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For the 12Z, I have these curves too.
And a personal pic of the (big) 12Z Turbomeca supercharger, with well-known twin inlet, but single outlet :
Thank you both for those diagrams.
Am I correct that the PS system has three rows of inlet guide vanes with only the first being variable (and the other two locked and rotating with the centrifugal wheel while the Russian only had one set of inlet guide vanes.
EDIT - I have just read the USAAF report and realise I have misinterpreted the PS system - the PS system on the 12Z is downstream of the comprssor, not upstream as I was envisaging.
Nice photo. That distributor on the RH cylinder head - is it fuel injection or pneumatic starting?
Is there an on line manual for that engine?
No one claims that the principles were different.No one disputes that these two superchargers are constructed differently.
However, their operating principle is identical
The "moteur-canon" arrangement would have been ideal owing to the recoil expected from a weapon with a caliber significantly larger than the 20 mm HS 404.Something relevant to this thread: if all goes right I intend to go to the French archives again in the first week of October.
Among the documents I will be looking for are 1937-40 docs on the 33 mm APX and 30 mm MAT aircraft autocannons. This will be a nice opportunity to know more about these obscure guns and whether the French already airframes or engines (if motor-cannon) in mind for them.
If the documents on 30 mm and under AP ammo discuss ammo for aircraft autocannons, I will discuss those here as well.
????With these, an aircraft such as the Bloch 152 initially had structural problems, and the wings had to be reinforced with Bloch's famous diagonal ribs. But of course, two canons out of the propeller circle provided exceptional firepower compared to synchronized, and therefore necessarily slowed, cowl-mounted weapons.
It is sufficient even for 45 mm caliber.Returning to the "moteur-canon", the Hispano 12Y's hollow propeller shaft had an internal diameter of 61 mm. Was such a dimension sufficient for a 30 mm caliber weapon?
We will see if the docs say how it was supposed to be mounted or how large the barrel is.The "moteur-canon" arrangement would have been ideal owing to the recoil expected from a weapon with a caliber significantly larger than the 20 mm HS 404.
With these, an aircraft such as the Bloch 152 initially had structural problems, and the wings had to be reinforced with Bloch's famous diagonal ribs. But of course, two canons out of the propeller circle provided exceptional firepower compared to synchronized, and therefore necessarily slowed, cowl-mounted weapons.
Returning to the "moteur-canon", the Hispano 12Y's hollow propeller shaft had an internal diameter of 61 mm. Was such a dimension sufficient for a 30 mm caliber weapon?
????
Motor cannon were not synchronized. They shot through the hub so it didn't matter where the blades were.
On the other hand, the HS 404 was never synchronized. Perhaps the time between sear release and shell exiting barrel was too variable?
It any case it was never "cowl mounted".
The US .50 cal in cowl mountings suffered a huge loss in rate of fire.
It is sufficient even for 45 mm caliber.
The NS-45 had a barrel wall thickness of 4 mm (!!!) at the muzzle.Really? And what about the thickness of the gun barrel?
So the 33mm was indeed probably a motor-cannon, though I suspect that its integration to an Hispano-Suiza 12-cyl engine would look rather different to 20mm mountings. Then again, some Yaks with similar engines got to use 30 or 37mm ACs?
Yaks were fitted with 20 mm, 23 mm, 30 mm, 37 mm and 45 mm motor cannons. Khazanov and Gordon in Red Star Volume 5 note a single Yak-9 that was converted to use a 57 mm motor cannon as well. Considering this, it's a pretty reasonable conclusion that the MAT and APX motor cannons would work reasonably well in something like a D.520.- 33mm APX "machinegun", developped after the 120 rpm cannon tested in a Farman aircraft, firing through the propeller hub: 900 m/s, 250 rpm, in 1936 260 rpm was tested without trouble, updated in 1937 to 800 m/s and 300rpm, and finally 900m/s, 400rpm, 100kg weight without loader and ammo, still in development as of 1940.
- MAT (Tulle arsenal) 30x167mm aircraft gun: started development in 1936, 1000 m/s and 320 MPa pressure
So the 33mm was indeed probably a motor-cannon, though I suspect that its integration to an Hispano-Suiza 12-cyl engine would look rather different to 20mm mountings. Then again, some Yaks with similar engines got to use 30 or 37mm ACs?
Although I do wonder if they would be better suited for specialized aircraft like interceptors, or some kind of variant of a D.520 meant for bomber-busting. A 3 x 20 mm setup (especially if they get the belt feed for the 404's in service faster) is more than enough to deal with any fighter, and still quite solid against twin-engined aircraft; which raises the question of why a 30/33 mm with limited ammo capacity would be necessary.
Yaks were fitted with 20 mm, 23 mm, 30 mm, 37 mm and 45 mm motor cannons. Khazanov and Gordon in Red Star Volume 5 note a single Yak-9 that was converted to use a 57 mm motor cannon as well. Considering this, it's a pretty reasonable conclusion that the MAT and APX motor cannons would work reasonably well in something like a D.520.
Although I do wonder if they would be better suited for specialized aircraft like interceptors, or some kind of variant of a D.520 meant for bomber-busting. A 3 x 20 mm setup (especially if they get the belt feed for the 404's in service faster) is more than enough to deal with any fighter, and still quite solid against twin-engined aircraft; which raises the question of why a 30/33 mm with limited ammo capacity would be necessary.
Agreed.The "moteur-canon" concept assumes a hollow propeller shaft with an internal diameter larger than that of the integrated weapon.
Yes... but that's not enough!
The propeller hub and the entire blades control system must also have a large-diameter central hole. This isn't simple.
Having the working G&R 14R means they can have a single engine per a fighter and still have a lot of firepower, while not sacrificing the performance.And in any case, this concept remains a single-weapon system. Ultimately, the choice of a twin-engined, multi-gun aircraft in the nose isn't such a bad one.
In France, this could have been the Sud-Est 100 with G&R 14Rs, but without its unnecessary complications (landing gear, wooden wing structure, etc.).
This is relatively simple, compared to other problems encountered when mounting a large caliber gun on a motor - primarily, ensuring structural strength at high recoil. In general, any gun larger than 23mm caliber was redundant against German aircraft. How important big guns were for ground attacks is a question. Judging from Soviet pilots' accounts, they (ok, the most of them) were not thrilled with the heavy guns on Soviet fighters and ground attack aircraft, with perhaps one exception, the P-39.The propeller hub and the entire blades control system must also have a large-diameter central hole. This isn't simple.
Having the working G&R 14R means they can have a single engine per a fighter and still have a lot of firepower, while not sacrificing the performance.