[go: up one dir, main page]
More Web Proxy on the site http://driver.im/

Siadkowska, 2021 - Google Patents

Smart materials technologies in composite structures of aerial vehicles

Siadkowska, 2021

Document ID
15990303181823746683
Author
Siadkowska K
Publication year
Publication venue
AIP Conference Proceedings

External Links

Snippet

The paper discusses the concepts of the solutions to improve functionality and performance of unmanned aerial vehicles. The analysis of the unmanned aerial vehicle (UAV) market was performed with particular emphasis on innovative ideas. The paper describes the …
Continue reading at pubs.aip.org (other versions)

Classifications

    • 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
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/60—Efficient propulsion technologies
    • Y02T50/67—Relevant aircraft propulsion technologies
    • Y02T50/671—Measures to reduce the propulsor weight
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLYING SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D27/00—Arrangement or mounting of power plant in aircraft; Aircraft characterised thereby
    • B64D27/02—Aircraft characterised by the type or position of power plant
    • B64D27/16—Aircraft characterised by the type or position of power plant of jet type
    • B64D27/18—Aircraft characterised by the type or position of power plant of jet type within or attached to wing
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C2201/00—Unmanned aerial vehicles; Equipment therefor
    • B64C2201/02—Unmanned aerial vehicles; Equipment therefor characterized by type of aircraft
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C27/00—Rotorcraft; Rotors peculiar thereto
    • B64C27/04—Helicopters
    • B64C27/08—Helicopters with two or more rotors
    • B64C27/10—Helicopters with two or more rotors arranged coaxially
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C2201/00—Unmanned aerial vehicles; Equipment therefor
    • B64C2201/08—Unmanned aerial vehicles; Equipment therefor characterised by the launching method
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C2201/00—Unmanned aerial vehicles; Equipment therefor
    • B64C2201/10—Unmanned aerial vehicles; Equipment therefor characterised by the lift producing means
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C39/00—Aircraft not otherwise provided for
    • B64C39/02—Aircraft not otherwise provided for characterised by special use
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C29/00—Aircraft capable of landing or taking-off vertically
    • B64C29/0008—Aircraft capable of landing or taking-off vertically having its flight directional axis horizontal when grounded
    • B64C29/0016—Aircraft capable of landing or taking-off vertically having its flight directional axis horizontal when grounded the lift during taking-off being created by free or ducted propellers or by blowers
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C27/00—Rotorcraft; Rotors peculiar thereto
    • B64C27/008—Rotors tracking or balancing devices
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C2201/00—Unmanned aerial vehicles; Equipment therefor
    • B64C2201/04—Unmanned aerial vehicles; Equipment therefor characterised by type of power plant

Similar Documents

Publication Publication Date Title
Tyan et al. Comprehensive preliminary sizing/resizing method for a fixed wing–VTOL electric UAV
He et al. Quasi-steady in-ground-effect model for single and multirotor aerial vehicles
Finger Comparative performance and benefit assessment of VTOL and CTOL UAVs
Rehan et al. Vertical take-off and landing hybrid unmanned aerial vehicles: An overview
Sridharan et al. Design Considerations of a Lift-Offset Single Main Rotor Compound Helicopter
Zhang et al. Performance evaluation and design method of lifting-wing multicopters
Konar et al. Improvement of the thrust-torque ratio of an unmanned helicopter by using the ABC algorithm
Siadkowska Smart materials technologies in composite structures of aerial vehicles
Huang et al. PSO algorithm parameter settings and optimal multi-rotor layout design
Su et al. eVTOL Performance Analysis: A Review From Control Perspectives
Aksugur et al. Design methodology of a hybrid propulsion driven electric powered miniature tailsitter unmanned aerial vehicle
Zhang et al. Conceptual Design and System Level Analysis of Tilt-Duct eVTOL Aircraft
Poggi et al. Influence of trim control strategy on noise radiated by multi-rotor systems
Wang et al. Hover performance estimation and validation of battery powered vertical takeoff and landing aircraft
Cai et al. Control and dynamics analysis for miniature autogyro and compound autogyro
Su et al. Flight performance characteristics of a modified Quadcopter with and without a wing based on flight test
Çoban Stochastic redesign of mini UAV wing for maximizing autonomous flight performance
Phung Conception, modeling, and control of a convertible mini-drone
Saeed et al. A feasibility assessment of annular winged VTOL flight vehicles
Kinkaid Study of micro-sized technology, micro air vehicles, and design of a payload carrying flapping wing micro air vehicle
Meng et al. Take-off characteristics and longitudinal controllability of FanWing
Avanzini et al. Optimal sizing of electric multirotor configurations
Aksugur et al. Hybrid propulsion system design of a vtol tailsitter UAV
Strbac et al. Concept Study of a fast VTOL-UAV Technology-Demonstrator for MUM-T
Huang et al. INFLUENCE OF OVERALL LAYOUT DESIGN OF COMPOUND MULTIROTOR VEHICLES ON FLIGHT PERFORMANCE