[go: up one dir, main page]

Bilger et al., 1982 - Google Patents

In-flight structural dynamic characteristics of the XV-15 tilt-rotorresearch aircraft

Bilger et al., 1982

Document ID
13290397569092320321
Author
Bilger J
Marr R
Zahedi A
Publication year
Publication venue
Journal of Aircraft

External Links

Snippet

THE XV-15 tilt-rotor research aircraft was designed, built, and tested by Bell Helicopter Textron (BHT) under a joint NASA/Army/Navy Contract (NAS2-7800). Characteristic of the tilt- rotor aircraft is a 25 ft diam, three-bladed rotor mounted on each wing tip (Figs. 1 and 2). The …
Continue reading at arc.aiaa.org (other versions)

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C27/00Rotorcraft; Rotors peculiar thereto
    • B64C27/008Rotors tracking or balancing devices
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLYING SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D27/00Arrangement or mounting of power plant in aircraft; Aircraft characterised thereby
    • B64D27/02Aircraft characterised by the type or position of power plant
    • B64D27/16Aircraft characterised by the type or position of power plant of jet type
    • B64D27/18Aircraft characterised by the type or position of power plant of jet type within or attached to wing
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C27/00Rotorcraft; Rotors peculiar thereto
    • B64C27/001Vibration damping devices
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C27/00Rotorcraft; Rotors peculiar thereto
    • B64C27/006Safety devices
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C27/00Rotorcraft; Rotors peculiar thereto
    • B64C27/32Rotors
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C27/00Rotorcraft; Rotors peculiar thereto
    • B64C27/04Helicopters
    • B64C27/12Rotor drives
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00Aeronautics or air transport
    • Y02T50/60Efficient propulsion technologies
    • Y02T50/67Relevant aircraft propulsion technologies
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C13/00Control systems or transmitting systems for actuating flying-control surfaces, lift-increasing flaps, air brakes, or spoilers
    • B64C13/02Initiating means
    • B64C13/16Initiating means actuated automatically, e.g. responsive to gust detectors

Similar Documents

Publication Publication Date Title
Čečrdle Whirl flutter of turboprop aircraft structures
Kreshock et al. Comparison of comprehensive analyses predicting whirl flutter stability of the wing and rotor aeroelastic test system
Kreshock et al. Development of a new aeroelastic tiltrotor wind tunnel testbed
Wang et al. Slowed hingeless rotor wind tunnel tests and validation at high advance ratios
Tran et al. Transient and quasi-steady numerical simulations of tiltrotor conversion maneuvers
Bilger et al. Results of structural dynamic testing of the XV‐15 tilt rotor research aircraft
Kunz Analysis of proprotor whirl flutter: review and update
Piatak et al. A wind-tunnel parametric investigation of tiltrotor whirl-flutter stability boundaries
Bilger et al. In-flight structural dynamic characteristics of the XV-15 tilt-rotorresearch aircraft
Kvaternik A review of some tilt-rotor aeroelastic research at NASA-Langley
Masarati et al. Further results of soft-inplane tiltrotor aeromechanics investigation using two multibody analyses
Hathaway Active and passive techniques for tiltrotor aeroelastic stability augmentation
Houston Modeling and analysis of helicopter flight mechanics in autorotation
Corle Time-Domain Aeroelastic Stability Predictions of a Semi-Span Tiltrotor
Johnson Calculation of the aerodynamic behavior of the tilt rotor aeroacoustic model (TRAM) in the DNW
Shen et al. Aeroelastic modeling of trailing-edge-flap helicopter rotors including actuator dynamics
Miller Methods for rotor aerodynamic and dynamic analysis
Detore et al. The Stopped‐Rotor Variant of the Proprotor VTOL Aircraft
Yang et al. Sensitivity of Rotor‐Fault‐Induced Vibrations to Operational and Design Parameters
Yeager et al. Rotorcraft Aeroelastic Testing in the Langley Transonic Dynamics Tunnel
Johnson Airloads and wake geometry calculations for an isolated tiltrotor model in a wind tunnel
Geyer Jr et al. Validation and Application of a Transient Aeroelastic Analysis for Shipboard Engage/Disengage Operations.
Kreshock et al. Tiltrotor Whirl-Flutter Stability Predictions Using Comprehensive Analysis
Donham et al. Lessons learned from fixed and rotary wing dynamic and aeroelastic encounters
Schroers Dynamic Structural Aeroelastic Stability Testing of the XV-15 Tilt Rotor Research Aircraft.