Accession Number:

AD0849841

Title:

Reviews of Rolls-Royce Small Engine Division and RR 360-07 Two Spool Gas Turbine,

Descriptive Note:

Corporate Author:

OFFICE OF NAVAL RESEARCH LONDON (UNITED KINGDOM)

Personal Author(s):

Report Date:

1969-03-24

Pagination or Media Count:

19.0

Abstract:

The 360-07 turboshaft gas turbine engine is being developed. Two 360 engines will be used to power the WG-13 helicopter for use by the British and French Armed Forces. The engine incorporates a two spool gas generator axial LP and centrifugal HP compressors, a two stage free power turbine, short shafts, modular construction, a compact reduction gear unit, wide performance characteristics and no variable geometry. The engine has a guaranteed SFC of 0.62 lbshphr at 415 shp at sea level ISA without installation losses. Max power is 830 shp contingency rating 900 shp, overall pressure ratio is 12.151, design point SFC is 0.479 lbshphr, mass flow is 7.21 lb airsec, dry weight is 300 lb, length 41 in, height 22 in, and width 22 in. Author

Subject Categories:

  • Jet and Gas Turbine Engines

Distribution Statement:

APPROVED FOR PUBLIC RELEASE