- Thread starter
-
- #21
Ad: This forum contains affiliate links to products on Amazon and eBay. More information in Terms and rules
As for re-engined B-17s, I like the concept of master-slave engines. The Do-217P used it, with one DB-605 acting as supercharger for two DB-603 engines - the plane was able to do beyond 700 km/h above 10 km altitude IIRC. So I'd propose the 4 x Allison on wings, and 5th in hull, acting as 'slave'. Of course, the MG turrets and posts would be deleted, and crew cut down to 4-5 members. The resulting plane would render the 90% of German AAA useles, since it would fly at 40kft (hopefully). Same for Fw-190 Bf-109.
.
Real Hurricanes were armed with twin 40mm cannon so why not give yours three? The other two being outboard in the normal fashion.
I have no hard proof that 'my' B-17 could do what I was claiming, but this is a what-if thread anywayNo reason to suppose any such performance. Look up the XB-38. A B-17 with four turbo-charged Allison engines. 1425 hp apiece to 25,000ft.
Changing the supercharger system to a master-slave set up isn't going to increase the basic HP of the engines. Considering the fact the the German set up decreased in HP as it went up from 3500hp total for take off to 3240Hp at 18,700ft to 2880hp at 45,000ft. the American system of maintaining take-off power to 25,000 ft doesn't look so bad. I would also note that the DO-217P carried NO internal bombs.
For a bit of a reality check on some of the performance figures I might suggest looking at the Savoia-Marchetti SM.92. 382mph with two DB 605s.
Lets see some twin bombers.
For a bit of a reality check on some of the performance figures I might suggest looking at the Savoia-Marchetti SM.92. 382mph with two DB 605s.
Here 'tis, placing of 5th engine (original picture from our forum):
I've just checked out the data for SM.92- the plane was a real blooper. Eg. Fiat G.55 was faster with just one DB-605. But Italians had another plane that disappointed them similarly - Ba.88 - voted many times as worst of WW2 planes in our forum. Even some Ambrosini fighters with 750 HP were faster (but with less firepower, admitedly). I guess there are excellent designs, and there are bad ones
I'm also deleting the MGs (10-11 x 90 lbs = cca 1000 lbs), ammo (? lbs), 5-6 crew members their flak jackets (x 200 lbs per man = cca 1000 lbs), turrets their armor (??lbs) - perhaps 2500-3000 lbs saved on these accounts. The drag of cooling system is less then the drag of MG turrets, single MGs and MG openings.It still doesn't make much sense. you are replacing 800-1000lbs of turbo superchargers with 1600-1800lb worth of 5th engine, radiator, oil cooler PLUS the weight of the central supercharger PLUS the weight of the ducting to get the air to the engines in the wings. You also have the cooling drag of the 5th engine. You would probably get some increase in performance but is it enough to make the project worth while?
Your proposed engine location is aft of the center of gravity and would require some shifting or removal of weight. deleting ball turret and waist guns and gunners would help but this is in the nature of balancing the plane and canceling weights rather than reducing weight for performance gain.
the French and Germans who used this system didn't have workable turbo-chargers.
Your additional thrust from exhaust gases might help cancel the fuel burn of the 5th engine to help keep the range of the aircraft but since the exhaust thrust also varies with the speed (better at higher speeds) bomber cruising speeds might not give you the boost that fighters get.
I am not sure how it is a "blooper"?
It is after all 30-40 mph faster than an BF 110 using the same engines and it is alsol faster than than a ME 210 using the same engines.
It is almost the same speed as a ME 410 using 1750hp DB 603s. With three 20mm cannon and 5 12.7 mm mgs it doesn't look like it sacrificed much armament to it either.
The 1200 mile range without drop tanks might have something to do with it also.
I'm also deleting the MGs (10-11 x 90 lbs = cca 1000 lbs), ammo (? lbs), 5-6 crew members their flak jackets (x 200 lbs per man = cca 1000 lbs), turrets their armor (??lbs) - perhaps 2500-3000 lbs saved on these accounts. The drag of cooling system is less then the drag of MG turrets, single MGs and MG openings.
Is my project worthwhile? Again, I can't prove it, but in my eyes it has merit
The Russians ditched weight because their engines couldn't make any more power.Then I'd say we disagree
Russians were known for cutting the weight to gain performance, and NAA also put P-51 to the treatment to have P-51H.
the Higher the bombers flew the worse the accuracy of bombing was. stripping out a few thousand pounds of weight from the B-17/XP-38 might have given it a few thousand more feet of ceiling and accomplished much of your goal with less trouble. Standard B-17s were credited with about 7,000ft more ceiling than B-24s and their turbo charged cyclone engines could cruise at 35,000ft putting out 750HP for as long as the fuel would last. The turbo Allisons should do a bit better.Despite employing turbo-chargers, B-17s and B-24s could not owerflew the 109/190 combo and heavy AAA, so I propose something that could
Do-217 had the boost, and flew as high as 53kft (data from Wiki), and it was bomber. So I'd guess again that concept had merit
If the plane really used 2 x DB 605 (x 1450 HP) engines and managed 610 km/h (with really low-drag airframe), it was way slower then P-38J with 2 x Allison ( x 1475 HP IIRC) that had bigger (=draggier) central nacelle.
It would be a significiant boost for Italian air force, but I guess they prefered G.55 and Re 2005.