Development and qualification of the S-76C+helicopter with 30-second/2-minute OEI power ratings

Citation
Jl. Cole et al., Development and qualification of the S-76C+helicopter with 30-second/2-minute OEI power ratings, J AMER HELI, 46(2), 2001, pp. 117-128
Categorie Soggetti
Aereospace Engineering
Journal title
JOURNAL OF THE AMERICAN HELICOPTER SOCIETY
ISSN journal
00028711 → ACNP
Volume
46
Issue
2
Year of publication
2001
Pages
117 - 128
Database
ISI
SICI code
0002-8711(200104)46:2<117:DAQOTS>2.0.ZU;2-I
Abstract
The S-76C+ is the first U.S. manufactured helicopter to be certified in acc ordance with the FAA's new 30-second/2-minute OEI power ratings, and the fi rst Sikorsky helicopter to be FAA/CAA certified to fully harmonized FAR/JAR -29 performance criteria. This paper discusses the joint Sikorsky/Turbomeca development flight test effort commencing with the shipment of Sikorsky's S-76C test aircraft to Turbomeca's CGTM flight test subsidiary at Pau, Fran ce where it was converted into a "flying test bench" for Arriel 2S1 engine development. Concurrent with Turbomeca's engine development effort, custom engine FADEC software was developed and refined, applying the lessons learn ed during previous FADEC development testing to optimize S-76C+/Arriel 2S1 engine operating characteristics. Unique engine integration and pilot train ing features were developed to accommodate the new 30-second/2-minute OEI p ower rating structure. Upon completion of development testing, the S-76C+ t est aircraft returned to Sikorsky's Development Flight Center at West Palm Beach, Florida for low altitude, warm weather qualification testing. That w as followed by cold weather testing at Fairbanks, Alaska, high altitude tes ting at Leadville, Colorado, and elevated helideck testing at a North Sea b ased oil drilling rig off the coast of Wick, Scotland.