Accession Number:

AD0602565

Title:

CERTAIN PROBLEMS OF THE JET DRIVE OF A HELICOPTER ROTOR BY MEANS OF A TURBOJET ENGINE ATTACHED TO THE BLADES,

Descriptive Note:

Corporate Author:

FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OHIO

Personal Author(s):

Report Date:

1964-03-30

Pagination or Media Count:

30.0

Abstract:

The creation of a turbojet engine suitable for work on rotor blades requires the effectuation of various experimental and design investigations. The following are the main problems Ensuring efficiency of bearings and heat dissipation from oil under the conditions of large radial loads and balancing the gyroscopic moment created by the engine rotor revolving together with the rotor blade. Author

Subject Categories:

Distribution Statement:

APPROVED FOR PUBLIC RELEASE