[go: up one dir, main page]

Vos et al., 2007 - Google Patents

Post-buckled precompressed elements: a new class of control actuators for morphing wingUAVs

Vos et al., 2007

View PDF
Document ID
389297871518813313
Author
Vos R
Barrett R
de Breuker R
Tiso P
Publication year
Publication venue
Smart materials and structures

External Links

Snippet

This paper describes how post-buckled precompressed (PBP) piezoelectric bender actuators are employed in a deformable wing structure to manipulate its camber distribution and thereby induce roll control on a subscale UAV. By applying axial compression to …
Continue reading at repository.tudelft.nl (PDF) (other versions)

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C3/00—Wings
    • B64C3/38—Adjustment of complete wings or parts thereof
    • B64C3/44—Varying camber
    • B64C3/48—Varying camber by relatively-movable parts of wing structures
    • Y—GENERAL 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
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02E—REDUCTION OF GREENHOUSE GASES [GHG] EMISSION, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
    • Y02E10/00—Energy generation through renewable energy sources
    • Y02E10/70—Wind energy
    • Y02E10/72—Wind turbines with rotation axis in wind direction

Similar Documents

Publication Publication Date Title
Vos et al. Post-buckled precompressed elements: a new class of control actuators for morphing wingUAVs
Vos et al. Morphing wing flight control via postbuckled precompressed piezoelectric actuators
Hall et al. Development of a piezoelectric servoflap for helicopter rotor control
Lazarus et al. Static aeroelastic control using strain actuated adaptive structures
Bilgen et al. Dynamic control of a bistable wing under aerodynamic loading
Kudva et al. Overview of the DARPA/AFRL/NASA smart wing phase II program
Bilgen et al. Macro-fiber composite actuated simply supported thin airfoils
Vos et al. Mechanics of pressure-adaptive honeycomb and its application to wing morphing
Centolanza et al. Induced-shear piezoelectric actuators for rotor blade trailing edge flaps
Kudva et al. DARPA/AFRL/NASA Smart Wing program: final overview
Giurgiutiu Recent advances in smart-material rotor control actuation
Bilgen et al. Surface actuated variable-camber and variable-twist morphing wings using piezocomposites
Bernhard et al. Analysis of a bending-torsion coupled actuator for a smart rotorwith active blade tips
Suleman et al. Adaptive control of an aeroelastic flight vehicle using piezoelectric actuators
Thakkar et al. Helicopter vibration reduction in forward flight with induced-shear based piezoceramicactuation
Barrett et al. Post-buckled precompressed piezoelectric flight control actuator design, development anddemonstration
Barrett et al. Post-buckled precompressed (PBP) actuators: enhancing VTOL autonomous high speed MAVs
Chen et al. The smart morphing winglet driven by the piezoelectric Macro Fiber Composite actuator
Barrett et al. Design, construction and characterization of a flightworthy piezoelectric solid state adaptive rotor
Barrett et al. Post-buckled precompressed (PBP) elements: a new class of flight control actuators enhancing high-speed autonomous VTOL MAVs
Thiel et al. Actuation of an active Gurney flap for rotorcraft applications
Barrett et al. Design and testing of a 1/12th-scale solid state adaptive rotor
Bilgen et al. Minimum energy cross-well actuation of bistable piezocomposite unsymmetric cross-ply plates
Barrett et al. Design and testing of a subsonic all-moving adaptive flight control surface
Vos et al. Pressure adaptive honeycomb: a new adaptive structure for aerospace applications