Murthy, MVA and Thunga, KS and Murthy, SJK (1989) Turbo power pack - Phase I. Project Report. National Aerospace Laboratories, Bangalore.
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Abstract
A compact turbo power pack was designed for application i n underwater propulsion . The turbo power pack designed consists of a high pressure ratio supersonic partial admission impulse turbine coupled to a reduction gear box to reduce the turbine shaft speed to the level of the shaft speeds of the contrarotating propellers . The possible configurations of the turbine and gear box were studied to optimise the system and the design parameters . The report presents the details of the final configuration of the system .
| Item Type: | Proj.Doc/Technical Report (Project Report) |
|---|---|
| Uncontrolled Keywords: | Supersonic turbine, Propulsion, Reduction gear box |
| Subjects: | AERONAUTICS > Aircraft Propulsion and Power |
| Division/Department: | Propulsion Division, Propulsion Division, Propulsion Division |
| Depositing User: | Ms Indrani V |
| Date Deposited: | 09 Oct 2012 13:58 |
| Last Modified: | 09 Oct 2012 13:58 |
| URI: | http://nal-ir.nal.res.in/id/eprint/11075 |
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