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

Strobl et al., 2015 - Google Patents

Feasibility study of a hybrid ice protection system

Strobl et al., 2015

Document ID
14426857878821355537
Author
Strobl T
Storm S
Thompson D
Hornung M
Thielecke F
Publication year
Publication venue
Journal of Aircraft

External Links

Snippet

A key design factor impacting the use of electrical power to drive aircraft systems and subsystems is energy efficiency. With the design of an all-electric, hybrid ice protection system, energy consumption can be reduced to a large extent. The hybridization is achieved …
Continue reading at arc.aiaa.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
    • Y02T50/672—Measures to reduce the propulsor weight using composites
    • 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
    • Y02T50/40—Weight reduction
    • Y02T50/42—Airframe
    • Y02T50/43—Materials
    • Y02T50/433—Composites
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces and the like
    • B64C1/06—Frames; Stringers; Longerons; Fuselage sections
    • B64C1/12—Construction or attachment of skin panels
    • 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
    • B64D15/00—De-icing or preventing icing on exterior surfaces of aircraft
    • B64D15/12—De-icing or preventing icing on exterior surfaces of aircraft by electric heating
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces and the like
    • B64C1/40—Sound or heat insulation, e.g. using insulation blankets

Similar Documents

Publication Publication Date Title
Strobl et al. Feasibility study of a hybrid ice protection system
Zhou et al. Utilization of thermal effect induced by plasma generation for aircraft icing mitigation
Yin et al. Numerical simulation and experimental validation of ultrasonic de-icing system for wind turbine blade
Palacios et al. Ultrasonic de-icing of wind-tunnel impact icing
Myers Extension to the Messinger model for aircraft icing
Liu et al. An experimental study on the thermal effects of duty-cycled plasma actuation pertinent to aircraft icing mitigation
Beaugendre et al. FENSAP-ICE's three-dimensional in-flight ice accretion module: ICE3D
Budinger et al. Ultrasonic ice protection systems: analytical and numerical models for architecture tradeoff
Overmeyer et al. Ultrasonic de-icing bondline design and rotor ice testing
Budinger et al. Electromechanical resonant ice protection systems: analysis of fracture propagation mechanisms
Shi et al. Multimodal shear wave deicing using fibre piezoelectric actuator on composite for aircraft wings
Qiang et al. Research progress on construction strategy and technical evaluation of aircraft icing accretion protection system
Sommerwerk et al. Numerical simulation and validation of electro-impulse de-icing on a leading edge structure
Strobl et al. Development of a hybrid ice protection system based on nanostructured hydrophobic surfaces
Palacios et al. Ultrasonic shear wave anti-icing system for helicopter rotor blades
Rodrigues et al. Recent developments on dielectric barrier discharge (DBD) plasma actuators for icing mitigation
Palacios Design, fabrication, and testing of an ultrasonic de-icing system for helicopter rotor blades
Palanque et al. Piezoelectric resonant ice protection systems–Part 1/2: Prediction of power requirement for de-icing a NACA 0024 leading edge
Yang et al. Novel hybrid ice protection system combining thermoelectric system and synthetic jet actuator
Palanque et al. Piezoelectric resonant ice protection systems-Part2/2: benefits at aircraft level
Palacios et al. Ultrasonic shear and lamb wave interface stress for helicopter rotor de-icing purposes
Strobl et al. Synergic effects of passive and active ice protection systems
Strobl et al. Feasibility study of a hybrid ice protection system based on passive removal of residual ice
Gastaldo et al. Full instantaneous de-icing using extensional modes: The role of architectured and multilayered materials in modes decoupling
Maio et al. Development of a de-icing system for aerodynamic surfaces based on ultrasonic waves