Tbag
12-06-2011, 08:18 PM
I know, i know, there are already a few out there (e.g. http://forum.1cpublishing.eu/showthread.php?t=24443). And I'm sure that there would be a more appropriate sub-forum. But I was worried that it might get lost there and now that there is a community manager I hope that this info might actually reach the devs. Fingers crossed :)
Since the Ju88 is one of my all-time favourites I started delving deeper into the original manuals. The Ju88 underwent literally 1000s of changes and therfore the Ju88 A-1 is very different in a lot of respects from, for example, the Ju88 A-4. Unfortunately there is far more information out there about the A-4 than about the A-1 (I'm more than happy to be proven wrong. If you have any Ju88 documents I'd be grateful if you could share them with me!).
Most of the systems of the Ju88 are implemented incorrectly in CloD when judging by the Ju88 A-1 manual from March 1940 (it is written for planes equipped with Jumo 2011B/1 engines). So I thought I simply start to put together what can be gathered from that manual. Today I will start with the propeller controls and will continue with the hydraulic system and the fuel system as soon as I find the time. Any constructive comments are of course welcome. Please PM me if you want a PDF of the manual.
Part 1: Propeller pitch control
The propeller pitch control in the J88 A-1 can be either set to manual or automatic. In both modes, an electrical motor changes the pitch of the propeller. In manual mode it works very much the same way than is already modeled in the Bf109 E-3 in CloD. In automatic mode a centrifugal governor keeps (or tries to keep) the RPM at 2350. The manual states the following things:
Propeller RPM: The ratio of engine RPM to propeller RPM is 1.68 (Page 0 III in the manual)
Manual control:
-The manual propeller pitch control lever is spring centered and needs to be held in the position "größer" (increase RPM) or "kleiner" to change the propeller pitch.
-The manual propeller pitch control lever can be locked in the position “Segelstellung” (feather).
-It takes about 40 seconds for the propeller to move into the position “Segelstellung” (it is interesting to note that in the Ju88 A-4 manual this time is given with 10 seconds)
-The propeller can only be moved from the position “Segelstellung” into the normal operating range by keeping the manual pitch control lever pushed forward. (Page 7 - 05)
-The 12 o’clock position on the propeller pitch indicator (it's mounted on the engine mount) equals 25 degrees propeller pitch (Page 7 – 87 in the manual)
Automatic control:
-In automatic mode a centrifugal governor keeps the RPM at 2350. (Page 7 - 05)
-The automatic control should be engaged during take-off and diving (Page 7 - 03)
Please see the image below for the location of the controls in the Cockpit:
http://img546.imageshack.us/img546/1390/propellercontrolunit2.jpg
Since the Ju88 is one of my all-time favourites I started delving deeper into the original manuals. The Ju88 underwent literally 1000s of changes and therfore the Ju88 A-1 is very different in a lot of respects from, for example, the Ju88 A-4. Unfortunately there is far more information out there about the A-4 than about the A-1 (I'm more than happy to be proven wrong. If you have any Ju88 documents I'd be grateful if you could share them with me!).
Most of the systems of the Ju88 are implemented incorrectly in CloD when judging by the Ju88 A-1 manual from March 1940 (it is written for planes equipped with Jumo 2011B/1 engines). So I thought I simply start to put together what can be gathered from that manual. Today I will start with the propeller controls and will continue with the hydraulic system and the fuel system as soon as I find the time. Any constructive comments are of course welcome. Please PM me if you want a PDF of the manual.
Part 1: Propeller pitch control
The propeller pitch control in the J88 A-1 can be either set to manual or automatic. In both modes, an electrical motor changes the pitch of the propeller. In manual mode it works very much the same way than is already modeled in the Bf109 E-3 in CloD. In automatic mode a centrifugal governor keeps (or tries to keep) the RPM at 2350. The manual states the following things:
Propeller RPM: The ratio of engine RPM to propeller RPM is 1.68 (Page 0 III in the manual)
Manual control:
-The manual propeller pitch control lever is spring centered and needs to be held in the position "größer" (increase RPM) or "kleiner" to change the propeller pitch.
-The manual propeller pitch control lever can be locked in the position “Segelstellung” (feather).
-It takes about 40 seconds for the propeller to move into the position “Segelstellung” (it is interesting to note that in the Ju88 A-4 manual this time is given with 10 seconds)
-The propeller can only be moved from the position “Segelstellung” into the normal operating range by keeping the manual pitch control lever pushed forward. (Page 7 - 05)
-The 12 o’clock position on the propeller pitch indicator (it's mounted on the engine mount) equals 25 degrees propeller pitch (Page 7 – 87 in the manual)
Automatic control:
-In automatic mode a centrifugal governor keeps the RPM at 2350. (Page 7 - 05)
-The automatic control should be engaged during take-off and diving (Page 7 - 03)
Please see the image below for the location of the controls in the Cockpit:
http://img546.imageshack.us/img546/1390/propellercontrolunit2.jpg