Uni-UAV ~
Power Train - Reduction - Final
Overview:
Use angular spiral bevel gear.
Picture:
Eventually
Working Papers:
|
|
DESIGN: |
|
MAKE: |
|
Items:
DESIGN:
|
|
Name |
Item |
|
|
|
|
MAKE:
|
|
Name |
Item |
|
|
|
|
BUY:
|
|
Name |
Item |
|
|
|
|
Item page stuff.
4:1 intermediate to rotorhub.
Or is it to be 3:1.FORM: Arrow Spiral Stock Gear Selection.
This is for 3:1 for the basic and smallest Arrow gear 10.0 PD, 16/48 tooth. 10P45L15 & 10P15R45. Spiral bevel.
|
|
Horsepower: |
11.4 |
hp |
|
|
Pinion Speed: |
1288 |
rpm |
|
|
Pinion Working Torque: |
558 |
in-lb |
|
|
Estimated Rated Pinion Torque: |
1116 |
in-lb |
|
|
Catalog Rated Pinion Torque: |
540 |
in-lb |
|
|
Catalog Pinion Pitch Diameter: |
1.5 |
in |
|
|
Pitch Line Velocity: |
506 |
ft/min |
|
|
Dynamic Factor: |
0.881 |
|
|
|
Allowable Pinion Torque: |
476 |
in-lb |
|
|
Service Factor: |
.853 |
:1 |
FORM: Hamilton Bevel Gear Selection.
This is for Rush Gears page 557, Straight teeth
|
|
Pinion Speed |
1289 |
|
rpm |
|
|
|
Catalog Pinion Pitch Dia. |
1.5 |
|
in. |
|
|
|
Pitch Line Velocity |
507 |
|
ft/min |
|
|
|
Diametral Pitch |
12 |
|
|
|
|
|
Face Width |
0.61 |
|
in |
|
|
|
Allowable Contact Stress |
200,000 |
|
Steel Rockwell 55 min. |
|
|
|
Allowable Bending Stress |
300,000 |
|
Steel Rockwell C 55 min. |
|
|
|
Elastic Coefficient |
Pinion & Gear - Steel |
|
|
|
|
|
Load Distribution Factor |
Neither member straddle mounted |
|
|
|
|
|
Geometry Factor [I] |
.074 |
|
|
|
|
|
Geometry Factor [J] |
.225 |
|
|
|
|
|
Durability |
4.0 |
|
hp. Service factor is 0.35 (1) |
|
|
|
Strength |
7.4 |
|
hp. Service factor is 0.65 (1) |
|
|
|
See form for additional data. |
|
|
|
|
(1) The horsepower is 11.4 going to each rotor.
Spiral Bevel Gears Reduction:
Same Page ~ Different Craft:
Related Pages this Site:
Introduction Page | Uni-UAV Home Page | UniCopter Home Page | Nemesis Home Page | SynchroLite Home Page
Latest revision; August 28, 2007