Matches 1 - 50 out of 51 1 2 >


Match Document Document Title
US20120312925 ELECTROMECHANICAL ACTUATOR (EMA) HEAT SINK INTEGRATED DE-ICING SYSTEM  
A de-icing system and method is disclosed. An electromechanical actuator heat sink is operable to receive heat from an electromechanical actuator, and a heat distribution element is operable to...
US20140346278 THERMAL PNEUMATIC DEICING SYSTEM FOR AN AIRCRAFT RAM AIR HEAT EXCHANGER  
A thermal pneumatic deicing system for deicing a RAM air heat exchanger includes an environmental control system (ECS) including a RAM air heat exchanger and an outlet, an electronics housing...
US20110036950 DE-ICING AND/OR ANTI-ICING SYSTEM FOR THE LEADING EDGE OF AN AIRCRAFT WING  
The invention relates to a de-icing and/or anti-icing system for the leading edge of an aircraft wing or for the lip (1) of the air intake of an aircraft engine, characterised in that it includes...
US20130181093 ANTI-ICING SYSTEM, WING, AIRCRAFT, AND ANTI-ICING METHOD  
Provided are an anti-icing system, wing, aircraft, and anti-icing method which prevent icing on the aircraft flying in an environment under icing conditions, using a simple configuration. An...
US20110297789 Aircraft De-Icing System And Method  
An aircraft de-icing system and method for removing the ice from the surface of an aircraft. The aircraft de-icing system reduces power requirements by allocating power from a single power source...
US20060226292 Dual-channel deicing system for a rotary wing aircraft  
A deicing system includes dual deice system components to provide a redundant deice system. Each redundant portion of the system generally includes a controller, an air data computer, an ice rate...
US20130228647 Rotary Wing Aircraft Propulsion System  
A rotary wing aircraft propulsion system includes an engine, a heat exchanger cooling a fluid from the engine and a thermoelectric generator in thermal communication with the fluid to generate...
US20140138490 DEICER ZONES WITH HEATER-ENHANCED BORDERS  
An ice protection system comprises deicing zones wherein each zone includes an envelope with an electrothermal heater layer Adjacent envelopes have edge regions flanking shared interzone borders....
US20080149771 System for Deicing the Leading Edge of a Nose Inlet Cowl Turbine Engine  
The invention concerns a system for deicing the leading edge of a nose inlet cowl for a turbine engine. The invention is characterized in that one of the two elements formed by the pressurized hot...
US20090294551 APPARATUS AND METHOD FOR BLENDING FLUIDS  
An apparatus and method for blending fluids and applying the blended fluid to a surface of an aircraft during deicing and anti-icing operations having a first tank, second tank, blend tank, pumps,...
US20060032983 Foreign object damage tolerant nacelle anti-icing system  
A nacelle for housing a gas turbine engine is disclosed. The nacelle comprises an inlet lip defining a leading edge of the nacelle and a conduit located within the inlet lip, the conduit having a...
US20130299638 MECHANICAL VIBRATION DEICING SYSTEM  
An aircraft deicing system including at least one motor operative to drive at least one eccentric mass in rotational motion and at least one displacer coupled to at least one location on at least...
US20110210207 MECHANICAL VIBRATION DEICING SYSTEM  
An aircraft deicing system including at least one motor operative to drive at least one eccentric mass in rotational motion and at least one displacer coupled to at least one location on at least...
US20090224104 ANTI-ICING / DE-ICING SYSTEM AND METHOD AND AIRCRAFT STRUCTURE INCORPORATING THIS SYSTEM  
The present invention provides an anti-icing/de-icing system and method using ultrasound waves for an external surface of a structure likely to be iced, such as an aircraft wing or engine nacelle,...
US20150176490 Aircraft Engine Anti-Icing (EAI) Barrier Assembly, System and Method  
There is provided an aircraft engine anti-icing (EAI) barrier assembly. The aircraft EAI barrier assembly has a slip joint subassembly having a forward end and an aft end. The forward end is...
US20140166812 Condenser Ice Removal for Environmental Control System  
Environmental control system bleed air is cooled by a heat exchanger. A fan pulls ambient air from a ram inlet duct across the at least heat exchanger and to an outlet. An air cycle machine drives...
US20070278349 Helicopter-borne power line deicer  
A deicer for removing ice or snow from a high voltage electric power transmission line suspended between opposed supports. The deicer incorporates a frame, a tether, an electric power source and a...
US20080111028 WING ICE PROTECTION HEATER ELEMENT NETWORK  
An ice prevention network comprising a plurality of non-overlapping heater elements arranged in a grid along an airfoil is provided, powered by a multiphase power source, each phase powering...
US20090294593 DEVICE FOR PROTECTION AGAINST ICING FOR AIRCRAFT ENGINES AND RELATED DE-ICING METHOD  
A device for protection against icing for aircraft engines including at least one sensor, sensitive to an amount of accumulated ice, arranged in the air intake of an aircraft engine, a system for...
US20130341465 ON BOARD INERT GAS GENERATION SYSTEM  
An on board inert gas generation system for an aircraft receives air from a relatively low pressure source such as low pressure engine bleed air or ram air and passes it to a positive displacement...
US20110049301 DE-ICER, A FIXTURE AND A METHOD OF ADJUSTING THE POSITION OF A DE-ICER  
A de-icer including a bracket arranged on a structural member and a de-icer module mounted on the bracket. The de-icer module is adjustable arranged on the bracket such that a position of the...
US20090194633 ICING PROTECTION FOR AIRCRAFT AIR INLET SCOOPS  
Aircraft air scoop icing protection systems and methods include an air duct having air inlet and outlet openings and a fairing which covers the air duct and defines an interior fairing space in...
US20120241561 METHOD AND APPARATUS FOR PROTECTING AIRCRAFT AND AIRCRAFT ENGINES AGAINST ICING  
An aircraft engine generates engine power by burning hydrocarbon fuel such as Jet-A. A minute quantity of the fuel is burned in such a manner as to generate no engine power, and the heat generated...
US20140077039 Heated Screen For Air Intake Of Aircraft Engines  
An aircraft includes a fuselage and wings mounted on opposite sides of the fuselage for sustained forward flight. An engine is mounted in the fuselage or at least one of the wings and includes an...
US20120074262 DE-ICING SYSTEM FOR A FIXED OR ROTARY AIRCRAFT WING  
A de-icing system for a fixed or rotary aircraft wing, the system including means for generating ultrasound that is transmitted at least locally to an outside surface of the wing, which means...
US20100155539 IMPROVEMENTS RELATING TO TEMPERATURE MONITORING  
A temperature monitoring arrangement for an electro-thermal ice protection system is provided for a slat of an aircraft wing, incorporating heater mats of composite material, wherein, in order to...
US20080099617 Ice Protection of Aerodynamic Surfaces  
An electrothermal heater mat for anti-icing or de-icing of a helicopter rotor blade or other aerodynamic surface comprises a substrate, such as a flexible polyimide sheet, bearing tracks of a...
US20120261512 FUEL CELL SYSTEM AND METHOD FOR DRYING OF EXHAUST GAS OF A FUEL CELL SYSTEM  
A fuel cell system having an apparatus for gas drying that includes, but is not limited to at least one cooling element with at least one first surface and at least one detachment device. The...
US20120256053 Rotor Blade De-Icing System  
An aircraft includes a heat absorbent material carried by an airfoil susceptible to ice buildup and a transmitter spaced apart from the heat absorbent material. A method includes the process of...
US20090095842 Power distribution architecture for an ice protection system  
An ice protection system for a vehicle is disclosed which includes a plurality of de-ice power distribution units positioned proximate to a leading edge surface of the vehicle that is susceptible...
US20130187007 BLEED AIR SYSTEMS FOR USE WITH AIRCRAFTS AND RELATED METHODS  
Bleed air systems for use with aircrafts and related methods are disclosed. An example apparatus includes a turbo-compressor including a compressor having a compressor inlet fluidly coupled to a...
US20150120092 ICE AND SUPERCOOLED WATER DETECTION SYSTEM  
A system for detecting ice or supercooled large droplets within an area of interest having a detection system measuring radiance or reflectance of the area of interest when exposed to shortwave...
US20100243811 ICE PROTECTION HEATER SYSTEM  
There is disclosed an ice protection system for a structure (1100), the ice protection system comprising: a plurality of independently controllable heater elements (1108, 1110, 1112) arranged on...
US20150129720 Device and Method for Deicing and/or Preventing Ice Formation and Profile Element and Aircraft Having Such a Device  
In order to maintain a surface region of an aircraft free of ice in a particularly energy-efficient manner, a device for deicing and/or for preventing ice formation is provided on an aircraft. The...
US20070040064 Method, apparatus and system for aircraft deicing and estimating deicing completion times  
The overall operating efficiency of processing objects, which are placed in a selected one of several available queues for subsequent processing at respective processing sites, is improved using a...
US20090108134 ICING PROTECTION SYSTEM AND METHOD FOR ENHANCING HEAT TRANSFER  
An icing protection system and method for enhancing heat transfer includes a substrate having an inner wall, an outer wall and a thickness separating the inner wall and the outer wall. A metallic...
US20100155538 ANTI-ICING SYSTEM AND METHOD FOR PREVENTING ICE ACCUMULATION  
An anti-icing system includes a component surface having a composite structure including a composite layer, and at least one heating element formed within the composite layer, wherein the heating...
US20130032671 METHOD AND APPARATUS FOR INHIBITING FORMATION OF AND/OR REMOVING ICE FROM AIRCRAFT COMPONENTS  
Methods and systems are generally described that inhibit debris (such as ice) accretions and/or remove debris (such as ice) accretions from the exterior surface of an aircraft. In some...
US20100102172 AIRCRAFT STRUCTURE  
A heated leading edge component for an aircraft and a method of manufacture thereof. The leading edge component includes an outer skin, a supporting rib for the outer skin, and a cavity located...
US20100123044 Aircraft Ice Protection System  
An ice protection system (40) is provided for an aircraft surface having a plurality of ice-susceptible regions. The system (40) comprises an ice protector (51-55) for each ice-susceptible region,...
US20170174365 High-Speed Airplane Deicing Installation Systems and Methods  
The present disclosure provides an airplane ground deicing installation that minimizes the impact of deicing operations on the airport during icing conditions. The installation does not require...
US20170057643 INJECTOR NOZZLE CONFIGURATION FOR SWIRL ANTI-ICING SYSTEM  
An anti-icing system for annular turbofan engine housings what include a substantially closed annular housing at a leading edge of the turbofan engine housing, the annular housing containing a...
US20170021934 ICE DETECTING APPARATUS  
An ice detecting apparatus comprising: a body including at least one ice detector mounted thereon and having an ice detecting surface and a scraping member so mounted relative to said body as to...
US20160280379 METHOD AND APPARATUS FOR INHIBITING FORMATION OF AND/OR REMOVING ICE FROM AIRCRAFT COMPONENTS  
Methods and systems are generally described that inhibit debris (such as ice) accretions and/or remove debris (such as ice) accretions from the exterior surface of an aircraft. In some...
US20160200442 ANTI-ICING SYSTEMS  
A bleed air pressure regulation system for an aircraft anti-icing system comprises a first, upstream pressure regulating valve and a second, downstream pressure regulating valve arranged in series...
US20160185457 DEVICE FOR REMOVING DEBRIS FROM AN AERODYNAMIC STRUCTURE  
A device for removing debris, such as insects and ice, from an aerodynamic structure of an aircraft and in which the aerodynamic structure has upper and lower surfaces separated by a leading edge...
US20160114895 ANTI-ICING / DE-ICING SYSTEM FOR AIRCRAFT DOOR AND AIRCRAFT DOOR EQUIPPED WITH SUCH A SYSTEM  
The invention aims to make aircraft doors easier to open by preventing ice formation or, at the very least, favoring rapid breaking of the ice on the door edges connected to the skin of the...
US20160102610 DE-ICING AND CONDITIONING DEVICE FOR AN AIRCRAFT  
The present disclosure provides a device for de-icing an air inlet lip of an aircraft nacelle. The device includes a pre-exchanger, an intake orifice of taking in low-pressure air downstream from...
US20160068272 METHOD AND A SYSTEM FOR TREATING ICE FOR AN AIRCRAFT WINDSHIELD  
A method of treating ice for a windshield of an aircraft, in which method at least two distinct de-icing zones of the windshield are defined. During a de-icing step, at least one de-icing means is...
US20160009400 ICE PROTECTION SYSTEM  
An ice-protection system suitable for use in an aircraft comprises first de-icing apparatus operable to de-ice a first zone; a first ice-detection sensor positioned in the first zone and arranged...

Matches 1 - 50 out of 51 1 2 >