stroke figures, maintaining the 35 litre displacement of the Jumo 211 series – and then further increasing boost settings on the supercharger, the
172:
used a pressurized coolant system that ran at the same pressure regardless of altitude, raising the boiling point to about 110 °C. This allowed it to use considerably less water for the same cooling effect, which remained the same at all altitudes. Although otherwise similar to the Jumo 211 in
180:
firm was not happy with this state of affairs, and started its own efforts to produce a pressurized cooling system as early as 1938. Experiments on the 211 proved so successful that it became clear that not only could the engine be built smaller and lighter (by reducing the water requirement), but
160:
When the Jumo 211 entered production in the late 1930s it used an unpressurized liquid cooling system based on an "open cycle". Water was pumped through the engine to keep it cool, but the system operated at atmospheric pressure, or only slightly higher. Since the boiling point of water decreases
447:
2x 24H engines in tandem driving co-axial propellers. Example exhibited at 1946 Paris Air Show had take-off power of 7,200 hp (5,400 kW). Proposed for Sud-Est SE.1200 trans-Atlantic flying boat project, which would have used four 24H Tandem installations, each rated at 8,000 hp
221:
of 44.52 litre displacement. Junkers decided to go after the 603's market, and placed the 213's mounting points and fluid connections in the same locations as the 603, allowing it to be "dropped in" as a replacement, with the exception of the Jumo's standard starboard-side supercharger intake
309:), completely unitized power plant "modules" for any twin or multi-engined aircraft, much as the Jumo 211 had evolved for earlier aircraft designs – but with the annular radiators noticeably reconfigured for better cooling of the more powerful Jumo 213 engine.
173:
most respects, the 601 was smaller and lighter than the 211, and could be run at higher power settings at higher altitudes, making it popular in fighter designs. The 211 was relegated to "secondary" roles in bombers and transports.
161:
with altitude (pressure) this meant that the temperature of the cooling water had to be kept quite low to avoid boiling at high altitudes, which in turn meant that the water removed less heat from the engine before flowing into the
147:
which allowed the engine to be built smaller and lighter, and a number of improvements that allowed it to run at higher RPM. These changes boosted power by over 500 hp and made the 213 one of the most sought-after
440:
engine utilizing 12H cylinder blocks, crankshafts and pistons mounted on a new crankcase driving a single propeller. Rated at 3,600 hp (2,700 kW) take-off power and 3,000 hp (2,200 kW) at rated
226:
time the engines were available in any sort of number in 1944, Allied bombing repeatedly destroyed the production lines. Production of the A model was limited to about 400–500 a month for most of 1944/45.
281:
for additional high-altitude performance, while the F model lacked this and was optimized for slightly lower altitudes. The E and F models were in high demand for many late-war aircraft, including the
217:
model was able to deliver 1,750 PS (metric hp) at 3,250 RPM. This made it considerably more powerful than the corresponding DB 601E which provided 1,350 PS, and about the same power as the much larger
277:. These engines were equipped with a new two-speed, two-stage supercharger that dramatically improved altitude performance. The only difference between the two models was that the E included an
965:
390:
High altitude version of 213A, equipped with a three-speed two-stage intercooled supercharger and delivering 1,750 PS take-off power (2,050 PS with MW 50 boost).
301:. All of these aircraft used annular radiators characteristic of the earlier Jumo 211 engine installations on twin-engined aircraft, often standardized as
1170:
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879:
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model, which delivered 1,340 PS (1,322 hp, 986 kW) at 2,600 RPM, up from 1000 PS at 2,200 RPM in the first version 211A.
415:
335:
402:
Project, redesigned with four valves per-cylinder and a two-stage three-speed supercharger, delivering 2,380 PS at takeoff.
629:
162:
743:
513:
316:, which replaced the earlier model's three valves with a new four-valve-per-cylinder design for increased
246:
was essentially an A model with re-arranged secondary equipment (supercharger, oil pump, etc.) to allow a
686:
523:
317:
242:"C3" fuel, allowing the boost pressure to be increased and the take-off power improved to 2,000 PS. The
1123:
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Post-war development of the
Junkers Jumo 213 which had been in production for the Germans at the
81:
61:
1006:
181:
could be run at higher power settings without overheating. Additional changes to strengthen the
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894:
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143:. The design added two features, a pressurized cooling system that required considerably less
85:
872:
The Race for Hitler's X-Planes: Britain's 1945 Mission to
Capture Secret Luftwaffe Technology
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First version, 1,750 PS (2,100 PS with MW50 boost) take-off power, major production version.
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140:
111:
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661:
1,750 PS (1,726 hp, 1,287 kW) at 3,250 rpm for takeoff; rated altitude 9,600 m (31,500 ft)
562:
222:(Daimler-Benz inverted V12 engines always had the supercharger intakes on the port side).
136:
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51:
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A range of advanced versions were also developed during the lengthy teething period. The
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As 213A but equipped for mounting of a cannon firing through the propeller axis (
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Project, a 213A with C3 fuel (100 octane) and up to 2,000 PS take-off power.
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437:
891:
World
Encyclopedia of Aero Engines: From the Pioneers to the Present Day
261:
974:
465:
455:
265:
Junkers Jumo 213E-1 at
Flugmuseum Aviaticum in Wiener Neustadt, Austria
44:
28:
384:
213C with a new three-speed supercharger, did not enter production.
349:
260:
200:
633:
947:
354:
A Jumo 213-powered Ju 188, with reconfigured annular radiators
664:
2,050 PS (2,022 hp, 1,508 kW) for takeoff with MW50 injection
258:
and improved altitude performance, but it was not produced.
334:
Further development of the Jumo 213 was carried out at
424:
2x 12H engines in tandem driving co-axial propellers.
1116:
1095:
984:
312:A further substantial upgrade was projected as the
865:. London: Sampson Low, Marston & Company, Ltd.
254:added a new three-speed supercharger for smoother
396:Similar to the 213E, but without the intercooler.
545:12-cylinder supercharged liquid-cooled inverted
250:cannon to fire through the propeller shaft. The
205:Jumo 213 fuel injector system components in the
959:
934:Jumo 213-powered Fw 190D engine startup video
796:"Arsenal 24H and 24H Tandem Aircraft Engines"
8:
269:The next major production versions were the
966:
952:
944:
939:Enginehistory.org's Junkers Jumo 213 page
844:Major Piston Aero Engines of World War II
910:Junkers Aircraft & Engines 1913–1945
789:
787:
760:
846:. Shrewsbury, UK: Airlife Publishing.
18:
912:. London: Putnam Aeronautical Books.
645:Pressurized water up to 120°C (248°F)
7:
893:(5th ed.). Stroud, UK: Sutton.
863:Jane's All the World's Aircraft 1948
777:
775:
773:
189:for increased boost resulted in the
152:engine designs in the late-war era.
14:
1138:(Junkers design built by Heinkel)
636:injection into the intake and an
1171:Inverted aircraft piston engines
673:50 PS/L (0.81 hp/in³, 36.8 kW/L)
27:
430:Further development of the 12H.
794:Pearce, William (2016-02-26).
408:Proposed turbocharged variant.
324:for low-altitude use, and the
1:
1166:Inverted V12 aircraft engines
1161:1940s aircraft piston engines
874:. Stroud, UK: History Press.
630:centrifugal type supercharger
238:was designed to run on 100
1187:
870:Christopher, John (2013).
861:Bridgman, Leonard (1948).
828:Bridgman 1948, pp. 47d–48d
682:6.5:1 (B4 fuel, 87 octane)
530:Specifications (Jumo 213E)
1132:
619:Three valves per cylinder
416:Arsenal de l'Aéronautique
336:Arsenal de l'Aéronautique
185:and add a fully shrouded
35:
26:
21:
1156:Junkers aircraft engines
842:Bingham, Victor (1998).
744:List of aircraft engines
691:1.37 kW/kg (0.83 hp/lb)
537:General characteristics
514:Messerschmitt Me 209-II
139:'s earlier design, the
889:Gunston, Bill (2006).
628:Two-stage three-speed
549:piston aircraft engine
464:The Arsenal 12K after
454:The Arsenal 12H after
378:), limited production.
355:
266:
209:
168:By contrast, the 1940
156:Design and development
819:Bridgman 1948, p. 48d
687:Power-to-weight ratio
524:SNCASO SO.8000 Narval
353:
318:volumetric efficiency
264:
204:
908:Kay, Antony (2004).
338:in France after the
207:Technikmuseum Speyer
178:Junkers Motorenwerke
170:Daimler-Benz DB 601E
800:oldmachinepress.com
732:Rolls-Royce Griffon
717:Daimler-Benz DB 605
712:Daimler-Benz DB 603
135:, a development of
16:WW2 Aircraft Engine
781:Christopher, p. 79
767:Christopher, p. 78
701:Comparable engines
603:1040 kg (2,072 lb)
582:2,266 mm (89.2 in)
576:35 L (2,135.2 in³)
499:Focke-Wulf Fw 190D
479:Heinkel He 111H-22
444:Arsenal 24H-Tandem
421:Arsenal 12H-Tandem
356:
299:Focke-Wulf Ta 152H
295:Focke-Wulf Fw 190D
267:
210:
82:Focke-Wulf Fw 190D
77:Major applications
1143:
1142:
881:978-0-7524-6457-2
678:Compression ratio
567:165 mm (6.496 in)
558:150 mm (5.906 in)
509:Focke-Wulf Ta 154
504:Focke-Wulf Ta 152
468:absorbed Arsenal.
458:absorbed Arsenal.
230:Advanced versions
117:
116:
86:Focke-Wulf Ta 152
36:Junkers Jumo 213
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978:aircraft engines
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594:980 mm (38.6 in)
588:777 mm (30.6 in)
448:(6,000 kW).
340:Second World War
273:and the similar
121:Junkers Jumo 213
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133:aircraft engine
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928:External links
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293:models of the
291:Langnasen-Dora
287:Junkers Ju 388
283:Junkers Ju 188
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131:liquid-cooled
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107:Developed from
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738:Related lists
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727:Mikulin AM-35
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722:Klimov VK-107
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484:Junkers Ju 88
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975:Junkers Jumo
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836:Bibliography
824:
815:
803:. Retrieved
799:
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737:
736:
700:
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685:
676:
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655:
642:
624:Supercharger
622:
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597:
591:
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579:
572:Displacement
570:
561:
552:
542:
533:
473:Applications
375:
333:
328:
326:turbocharged
321:
313:
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290:
274:
270:
268:
256:power curves
251:
247:
243:
235:
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224:
214:
211:
190:
187:supercharger
177:
175:
167:
165:to cool it.
159:
125:World War II
120:
118:
97:Number built
650:Performance
638:aftercooler
519:Nord Noroit
461:SFECMAS 12K
451:SFECMAS 12H
433:Arsenal 24H
427:Arsenal 12K
411:Arsenal 12H
376:Motorkanone
279:intercooler
248:Motorkanone
52:aero-engine
1150:Categories
750:References
615:Valvetrain
608:Components
599:Dry weight
418:factories.
213:resulting
183:crankshaft
68:First run
1134:See also
1117:Turboprop
307:power-egg
191:Jumo 211F
47:inverted
22:Jumo 213
1096:Turbojet
696:See also
346:Variants
297:and the
163:radiator
141:Jumo 211
112:Jumo 211
592:Height:
580:Length:
466:SFECMAS
456:SFECMAS
441:height.
303:Kraftei
62:Junkers
1136:HeS 30
916:
897:
878:
850:
586:Width:
563:Stroke
289:, the
240:octane
219:DB 603
123:was a
101:9,000
45:Piston
805:8 May
755:Notes
632:with
543:Type:
127:-era
71:1940
41:Type
914:ISBN
895:ISBN
876:ISBN
848:ISBN
807:2016
634:MW50
554:Bore
438:H-24
405:J13T
399:213J
393:213F
387:213E
381:213D
371:213C
365:213B
359:213A
329:213T
322:213S
314:213J
275:213F
271:213E
252:213D
244:213C
236:213B
215:213A
197:213A
176:The
150:Axis
129:V-12
119:The
49:V-12
1124:022
1108:012
1103:004
1087:224
1082:223
1077:222
1072:218
1067:213
1062:211
1057:210
1052:208
1047:207
1042:206
1037:205
1032:204
1027:203
1022:L88
1017:L55
547:Vee
1152::
1012:L8
1007:L7
1002:L5
997:L2
992:L1
798:.
786:^
772:^
342:.
331:.
285:,
967:e
960:t
953:v
922:.
903:.
884:.
856:.
809:.
689::
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671::
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305:(
Text is available under the Creative Commons Attribution-ShareAlike License. Additional terms may apply.
