STUDY OF AN AERONAUTIC PLANETARY GEARBOX FOR A … Internet/Catalogo Tesi/Motori Diesel/Avio... ·...
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ALMA MATER STUDIORUMUNIVERSITA’ DI BOLOGNAFACOLTA DI INGEGNERIA
DEGREE IN MECHANICAL ENGINEERING
Graduation thesis by:
Simone Paolizzi
Supervisor:
Chiar.mo Prof. Ing. Luca Piancastelli
Academic year 2010-2011
Session I
STUDY OF AN AERONAUTIC PLANETARY GEARBOX FOR A COUNTER-ROTATING PROPELLERS PROPULSION SYSTEM
GOALS
STUDY OF A PLANETARY GEARBOX
- Variable step counter-rotating propellers
- Reduction from 6000 rpm to 1000 rpm
- Engine 1300 JTD 150 cv
RELIABILITY
SIMPLICITY
LIGHTNESS
Gears sizing
Components studying
It has been used the Solid Edge v.18utility ‘Spur gearing Component’
All the components have been sized andverified thanks to SolidWorks simulation
DESIGN DEVELOPMENT
Sun gear Planets
Ring gear Carrier
By vincolating or moving the elements in different waysit has been possible to obtain several working typologies
TWO DOFs
1 crankshaft:6000 rpm
2 propellerhubs:
1000 rpm
-1000 rpm
Only the carter is bolted to the engine basement
PUSHING PROPELLERS
CONTRACTING PROPELLERS
1250 rpm 1000 rpm
The speed of the propellers may be chosen between1250 rpm and 1000 rpm
due to a better gears proportions: 1000 rpmhas been chosen
Ring gearNumber of teeth : 77
Pitch diameter : 115.5 mmFacewidth : 26 mm
Sun gearNumber of teeth: 31
Pitch diameter: 46.5 mmFacewidth: 24 mm
PlanetNumber of teeth : 18
Pitch diameter : 27 mmFacewidth : 24 mm
GEARSModule = 1.5 Pressure angle = 20°
PLANET
Straight-sided splinesconnect to the driveshaft
Thrust bearing lock
CARRIER’S CLUSTER
Solution with pivot and internal bearings
Solution without pivotwith external bearings
The external bearings solution reduces the number of elements and consequentlyIt also increases the SF. In addition it has removed the wearproblems.
PLANETARY CLUSTER
Planet
Angular contact ballbearings SKF 7205
Seeger ring A25
Seeger ring J52
INTERNAL SHAFT HANDLING SYSTEM
Carrier
Thrust bearingSKF 51201
Combined needle rollerbearing SKF NKX-40
Roller bearingNK 28/20
Propeller’s flange
Lock nut KMFE6
EXTERNAL SHAFT HANDLING SYSTEM
Ring gear
Screw M5 x 15
Combined needle roller bearing SKF NKX-70
Roller bearing NK 75/25
Propeller’s flange
Lock nut KMFE11
CARTER
The carter is the only elementbolted to the crankcase and it isthe less stressed; since thepropellers are counter-rotating ,the gyroscopic moment is inequilibrium.For this reason only axial forces
act on the carter.
USED MATERIALS
Gears: steel 15NiCr13
Carrier, propeller’s flange, external shaft: titanium alloy Ti6Al4V
Carter: aluminum alloy 2024
FEM ANALYSIS
PlanetDeformation Scale Factor : 350 S.F.= 5.8
Sun gearDeformation Scale Factor: 492S.F.= 8.7
All the components are verified thanks to Solidworks simulation, which is a FEM software
CarrierDeformation Scale Factor : 28S.F.= 2.6
Ring gearDeformation Scale Factor : 2768S.F.= 6.7
External shaftDeformation Scale Factor : 651S.F.= 5.9
CarterDeformation Scale Factor : 199S.F.= 10
CONCLUSION
RELIABILITY The lowest safety factor is 2.6
LIGHTNESS
SIMPLICITY
ALL THE GOALS HAVE BEEN REACHED:
Due to a new planetary gears constructivesolution it has been possible to decrease theelement’s number in favor to a better simplicity
The whole gearing mass is 7.667 kg
FUTURE DEVELOPMENTS
Whereas the minimal safety factor is near to the straight-sided splines it is possibleto increase the reliability by substituting involute splines in place of straight-sidedsplines; in this way there is a larger range of gearing lightening.
The FEM check has been executed thanks to Solidworks simulation. In order toobtain Simulations closer to reality I suggest to use more flexible FEA softwares.
It might be interesting to have a second look to the project considering also theeconomical aspects, that in this work have not been considerated.