Compressive stress system for a gas turbine engine [electronic resource]

• Ngôn ngữ: eng
• Ký hiệu phân loại: 621.4229 Prime movers and heat engineering
• Thông tin xuất bản: Oak Ridge, Tenn. : Distributed by the Office of Scientific and Technical Information, U.S. Dept. of Energy, 2015
• Mô tả vật lý: Medium: ED : , digital, PDF file.
• Bộ sưu tập: Metadata
• ID: 266995
• Chủ đề: 1. 33 advanced propulsion systems

Tóm tắt

The present application provides a compressive stress system for a gas turbine engine. The compressive stress system may include a first bucket attached to a rotor, a second bucket attached to the rotor, the first and the second buckets defining a shank pocket therebetween, and a compressive stress spring positioned within the shank pocket.