AGMA 90FTM6 PDF

AGMA 90FTM6 PDF

Name:
AGMA 90FTM6 PDF

Published Date:
10/01/1990

Status:
[ Active ]

Description:

Dynamic Responses of Aircraft Gears

Publisher:
American Gear Manufacturers Association

Document status:
Active

Format:
Electronic (PDF)

Delivery time:
10 minutes

Delivery time (for Russian version):
200 business days

SKU:

Choose Document Language:
$14.1
Need Help?

Rapid and destructive failures of high quality, high speed, lightweight and highly loaded aircraft gears are indication of the vibrational energy (associated with neutral frequency modes) exceeding the fatigue endurance limit of advance gear materials.

This paper reviews:

A) Experimental and analytical methods to identify and define resonant mode.

B) Affects of gear design and manufacturing variables to the generation and damping of vibrational energy.


Edition : 90
File Size : 1 file , 2.4 MB
Number of Pages : 21
Published : 10/01/1990

History


Related products

AGMA 2009-B01
Published Date: 01/01/2001
Bevel Gear Classification, Tolerances, and Measuring Methods
$45.6
AGMA 927- A01
Published Date: 01/01/2001
Load Distribution Factors - Analytical Methods for Cylindrical Gears
$39
AGMA 08FTM08
Published Date: 10/01/2008
PM Materials for Gear Applications
$14.1
AGMA 2000FTM6
Published Date: 10/01/2000
Did the Natural Convection Exist in Mechanical Power Transmissions? Theoretical and Experimental Results
$14.1

Best-Selling Products