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Matches 1 - 50 out of 1,012

Document Document Title
WO/2019/070688A1
An object has at least a first source of light secured thereto. At least a first light-bearing conduit operably couples to this source of light and also to at least a first heat-dispersion component that is also secured to the object. So...  
WO/2019/058109A1
In a method of manufacturing an electrothermal heater mat (3), there is provided a preform (7) which comprises a laminated stack of dielectric layers (51-56) which are made of thermoplastic material and include a central layer or group o...  
WO/2019/056030A1
The invention relates to a device (1) for simulating accretions, more particularly for simulating ice accretions on a surface for example, of an airplane (11) or an airplane part, said device comprising a contoured outer surface (7) for ...  
WO/2019/048772A1
The invention relates to a method for manufacturing a cellular core (34) for an acoustic panel (30), the cellular core (34) comprising at least one plurality of acoustic cells (36) and a plurality of de-icing channels (48) that extend lo...  
WO/2019/045849A1
A conductor in composite is disclosed. In various embodiments, an electrically conductive structure, such as an electrically conductive metal, is sandwiched between insulating material and two or more layers of fiber reinforced composite...  
WO/2019/043686A1
A coating applied to a surface to minimize or prevent the ability of drops of super-cooled water that impact on the surface from transforming into ice, comprises one or more layers collectively providing: a) thermal insulation between th...  
WO/2019/036803A1
Apparatus and methods for providing air to pneumatic loads such as an environmental control system for a passenger cabin of an aircraft or an ice protection device of the aircraft are disclosed. In one embodiment, the apparatus comprises...  
WO/2019/034821A1
The present invention relates to equipment for physically and thermochemically characterising a fog of droplets of dimensions comprised between 1 and 500 µm, in a zone of measurement and comparison with a reference profile comprising il...  
WO/2019/026066A1
A number of devices are provided for detecting presence of ice in an airstream. In some examples such device includes a housing defining a first chamber and a second chamber, and a partition wall separating the first chamber and the seco...  
WO/2019/002919A1
Systems and methods to facilitate a steep final approach phase of flight of an aircraft are disclosed. In one embodiment, a method for operating an aircraft during a steep approach phase of flight of the aircraft comprises operating an e...  
WO/2018/224440A1
Ice protection systems of aircraft and related methods are disclosed. In one embodiment, the system comprises a gas-discharge lamp configured to emit infrared radiation toward an inner surface of an aircraft skin and an electric power so...  
WO/2018/220370A1
We describe an ice protection system used for removing ice and/or other accretions from a structure. An actuator, coupled to a structure, is driven to generate vibrations in the structure. A controller drives the actuator using a signal ...  
WO/2018/220268A1
The invention relates to a measurement system (100) for establishing a forecast for structural icing of a mechanical structure. The measurement comprises a digital in-line holography apparatus (1) comprising a monochromatic light source ...  
WO/2018/204942A1
The invention relates to a rotor, in particular for aircraft and wind turbines, comprising a driven, rotatably mounted rotor head and rotor blades protruding from same and having a profiled cross-section, wherein a device (3) for mechani...  
WO/2018/197120A1
An aerodynamic body for use on an aircraft is presented. The aerodynamic body includes at least a first perforated surface portion (25) and an ice-protection system (31). The first perforated surface portion (25) has perforations, the ic...  
WO/2018/191523A1
Embodiments, described herein relate generally to devices, systems, and methods for producing lubricious surfaces with enhanced durability and which increase the ease of communication of viscous liquids across the same. The system can in...  
WO/2018/189341A1
An electrothermal heater (2) for an ice protection system includes a laminated heater mat (3) which comprises a primary heater element layer (36), a secondary heater element layer (37), and at least one dielectric layer (34) interposed b...  
WO/2018/169066A1
Provided are a method for manufacturing a resin sheet 10 capable of substantially transmitting heat, the resin sheet 10, a method for manufacturing a structural body using the resin sheet 10, the structural body, and an airframe of an ai...  
WO/2018/158766A1
An airborne vehicle made of thermally non-conductive materials and method for thermal conduction in an airborne vehicle are disclosed. The airborne vehicle comprising at least one structural element made of material with high thermal con...  
WO/2018/143860A1
The invention relates to a method for the application of heating mats (10) on a wing/blade of a wind power station or other devices for the purpose of achieving deicing also during operation when necessary. Temperature measurement and de...  
WO/2018/122373A1
There is disclosed a rotor (3, 3', 3", 3"') for an aircraft (1) capable of hovering, comprising a stationary support structure (10); a rotative element (11), which is rotatable about an axis (A) with respect to stationary support structu...  
WO/2018/060830A1
The present invention relates to a system for ice detection/prevention and flow control based on the impression of sliding plasma actuators with dielectric discharge barrier. This invention has advantages such as: reduced weight, low mai...  
WO/2018/060830A4
The present invention relates to a system for ice detection/prevention and flow control based on the impression of sliding plasma actuators with dielectric discharge barrier. This invention has advantages such as: reduced weight, low mai...  
WO/2018/060579A1
The invention relates to an aircraft electrical network comprising an electrical device (28, 29) for protecting an outer surface of the aircraft from frost, which is suitable for being able to be supplied with power by a shared electrica...  
WO/2018/060808A1
An aircraft (A) comprising at least a component part (1, 2, 3, 4, 5, 6, 7, 8) provided with thermal de-icing means (S) suitable to eliminate and/or prevent the formation of ice on said component part, said de-icing means (S) are directly...  
WO/2018/051152A1
Trailer-tops and aircraft are overlaid with carbon fiber chops in a felt-like structure, encased by electrodes at a constant distance or according to the density of carbon fiber layup.  
WO/2018/048615A1
An apparatus and method for deicing a surface (66) upon which ice accumulates, on for example an aircraft wing. The apparatus and method for the deicing module include an actuating component, a casing (28), and a movable member (36). The...  
WO/2018/037022A1
Disclosed herein is a method for determining if icing has occurred on a surface of an aircraft, the method comprising: heating a surface of an aircraft; after the heating has stopped, measuring the temperature of the surface as it cools;...  
WO/2018/004423A1
Disclosed is an aqueous deicing and/or anti-icing composition, and the use thereof on areas in need of deicing and/or anti-icing, exhibiting substantially improved corrosion inhibition, conductivity inhibition and/or hydrogen embrittleme...  
WO/2018/005529A1
A temperature monitoring unit may be removably installed inside an aircraft wing structure for monitoring temperature conditions along the span of the wing. The wing structure has a temperature-sensitive device (162) for monitoring a tem...  
WO/2018/002855A1
Apparatus and method for conditioning engine-heated air onboard an aircraft including a heat exchanger (140) at least partially disposed in a pylon structure (118) for supporting an engine (134) of the aircraft. The pylon heat exchanger ...  
WO/2017/196870A1
Methods and systems for providing self-lubricating icephobic elastomer coatings (SLICs) can include forming the coatings from a three-component composition of a silicon elastomer, silicone oil, and a solvent, such as xylene. The coatings...  
WO/2017/187073A1
The invention concerns an aircraft propulsion system comprising at least one member (1, 3, 4, 8) in contact with a turbulent flow of a stream (F), characterised in that said member is covered, at least partially, by a piezoelectric struc...  
WO/2017/180392A1
The modular aircraft system includes a single fuselage (10) having a permanently installed empennage (12) and plural sets of wing modules (46a, 46b, 66a, 66b, 68a, 68b) and engine modules (56, 60, 64), with each wing and engine module op...  
WO/2017/162862A1
The invention concerns an aircraft probe for resisting formation and propagation of ice comprising: • a base that is intended to be attached to an aircraft; • a housing extending from the base, said housing comprising:  a body ext...  
WO/2017/161920A1
An aircraft wing provided with a nanolayer having a spontaneous condensate drop propelling function, comprising an aircraft wing body made of a titanium material. The titanium material is prepared in a manner described below: a cathode a...  
WO/2017/143032A1
Apparatuses for and methods of deicing aircraft surfaces, engine inlets, windmill blades and other structures are disclosed. Deicing apparatuses comprising at least one standoff coupled with an actuator and a first region of an inner sur...  
WO/2017/137740A1
The invention concerns a noise attenuation panel comprising a sound absorbing honeycomb layer disposed between a perforated surface layer on an airflow facing side of the panel and a composite support layer on a second opposing side of s...  
WO/2017/138846A1
The proposed utility model relates to warning and monitoring means and may be used for remotely detecting ice formation and for determining environmental conditions similar to those in which ice forms or is predisposed to forming on vari...  
WO/2017/129536A1
The invention relates to an aircraft wing. The wing comprises a movable flap which is able to move in rotation relative to a fixed central body, flexible piping (40) and a rail (30) for guiding the movable flap and the flexible piping (4...  
WO/2017/103374A1
The invention relates to a defrosting device comprising an actuator (110) having a stationary portion (112) and a movable portion (114) designed to alternately move away from and move towards the stationary portion (112), and an intermed...  
WO/2017/055765A1
The invention relates to a device (10) for de-icing an air intake lip (12) of an aircraft turbojet engine nacelle (14), the device (10) comprising a de-icing circuit in which a heat transfer fluid (22) circulates, said heat transfer flui...  
WO/2017/055766A1
The invention relates to a device (10) for de-icing an air intake lip (12) of an aircraft turbojet engine nacelle (14), the device (10) comprising a de-icing circuit in which a heat transfer fluid (22) circulates, said heat transfer flui...  
WO/2017/032803A1
The invention relates to a heating system for electrothermal temperature control, having at least one areal heating element which is composed of a fibre composite material, wherein a current flow through the electrically conductive reinf...  
WO/2017/031397A1
The invention relates generally to gas turbine engines used for electrical power generation. More specifically, embodiments of the present invention provide ways for improving gas turbine engine performance by reducing ice build-up on th...  
WO/2017/023559A1
An anti-ice valve, a turbine engine including an anti-ice valve assembly and a method of operating an anti-ice valve where an anti-ice valve has a housing and a valve element configured to control a flow of hot bleed air through the hous...  
WO/2017/019165A1
A transparency, e.g. an aircraft laminated windshield, includes one or more moisture sensors (85, 87) to monitor moisture penetration to monitor performance of the moisture barrier (36). At least one of the moisture sensors (85, 87) incl...  
WO/2017/005737A1
The invention relates to a system for dual management of anti-icing and boundary layer suction for an aerofoil (4) of an aircraft, including: at least one anti-icing channel (44) and at least one suction channel (46); a device (26) for m...  
WO/2016/201417A1
An aircraft de-icing system has a nozzle with at least one movable element configured to move between a first position and a second position to change a spraying configuration of the nozzle between a first configuration and a second conf...  
WO/2016/191118A1
Thermally stable microstructured layers comprising polyurethane, polyurea and/or polyurethane/urea semi-IPN materials are provided which have microstructured surfaces which are highly durable, erosion resistant, and thermally stable. The...  

Matches 1 - 50 out of 1,012