From the Rolls-Royce experimental archive: a quarter of a million communications from Rolls-Royce, 1906 to 1960's. Documents from the Sir Henry Royce Memorial Foundation (SHRMF).
End thrust tests of hardened and white metal propeller shaft splines for the Peregrine engine.
| Identifier | ExFiles\Box 2\1\ B002_136 137-page15 | |
| Date | 24th October 1932 | |
| 8139 R.{Sir Henry Royce} from He/Ha. c. Sc. H.T. c. L. SY. c. Da.{Bernard Day - Chassis Design} HAY. He/Ha.14/KT.24.10.32. END THRUST OF PROPELLER SHAFT. K484. We have carried out tests on hardened splines and white metal splines on Peregrine. We attach curves which show the results we have obtained. It will be observed that the white metal splines running in steel are actually a disadvantage. We are not yet satisfied that we have done the best possible with the splines and are carrying out further tests. He/Ha. | ||