Wankelmotoren aller Art!

Hallo Leute

Ich habe gerade ein Forum gefunden, wo ein Mitglied eine ganz schöne Reihe von Wankelmotoren aufgelistet hat. Ich hab es einfach hier reinkopiert.
(orig. Quelle ist hier: http://www.ar15.com/archive/topic.html?b=8&f=36&t=266423 )

"Power figures are SAE net unless noted SAE gross, DIN, or JIS. Early (1960 and before) German horsepower figures are almost certainly gross even if not marked as such. American horsepower appears to have gone to net about 1970. Multiplying JIS by .80 or .85 gives SAE net.

Engine capacities are quoted as single chamber capacity. Various bodies de-rate the RCE by applying coefficients of 1.7, 1.8, 2.0 or even 3.0 to boost the apparent size.
NSU / Wankel Engines

Eng. Yrs Model cc x rotors Comp BHP/rpm, Torq(lb-ft/rpm)

DKM 32 35 Wankel's first experiment, non-operational
DKM 54 57 experimental 125 x 1 29 hp net at 17,000 rpm
KKM 125 58 (aka KKM 57) 125 x 1 25-30/10-12,000 net
KKM 250 59 exp. auto power 250 x 1 44/9000 gross
KKM 400 60 exp. auto 400 x 1 51/6000 net
KKM 60 60 Mk I exp aircool 60 x 1 3/6000
KKM 60 61 Mk II exper. 60 x 1 6/6000
KKM 150 61 prod. prototype 150 x 1 18/6000 net
KKM 150LI 61 port. fire pump 150 x 1 13.5/6000 net
KKM 2x300 61 295 x 2 = 590 66/6000 net
KKM 500X1 61 exp. 500 x 1 60/6000 net
61 NATO drone x 2
61 motor scooter
KKM 60 62 Mk III exper. 60 x 1 4.2/6500
KKM 507 63 exp. from 500X1 500 x 1 18/5000 net
KKM 509/506 64 exp. 498 x 2 = 996 110/6000 net
KKM 510 64 exp. air cool 215 x 1 10.5/5000 net
KKM 502 62-3 Spider Test 498 x 1 8.6 50/6000 net 52/2500 DIN.
KKM 502 64-67 Spider 498 x 1 = 498 8.6 64/5000, 54/3000 SAE
KKM 512 65 exp., military 498 x 2 = 996 110/6000 net
KKM 514 65-69 exp. air cool 500 x 2 = 1000 35/5000 net. Fr KKM 507
KKM 513 66 exp. liquid cool 500 x 1
KKM 613 66-67 from KKM 612 498 x 1 49/5500 net 51/2745
KKM 612 67-77 Ro80 115hp net 498 x 2 = 996 9.0 129/5800, 112/4500grSAE?
KKM 514 69 exp. air cool 500 x 2 = 1000 46/5000 net
KKM 619 69 x 3 150-180 bhp.
KKM 613 70 Citroën M35 x 1 49/5500 net 51/2745
KKM 622 73 Citr. GS birotor x 2 107 bhp
KKM 871 70-76 in Audi 100 test 750 x 2 = 1500 170 hp
W-87 marine aircool 108 x 1 = 108 8.5 8.7 hp 5800 rpm SAE 64lb
V-87 marine aircool 108 x 1 = 108 8.5 8.7 hp 5800 rpm SAE 68lb
W-120 marine aircool 160 x 1 = 160 8.0 12 hp 4700 rpm SAE 67lb
V-120 marine aircool 160 x 1 = 160 8.0 12 hp 4700 rpm SAE 76lb
H-120 marine aircool 160 x 1 = 160 8.0 12 hp 4700 rpm SAE 85lb
Audi ~85 Natural Gas stratified charge.

Mazda Engines

Eng. Yrs Model cc x rotors Comp BHP/rpm, Torq(lb-ft/rpm)

40A 61 experimental 386 x 1 = 386
L8A 62 experimental 399 x 1 = 399
L8A/0353 62 experimental 399 x 2 = 798
L8A/3804 63 experimental 399 x 3 = 1197
L8A/3805 63 experimental 399 x 4 = 1596 160/6000 gross
400/3867 67 experimental 395 x 2 = 790
400/3893 69 experimental 495 x 2 = 990
3912 70 experimental 356 x 1 = 356 35 bhp
X002 70 experimental 360 x 1 = 360
3915 70 experimental x 1 = 360?
6A 70s experimental 573 x 1 = 573 from 12A
7A 70s experimental 654 x 1 = 654 from 13B
2002 71 experimental 491 x 4 = 1964 180/6000 (from 10A)
10A/3820 64 prototype 491 x 2 = 982
10A/0810 67 Cosmo L10A 491 x 2 = 982 110/7000 (gross)
10A/0813 68 Cosmo L10B 491 x 2 = 982 128/7000 (gross)
10A/0820 68 Cosmo 491 x 2 = 982 100/7000 (gross)
10A/3883 68 Singapore GPrace 491 x 2 = 982 204 bhp
10A/0820 69-72 Presto (JpnR100) 491 x 2 = 982 100/7000 98/3500
10A/3877 69-72 R100(US) 491 x 2 = 982 100/7000 92/4000 akaM10A
10A/0866 71-5? RX-3(Jpn) 491 x 2 = 982 105/7000 (gross)
10B 68-69 Cosmo 128 (gross)
12A/3830 66 experimental 573 x 2 = 1146
12A/3872 68 prototype 573 x 2 = 1146
12A/3830 66 prototype 573 x 2 = 1146
12A 70-71 R100 573 x 2 = 1146 9.4 100/7000 (gr.), 92/4000
12A 70-71 RX-2 573 x 2 = 1146 9.4 120 (gross)
12A 72 R100 573 x 2 = 1146 9.4 77/6000, 80/4000
12A/3905 72 RX-2 US 573 x 2 = 1146 9.4 102/6800, 98/4000 net
12A/R612 72-75 RX-3 US 573 x 2 = 1146 9.4 90/6000, 96/4000 net
12A 73 Luce GR (Japan) 573 x 2 = 1146 9.4 120/6500, 116/3500 DIN
12A 73 Luce GR AP (Jpn) 573 x 2 = 1146 9.4 115/6500, 114/3500 DIN
12A 73 Luce GR II (Jpn) 573 x 2 = 1146 9.4 130/7000, 120/4000 DIN
12A 73 Luce GR IIAP (J) 573 x 2 = 1146 9.4 125/7000, 117/4000 DIN
12A 73 RX-2 573 x 2 = 1146 9.4 97/6500, 96/4000
12A 73 LeMans race tune 573 x 2 = 1146 250/8000
12A SIP 74 RX-2 573 x 2 = 1146 9.4 97/6500, 96/4000
12A 76 RX-3 Nikki 2bl 573 x 2 = 1146 9.4 95/6000, 102/4000
12A 77-78 RX-3SP 573 x 2 = 1146 9.4 95/6000, 102/4000
12ASport 77 Sports Kit(race) 573 x 2 = 1146 9.4 250+/9000
12A 79-80 RX-7 573 x 2 = 1146 9.4 100/6000, 105/4000
12A Lean 81-85 RX-7 US LeanBurn 573 x 2 = 1146 9.4? 100/6000?, 105/4000?
12A 6PI 82-85 Luce,Cosmo (Jpn) 573 x 2 = 1146
12A/Turb 83-8? Luce,Cosmo,RX-7 573 x 2 = 1146 8.5 160/6000JIS, 165/4000
12A/Turb 8?-85 Luce,Cosmo,RX-7 573 x 2 = 1146 8.5 165/6000JIS, 165/4000
12A 84-85 RX-7 (S,GS,GSL) 573 x 2 = 1146 9.4 101/6000, 107/4000
12B 73-75 racing one distr 573 x 2 = 1146 250+/9500
13A/0823 70-72 R130 front drv 655 x 2 = 1310 9.1 126/6000, 127/3500
13B 73 R130 (Japan) 654 x 2 = 1308 9.1 125/6000, 127/3500
13B 74-75 RX-4 654 x 2 = 1308 9.2 110/6000, 117/3500
13B 76-78 RX-4 654 x 2 = 1308 9.2 110/6000, 120/4000
13B 76-78 RX-5 (Cosmo) 654 x 2 = 1308 9.2 110/6000, 120/4000
13B Race 77 Racing 654 x 2 = 1308 9.4 290+/9000
13B Race 79 Le Mans Racing 654 x 2 = 1308 285/9000
13B Race 80 Le Mans Qualify 654 x 2 = 1308 300
13B Race 80 Le Mans Racing 654 x 2 = 1308 290/8500
13B DEI 83+ Cosmo,Luce,RX-7 654 x 2 = 1308
13B Race 84 Le Mans, factory 654 x 2 = 1308 330 sprint, 310 enduro
13B Turb 84 Racing 654 x 2 = 1308 7.5 500/8000, 326/7500
13B DEI 84-85 RX-7 (GSL-SE) 654 x 2 = 1308 9.4 135/6000, 133/2750
13B DEI 86-89 RX-7 2nd gen 654 x 2 = 1308 9.4 146/6500, 138/3500
13B Turb 86-89 RX-7 Turbo II 654 x 2 = 1308 8.5 182/6500, 183/3500
13B 89 Luce (Japan929) 654 x 2 = 1308 8.5 177/6500, 181/3500 JIS
13B VDEI 89-92 RX-7 Light Rotor 654 x 2 = 1308 9.7 160/7000, 140/4000
13B Turb 89-91 RX-7 T II Lt Rtr 654 x 2 = 1308 9.1 200/6500, 196/3500
13B Twin 92+ RX-7 Seq. Turbo 654 x 2 = 1308 9.0 255/6500, 217/5000
MSPRE 95+ RX-01 MulSidPrt x 2 220/8500, 159/6500
13G racing x 3
13J racing x 3
15A 73 experimental 737 x 2 = 1474 135/5750gross, 145/3500
84/5 MX-03 (exp) 654 x 3 = 1962 320/7000 JIS, 290 lbft
20G x 3
21A R-II 72 experimental 1046 x 2 = 2092 (22A 2x1169cc planned)
R26B racing 448 lb-ft 654 x 4 = 2616 700/9000 62mkg/6500
ROSCO 70s proposed stratified charge, late 70s
SCP proposed precombustion chamber engine
TISC experimental supercharged
DISC 80s late 80s
DISC-II 90s early 90s
Miller 90s Miller Cycle RCE
HR-X exp. hydrogen
HRX-2 exp. hydrogen

Mid-West Engines (background)

Eng. Yrs Application cc x rotors Comp BHP/rpm, Torq(lb-ft/rpm)

AE 50R 95-now aircraft 294 x 1 = 294 9 50
AE 100R 96-now aircraft 294 x 2 = 588 9 100
AE 110R 97-now fuel-inj. 294 x 2 = 588 9 105. aka GAEI 100R

Moller International (background)

Eng. Yrs Application cc x rotors Comp BHP/rpm, Torq(lb-ft/rpm)

PA 530 95-now aircraft, water 530 x 1 = 530
PL 1060 95-now aircraft, water 530 x 2 = 1060 150 est.

Curtiss-Wright

Eng. Yrs Application cc x rotors Comp BHP/rpm, Torq(lb-ft/rpm)

RC1-60 59 side port in 980 x 1 = 980 105/6000 108/3500
RC1-60 59 peripheral in 980 x 1 = 980 160/7000 135/5000
RC4-60 60 1st multi-rotor 980 x 4 = 3920 425/6500 400/4000
RC1-1920 60 Monster! 31500 x 1 =31500 782/1525
RC1-4.3 61 air-cooled 70.5 x 1 = 71 3.5/4000 bhp
RC1-4.3 61 air-cooled 70.5 x 1 = 71 3.5/4000 bhp
RC2-8.6 61 H20 cool 141 x 2 = 282 50/12000
RC2-602 61 980 x 2 = 1960 215/5000 212/3500
RC1-60J1 62 twin plugs 980 x 1 = 980 107 hp
RC1-60 62 stratified ch. 980 x 1 = 980
RC4-60J2 62 military 980 x 4 = 3920
RC2-60U5 63-68 vehicles 980 x 2 = 1960 200/5500 gross 200/4300
RC1-60J4 65 air cool 980 x 1 = 980
RC2-60M4 marine 980 x 2 = 1960 200/5500 continuous
RC2-60N 65? power generation 980 x 2 = 1960 95/4800 net contin.
RC2-60T3 66-68 military 980 x 2 = 1960 185/5000 gross
RC2-60U10 65-67 veh., per., JP4 980 x 2 = 1960 178/5000 to RollsRoyce
RC2-60U10 65-67 veh., side, JP4 980 x 2 = 1960 155/5000 to RollsRoyce
RC2-60Y8 66-68 QStar, Cessna177 980 x 2 = 1960 185/5000 gross
RC2-90Y2 66 aviation 1467 x 2 = 2934 275/6000 aka YRC-180-2
RC1-90 67-70+ H20 cool, per. 1467 x 1 = 1467
RC2-90J6 980 x 2 = 1960
RC2-75Y1 72 avi. mockup 1222 x 2 = 2444 285/6000 projected

Daimler-Benz

Eng. Yrs Application cc x rotors Comp BHP/rpm, Torq(lb-ft/rpm)

KP Serie 62 experimental 700 x 1 = 700
KP Serie 62 experimental 700 x 2 = 1400
KA Serie 65-66 Fuel inj. Cars 450 x 2 = 900
KA Serie 65-66 Fuel inj. Cars 450 x 3 = 1350
KC Serie 67 560 x 2 = 1120
KC Serie 67 560 x 3 = 1680
KE Serie 69 C111 600 x 3 = 1800 280/7000 net 220/5-6500
KE Serie 70 C111 305-400bhp 600 x 4 = 2400 350/7000 net 290/4-5500

Fichtel & Sachs

Horsepower figures are net.

Eng. Yrs Application cc x rotors Comp BHP/rpm, Torq(lb-ft/rpm)

KM 3 72 lawnmower 110 x 1 = 110 3/3300
KM 24 72+ snowmobiles 294 x 1 = 294 23/6000 21.7/4800
KM 37 65+ stationary 108 x 1 = 108 6.6/5500
KM 48 65+ stationary 160 x 1 = 160 8/4800
KM 914A 67+ station. aircool 303 x 1 = 303 16/4500 18.8/3500
KM 914B 67+ snowmobiles 303 x 1 = 303 19/5500 20.3/4000

Rolls-Royce

Developed experimental two stage units with low and high pressure stages to achieve Diesel cycle operation.

Eng. Yrs Application cc x rotors Comp BHP/rpm, Torq(lb-ft/rpm)

R1 66-67 exp. 2 stage 500 + 1126 = 1726 55/4500
R2 66 exp. 2 stage
R3 HP stage 1216 180/4500
R6 72 exp 2stg (1265+3250) x 2 = 9030 350/4500 expected

Norton

Eng. Yrs Application cc x rotors Comp BHP/rpm, Torq(lb-ft/rpm)

EMAP 70s NVT proto.
Interpol motorcycle 294 x 2 = 588 9.0 63 (85bhp)/9000
Classic 88 motorcycle 294 x 2 = 588 7.5 79/9000
Commander 88 Commander mcycle 294 x 2 = 588 9 85/9000
F1 90+ sport motorcycle 294 x 2 = 588 9 95PS/9500, 57/7500
NR 642 ~89 Light aircraft 90 bhp
NR 622 80s Ultra light aircraft 82 bhp
P62 80s from NR 622 90 bhp
NR 731 ~89 target drone 38 bhp
NR 801 ~89 Ultra light aircraft 23 kg 50/7500 or 40bhp/6000

Other Engines

Eng. Yrs Application cc x rotors Comp BHP/rpm, Torq(lb-ft/rpm)

Graupner 71-now models, toys 5 x 1 = 5 1.27 bhp Graupner/OS
Yanmar 69-73 R220 outbd mar. 220 x 1 22.5/6000 net
Yanmar 69-73 R450 outbd mar. 450 x 1 50/6000 net
- 70+ Hercules W2000 294 x 1 = 294 8.5 32/6500, 24.5/4500
OMC 471 72+ snow 528 x 1 = 528 35/5500, 37.5/4000
GM 73 prototype = 3300 (200ci)
Yamaha 73 motorcycle 330 x 2 = 660 68/6500
VW 70s 5 chamber KKM by Peter Hofbauer
Suzuki 75-76 RE5 motorcycle 497 x 1 = 497 8.6 48/6500, 45/3500 actual
- 76 Van Veen OCR 500 x 2 = 1000 110
Ingersoll ~86 Ingersoll-Rand IR-2500 41000 cc?
Lada 80s Soviet car x 2
Lada 80s car/ambul/mil. x 3 120-280 bhp
J Deere 80s stratified charged (SCORE?) 2250 bhp
J Deere 80s proposed tank engine 750 bhp,22.5 cu ft space
J Deere conv. Mazda to Nat. Gas
J Deere Nat. Gas 5800 x 1
Moller 85+ R&D based on OMC single rotor air-cooled eng.
Moller P1060 research
Moller 93+ RotaPower 375? x 2 = 750?
Moller 95+ Moller 530 I RotaPower 150 hp
Alturdyne/Alturair based on Mazda? San Diego 350 hp

DawnStar 95+? Israel, 95 lbs, 38 bhp (claim) 20 (est)"