THE DEVELOPMENT OF ADVANCED TECHNOLOGY BLADES FOR TILT-ROTOR AIRCRAFT

被引：0
|
作者：
ALEXANDER, HR
MAISEL, MD
GIULIANETTI, DJ
机构：
[1] Boeing Vertol Co, Philadelphia, PA,, USA, Boeing Vertol Co, Philadelphia, PA, USA
来源：
VERTICA | 1986年 / 10卷 / 3-4期
关键词：
HELICOPTERS; -; Rotors;
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 paper discusses the development and ground testing of blades for the XV-15 tilt-rotor demonstrator aircraft. These blades, known as the Advanced Technology Blades (ATB), replace the rectangular, steel blades which were part of the XV-15 original design. The materials used in the primary structure of the ATB are fiberglass and high strain graphite epoxy laminates. This facilitates the use of 43 deg of non-linear twist, a nonuniform tapered planform and thin airfoils required for aerodynamic efficiency. Instrumentation life is extended by encapsulating gages and wiring in the composite structure. Hover testing has demonstrated performance significantly superior to that predicted by contemporary methodology.
引用
收藏
页码：315 / 339
页数：25
相关论文
共 50 条
  • [1] Modeling and Control of Tilt-rotor Aircraft
    Lu Ke
    Liu Chunsheng
    Wang Zhengzhong
    Wang Weihong
    PROCEEDINGS OF THE 28TH CHINESE CONTROL AND DECISION CONFERENCE (2016 CCDC), 2016, : 550 - 553
  • [2] Modeling and Simulation of Rotor Dynamics of a Tilt-rotor Aircraft
    Sasongko, R. A.
    Muhammad, B.
    PROCEEDINGS OF 2017 5TH INTERNATIONAL CONFERENCE ON INSTRUMENTATION, COMMUNICATIONS, INFORMATION TECHNOLOGY, AND BIOMEDICAL ENGINEERING (ICICI-BME): SCIENCE AND TECHNOLOGY FOR A BETTER LIFE, 2017, : 51 - 56
  • [3] Mathematical modeling and control of a tilt-rotor aircraft
    Wang, Xinhua
    Cai, Lilong
    AEROSPACE SCIENCE AND TECHNOLOGY, 2015, 47 : 473 - 492
  • [4] The investigation on flight quality of tilt-rotor aircraft
    Lu, Ke
    Zhao, Shanyong
    Ma, Yujie
    Wu, Shangjing
    da Su, Cheng
    AIRCRAFT ENGINEERING AND AEROSPACE TECHNOLOGY, 2021, 93 (10): : 1582 - 1590
  • [5] STABILITY STUDY OF A TILT-ROTOR AIRCRAFT MODEL
    COSTES, JJ
    NICOLAS, J
    PETOT, D
    RECHERCHE AEROSPATIALE, 1982, (06): : 413 - 440
  • [6] Tilt-rotor technology takes off
    Snyder, WJ
    Zuk, J
    Marks, H
    AEROSPACE AMERICA, 1997, 35 (04) : 20 - 22
  • [7] ANALYSIS OF THE WING ROTOR AND ROTOR ROTOR INTERACTIONS PRESENT IN TILT-ROTOR AIRCRAFT
    CLARK, DR
    VERTICA, 1987, 11 (04): : 731 - 749
  • [8] MPC Flight Control for a Tilt-Rotor VTOL Aircraft
    Bauersfeld, Leonard
    Spannagl, Lukas
    Ducard, Guillaume J. J.
    Onder, Christopher H.
    IEEE TRANSACTIONS ON AEROSPACE AND ELECTRONIC SYSTEMS, 2021, 57 (04) : 2395 - 2409
  • [9] Formulation of a comprehensive aeroelastic analysis for tilt-rotor aircraft
    Univ of Maryland, College Park, United States
    J Aircr, 2 (280-287):
  • [10] End game in sight for Osprey tilt-rotor aircraft
    Koch, Andrew
    Jane's Defence Weekly, 2005, (JAN.):
12345