Jet engine compressor blade

被引:0
作者
不详
机构
来源
AIRCRAFT ENGINEERING AND AEROSPACE TECHNOLOGY | 1999年 / 71卷 / 01期
关键词
blades; jet engines; titanium;
D O I
暂无
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
The Broaches/Carpenter partnership found a solution to broaching the root form of a jet engine compressor blade made of titanium. The unique solution, referred to as Micro-Melt T-15 alloy, is made up of several elements including carbon, sulfur, chromium, vanadium, tungsten, cobalt, and balance iron in varying concentrations.
引用
收藏
页码:48 / 49
页数:2
相关论文
共 50 条
  • [21] Research on the Performance State Assessment of Aero-Engine Compressor Driven by Realistic Digital Aero-Engine Structure Model
    Wu, Xin
    Wei, Xiaolong
    Xu, Haojun
    He, Weifeng
    Zhou, Liucheng
    Hou, Yuanhan
    Wang, Yixuan
    IEEE TRANSACTIONS ON INSTRUMENTATION AND MEASUREMENT, 2024, 73
  • [22] Reliability Analysis of Aero-Engine Compressor Rotor System Considering Cruise Characteristics
    Zhao, Bingfeng
    Xie, Liyang
    Li, Haiyang
    Zhang, Shijian
    Wang, Bowen
    Li, Chong
    IEEE TRANSACTIONS ON RELIABILITY, 2020, 69 (01) : 245 - 259
  • [23] Towards a remote inspection of jet engine blades using time reversal
    de Rosny, Julien
    Farin, Maxime
    Prada, Claire
    Lhommeau, Tony
    El Badaoui, Mohammed
    JOURNAL OF SOUND AND VIBRATION, 2022, 525
  • [24] Data and Decision Level Fusion-Based Crack Detection for Compressor Blade Using Acoustic and Vibration Signal
    Song, Di
    Ma, Tianchi
    Li, Yang
    Xu, Feiyun
    IEEE SENSORS JOURNAL, 2022, 22 (12) : 12209 - 12218
  • [25] Low cycle fatigue cracking of titanium compressor disks of aircraft engine D-30.
    Shaniavski, AA
    Losev, AI
    LOW CYCLE FATIGUE AND ELASTO-PLASTIC BEHAVIOUR OF MATERIALS, 1998, : 845 - 850
  • [26] Aero-Engine Blade Cryogenic Cooling Milling Deformation Simulation and Process Parameter Optimization
    Chen, Ting
    Xu, Yun
    Huang, Bo
    Shi, Yan
    Zhang, Jiahu
    Li, Lei
    Meng, Yaozhi
    Li, Xuqing
    MATERIALS, 2023, 16 (11)
  • [27] Useful nonlinearities and global stabilization of bifurcations in a model of jet engine surge and stall
    Krstic, M
    Fontaine, D
    Kokotovic, PV
    Paduano, JD
    IEEE TRANSACTIONS ON AUTOMATIC CONTROL, 1998, 43 (12) : 1739 - 1745
  • [28] Jet engine stationary testing in the aspect of particles emission in real operation conditions
    Jasinski, Remigiusz
    13TH INTERNATIONAL SCIENTIFIC CONFERENCE ON SUSTAINABLE, MODERN AND SAFE TRANSPORT (TRANSCOM 2019), 2019, 40 : 1388 - 1395
  • [29] A Drive with a High-Speed Pneumatic Jet Engine. Dynamics and Control
    Kreinin, G. V.
    Kosarev, A. A.
    Misiurin, S. Yu.
    Ovchinnikov, A. A.
    Saiapin, V. V.
    JOURNAL OF MACHINERY MANUFACTURE AND RELIABILITY, 2010, 39 (06): : 523 - 529
  • [30] Robust and fast algorithm for estimating fundamental periodicity of jet engine modulation signals
    Yong, Yang Woo
    Hoon, Park Ji
    Young, Song Won
    Hoon, Myung Noh
    IET RADAR SONAR AND NAVIGATION, 2016, 10 (07) : 1286 - 1294