Life and Dynamic Capacity Modeling for Aircraft Transmissions
Author : Michael Savage
Publisher : DIANE Publishing
Page : 144 pages
File Size : 31,88 MB
Release : 1991
Category :
ISBN : 1428915443
Author : Michael Savage
Publisher : DIANE Publishing
Page : 144 pages
File Size : 31,88 MB
Release : 1991
Category :
ISBN : 1428915443
Author : Michael Savage
Publisher :
Page : 138 pages
File Size : 24,30 MB
Release : 1991
Category : Airplanes
ISBN :
Author :
Publisher :
Page : 1102 pages
File Size : 47,22 MB
Release : 1991
Category : Aeronautics
ISBN :
Author :
Publisher :
Page : 58 pages
File Size : 44,83 MB
Release : 1991-03
Category : Technology
ISBN :
Author :
Publisher :
Page : 920 pages
File Size : 45,63 MB
Release : 1973
Category : Aeronautics
ISBN :
Author :
Publisher :
Page : 538 pages
File Size : 30,78 MB
Release : 1991
Category : Aeronautics
ISBN :
Author : M. Savage
Publisher :
Page : 212 pages
File Size : 27,15 MB
Release : 1986
Category :
ISBN :
A computer program which simulates life and reliability of helicopter transmissions is presented. The helicopter transmissions may be composed of spiral bevel gear units and planetary gear units - alone, in series or in parallel. The spiral bevel gear units may have either single or dual input pinions, which are identical. The planetary gear units may be stepped or unstepped and the number of planet gears carried by the planet arm may be varied. The reliability analysis used in the program is based on the Weibull distribution lives of the transmission components. The computer calculates the system lives and dynamic capacities of the transmission components and the transmission. The system life is defined as the life of the component or transmission at an output torque at which the probability of survival is 90 percent. The dynamic capacity of a component or transmission is defined as the output torque which can be applied for one million output shaft cycles for a probability of survival of 90 percent. A complete summary of the life and dynamic capacity results is produced by the program.
Author :
Publisher :
Page : 1258 pages
File Size : 24,15 MB
Release : 1991
Category : Science
ISBN :
Author : National Aeronautics and Space Adm Nasa
Publisher : Independently Published
Page : 146 pages
File Size : 38,31 MB
Release : 2018-11-18
Category : Science
ISBN : 9781731323200
A computer program to simulate the dynamic capacity and life of parallel shaft aircraft transmissions is presented. Five basic configurations can be analyzed: single mesh, compound, parallel, reverted, and single plane reductions. In execution, the program prompts the user for the data file prefix name, takes input from a ASCII file, and writes its output to a second ASCII file with the same prefix name. The input data file includes the transmission configuration, the input shaft torque and speed, and descriptions of the transmission geometry and the component gears and bearings. The program output file describes the transmission, its components, their capabilities, locations, and loads. It also lists the dynamic capability, ninety percent reliability, and mean life of each component and the transmission as a system. Here, the program, its input and output files, and the theory behind the operation of the program are described. Savage, Michael AIRCRAFT PARTS; COMPONENT RELIABILITY; COMPUTER PROGRAMS; GEARS; LIFE (DURABILITY); SHAFTS (MACHINE ELEMENTS); LOADS (FORCES); TORQUE...
Author :
Publisher :
Page : 626 pages
File Size : 37,75 MB
Release : 1990
Category : Aeronautics
ISBN :