Research and Development of the FJR710 Turbofan Engine
Date Published: 1974-02-01
Paper Number:740809
DOI: 10.4271/740809
Citation:
Matsuki, M., Torisaki, T., Miyazawa, K., and Itoh, M., "Research and Development of the FJR710 Turbofan Engine," SAE Technical Paper 740809, 1974, doi:10.4271/740809.
Author(s):
Masakatsu Matsuki - National Aerospace Lab.
Tadao Torisaki - National Aerospace Lab.
Kiyoto Miyazawa - Ishikawajima-Harima Heavy Industries Co., Ltd.
Mototsugu Itoh - Ishikawajima-Harima Heavy Industries Co., Ltd.
Abstract:
Research and development of high bypass ratio turbofan engines have been conducted in Japan since 1971. Three prototype engines have been built and tested and have met design specifications. The project is conducted under the National Research and Development Program of the Japanese Government. The engineering background of the project's initiation is reviewed. The purpose and management of the system are discussed. The objectives and master schedule as well as engine specifications and design features of the engine are presented. The state of development of the engine, including performance data and problems encountered, are reviewed.
File Size: 3544K
Product Status: In Stock
Purchase more technical papers and save! With TechSelect,
you decide what SAE Technical Papers you need, when you need them, and how much you want to pay.
Learn more >
