| contributor author | Ernest K. Gatcombe | |
| contributor author | Roy W. Prowell | |
| date accessioned | 2017-05-09T00:07:33Z | |
| date available | 2017-05-09T00:07:33Z | |
| date copyright | August, 1960 | |
| date issued | 1960 | |
| identifier issn | 1087-1357 | |
| identifier other | JMSEFK-27438#223_1.pdf | |
| identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/126833 | |
| description abstract | In this paper a rocket motor turbine-pump reduction gear system is analyzed in regard to Hertzian gear tooth contact stresses and times of contact. It is found that the Hertzian contact stresses vary from approximately 100,000 psi to 200,000 psi. The times of contact vary from three to eight microsec. Some observations regarding the correlation between contact times and gear failures are made. It is indicated that it may be possible to establish design limitations on the contact times to insure satisfactory gear operation. Sample calculations for evaluating each of the typical quantities found in the tables are included. | |
| publisher | The American Society of Mechanical Engineers (ASME) | |
| title | Rocket Motor Gear Tooth Analysis (Hertzian Contact Stresses and Times) | |
| type | Journal Paper | |
| journal volume | 82 | |
| journal issue | 3 | |
| journal title | Journal of Manufacturing Science and Engineering | |
| identifier doi | 10.1115/1.3663048 | |
| journal fristpage | 223 | |
| journal lastpage | 229 | |
| identifier eissn | 1528-8935 | |
| keywords | Engines | |
| keywords | Stress | |
| keywords | Gear teeth | |
| keywords | Rockets | |
| keywords | Gears | |
| keywords | Pumps | |
| keywords | Turbines | |
| keywords | Failure AND Design | |
| tree | Journal of Manufacturing Science and Engineering:;1960:;volume( 082 ):;issue: 003 | |
| contenttype | Fulltext | |
