|Aeronautics patents - Monitor Patents|
USPTO Class 244 | Browse by Industry: Previous - Next | All
Recent | 14: | | | Sep | Aug | Jul | Jun | May | Apr | Mar | Feb | Jan | 13: Dec | Nov | Oct | Sep | Aug | Jul | Jun | May | Apr | Mar | Feb | Jan | 12: Dec | Nov | Oct | Sep | Aug | July | June | May | April | Mar | Feb | Jan | 11: Dec | Nov | Oct | Sep | Aug | Jul | Jun | May | Apr | Mar | Feb | Jan | 10: Dec | Nov | Oct | Sep | Aug | Jul | Jun | May | Apr | Mar | Feb | Jan | | 09: Dec | Nov | Oct | Sep | Aug | Jl | Jn | May | Apr | Mar | Fb | Jn | | 2008 | 2007 |
AeronauticsBelow are recently published patent applications awaiting approval from the USPTO. Recent week's RSS XML file available below.
Listing for abstract view: USPTO application #, Title, Abstract excerpt,Patent Agent. Listing format for list view: USPTO National Class full category number, title of the patent application. 02/05/2015 > 14 patent applications in 13 patent subcategories.
20150034759 - Bidirectional control surfaces for use with high speed vehicles, and associated systems and methods: Vehicles with bidirectional control surfaces and associated systems and methods are disclosed. In a particular embodiment, a rocket can include a plurality of bidirectional control surfaces positioned toward an aft portion of the rocket. In this embodiment, the bidirectional control surfaces can be operable to control the orientation and/or flight... Agent:
20150034772 - Composite flexure for tiltrotor rotor system: According to one embodiment, a composite flexure may secure a rotor blade to a yoke in a tiltrotor rotor system. The composite flexure includes a composite body, a first end configured to couple the composite member to the yoke, and a second end configured to couple the composite member to... Agent: Bell Helicopter Textron Inc.
20150034760 - Aircraft tail rotor system: An aircraft tail rotor system is provided and includes a rotating element, a translating element and a structure including a first bearing in series with a second bearing, the first bearing including a component rotatable with and movable within the rotating element in accordance with translational movement of the translating... Agent: Sikorsky Aircraft Corporation
20150034761 - Coupling device of a motorized wheel of aircraft landing gear: An elastic device for coupling between an aircraft landing gear wheel and a coaxial motorization member for motorization of the wheel. The elastic device comprises a plurality of arms to be rotationally coupled to the motorization member adjacent a first radially inner end and which are to be linked to... Agent:
20150034771 - Device for supplying air to an auxiliary power unit of an aircraft and associated aircraft: A device for supplying air to an auxiliary power unit for aircraft, including the auxiliary power unit; a turbocharger, and a cabin, the auxiliary power unit including a diesel engine coupled to the turbocharger in such a way that: the turbocharger includes a first air inlet in a compressor of... Agent:
20150034762 - Routings for articulated landing gear: An articulated landing gear may include electrical lines and/or hydraulic lines located within the articulated landing gear. The articulated landing gear may have a hollow structural post and a hollow trailing arm coupled by a pivot joint. The electrical lines and/or hydraulic lines may be routed through an interior of... Agent: Goodrich Corporation
20150034763 - Aircraft fuselage frame element integrating tabs for the fastening of stiffeners: In order to reduce the time and the cost of manufacturing an aircraft fuselage, the subject matter disclosed herein provide an aircraft fuselage frame element comprising a core provided with at least one through-opening intended for the passing of a fuselage stiffener, and further comprising, associated with each opening, a... Agent:
20150034764 - Aircraft fuselage structure: An aircraft fuselage structure is disclosed having an outer skin, a support structure arrangement with frame elements, and a floor structure arrangement with floor support struts, the floor structure arrangement connected to the support structure arrangement via connection parts. A connection exists between the floor structure arrangement and the support... Agent:
20150034765 - Rear fuselage section of an aircraft: A rear fuselage section of an aircraft comprises at least one closed frame constructed as a unitary body, and a horizontal tail plane comprising a box-type central element and two lateral torsion boxes, said horizontal tail plane trimmable with respect to a pivot axis. The horizontal tail plane is mounted... Agent:
20150034766 - Tool for simultaneously holding several attachment clips in contact with an aircraft fuselage frame element: The subject matter disclosed herein discloses a system with attachment clips designed to fix an attachment element of an aircraft fuselage frame onto a fuselage skin and/or to stiffeners fitted onto this fuselage skin, the system also comprising tooling elements arranged alternately with the clips that they connect to each... Agent:
20150034767 - Method for regulating the de-icing of a leading edge of an aircraft and device for its implementation: A method of regulating the de-icing of a leading edge of an aircraft includes regulating the flow of air used for de-icing by at least a first regulator valve in accordance with two regulation levels, a first regulation level corresponding to the regulated position of the first regulator valve and... Agent: Airbus Operations S.a.s.
20150034768 - Aircraft fuel system and aircraft: The present invention ensures explosion-proof performance without increasing the capacity for supplying nitrogen-enriched air in an aircraft fuel system having a ventilation function. An aircraft fuel system includes: fuel tanks; an NEA supply system; a left ventilation channel extending from a ventilation duct to a fuselage and leading into the... Agent:
20150034769 - Mechanism and method for arming/disarming the actuation of an emergency slide: A mechanism for arming and disarming an actuation of an emergency slide retained on a door of an aircraft and selectively configurable between an armed configuration and a disarmed configuration. The mechanism includes at least one transport hook extending radially from the rotating shaft and rotatable therewith about the longitudinal... Agent: Bombardier Inc.
20150034770 - Vented launch vehicle adaptor for a manned spacecraft with \"pusher\" launch abort system: A system, method, and apparatus for a vented launch vehicle adaptor (LVA) for a manned spacecraft with a “pusher” launch abort system are disclosed. The disclosed LVA provides a structural interface between a commercial crew vehicle (CCV) crew module/service module (CM/SM) spacecraft and an expendable launch vehicle. The LVA provides... Agent:01/29/2015 > 13 patent applications in 12 patent subcategories.
20150028156 - Variable drag area tow system and methods: A variable drag area tow system including a tow cable, and a variable drag area device having a variable projected area, the variable drag area device is configured to have a smaller projected area as the velocity of the variable drag area device with respect to a fluid increases. A... Agent: Adaptive Methods, Inc.
20150028150 - Transformation method of hybrid transportation vehicle for ground and air, and hybrid transportation vehicle itself: Transformation method of hybrid transportation vehicle for ground and air includes the following transformation and reciprocal steps: Tilting the compensation cover (7) on. Expansion of both whole wings (1) from the transportation vehicle longitudinal position around two vertical axes (2) into the flying position. Expansion of rear parts of wings... Agent: Aeromobil, S.r.o.
20150028151 - Aerodynamically efficient lightweight vertical take-off and landing aircraft with multi-configuration wing tip mounted rotors: An aerial vehicle adapted for vertical takeoff and landing using a set of wing tip mounted thrust producing elements for takeoff and landing. An aerial vehicle which is adapted to vertical takeoff with the wings in a horizontal flight attitude then transitions to a horizontal flight path. An aerial vehicle... Agent:
20150028152 - Helicopter rotor load reduction and tip clearance control: A method of controlling a helicopter having a rotor with blades is provided. The method includes receiving, by a computing device comprising a processor, at least one input associated with the helicopter; generating, by the computing device, control signals configured to counteract blade bending associated with the rotors based on... Agent: Sikorsky Aircraft Corporation
20150028153 - Regulated three-engined power plant for a rotary wing aircraft: A power plant (1) having two engine groups (10, 20) and a main gearbox (MGB) (2), and a rotary wing aircraft (30) having such a power plant (1). Each engine group (10, 20) drives said MGB (2) mechanically to rotate a main outlet shaft (3) and, consequently, a main rotor... Agent:
20150028161 - Hydraulic passenger lifting and maneuvering device: This invention relates to a fluid driven propulsion device comprising a body arranged in a manner to facilitate flight and lift for a person, passenger or object(s) with a production of thrust from a portable or fixed power unit. A power unit is designated to move an incompressible fluid via... Agent:
20150028154 - System, method and apparatus for widespread commercialization of hydrogen as a carbon-free alternative fuel source: A system for efficiently transporting hydrogen from where it can be economically made to where it is most needed using specially designed airships. Technologies such as geothermal, wind, solar, wave tidal or hydropower can be used to generate electricity in-situ or very near to the primary energy sources. This electricity... Agent:
20150028155 - Wing adjusting mechanism: The present invention relates to a device for generating aerodynamic lift and in particular an aircraft (100) for vertical take-off and landing. A wing arrangement (110) comprises at least one propulsion unit (111), wherein the propulsion unit (111) comprises a rotating mass which is rotatable around a rotary axis (117).... Agent:
20150028162 - Method and apparatus for minimizing dynamic structural loads of an aircraft: A method of dynamically alleviating loads generated on an aircraft by a disturbance of gust and/or turbulence. The method comprises monitoring, during flight of the aircraft, to automatically detect a disturbance due to gust and/or turbulence and determining an incidence angle or angle of attack of the disturbance. When a... Agent: Eads Deutschland Gmbh
20150028157 - Cargo bay catering container with a distribution system: In a craft such as a passenger aircraft, an apparatus is provided for storing and retrieving service trolleys (110) in a craft having a passenger deck (150) and a cargo bay. The apparatus can comprise a container (101) located in the cargo bay (100) and configured to hold at least... Agent: Driessen Aerospace Group N.v.
20150028158 - Quick-disconnecting device, in particular for kite-surf: A quick-disconnecting device (1), in particular for kite-surf, comprising a fixed element (3) and a moving element (5) having an operating connecting position in which the moving element (5) is kept integral with the fixed element (3) by interposing a blocking system (7), and an operating disconnecting position in which... Agent:
20150028159 - Side-by-side dual-launch arrangement with improved payload compatibility: A side-by-side dual-launch spacecraft arrangement is provided. The arrangement may include a dual-launch adaptor, a first spacecraft, and a second spacecraft. The first spacecraft and the second spacecraft may be mounted on the dual-launch adaptor and may be arranged side by side on the dual-launch adaptor. An aspect ratio of... Agent: Lockheed Martin Corporation
20150028160 - Wingtip for a general aviation aircraft: A wingtip for extending a wing of an aircraft having a NACA 23012 airfoil. The wingtip has an airfoil design for directing and associated wingtip vortex outward and upward to thereby increase the effective wingspan of the aircraft and to reduce induced drag. The wingtip is preferably molded and comprises... Agent:01/22/2015 > 17 patent applications in 17 patent subcategories.
20150021433 - System and method for a towable and inflatable recreational device with a retractable wind foil: Our system and method for a towable and inflatable recreational device with a retractable wind foil. This towable and inflatable recreational device expands the existing field of art in the water sports recreational devices.... Agent:
20150021427 - Airship launch from a cargo airship: A method for launch of an airship includes connecting a cargo airship to a second airship that is not positively buoyant at the launch site, launching the cargo airship, transferring lifting gas from the cargo airship to the second airship where said lifting gas is carried by the cargo airship... Agent:
20150021428 - Pressure-equalizing cradle for booster rocket mounting: A launch system and method improve the launch efficiency of a booster rocket and payload. A launch aircraft atop which the booster rocket is mounted in a cradle, is flown or towed to an elevation at which the booster rocket is released. The cradle provides for reduced structural requirements for... Agent:
20150021429 - Remote-controlled aerial device platform: The invention relates to an aircraft (10) for conveying one or more recording apparatuses, such as recorders, sensors, cameras, infrared cameras, microphones or the like, through the air. For this purpose, the aircraft (10) has one or more rotors (11) which control the flight movement, as well as a holder... Agent:
20150021430 - System, apparatus and method for long endurance vertical takeoff and landing vehicle: A vertical take-off and landing (VTOL) aircraft according to an aspect of the present invention comprises a fuselage, an empennage having an all-moving horizontal stabilizer located at a tail end of the fuselage, a wing having the fuselage positioned approximately halfway between the distal ends of the wing, wherein the... Agent:
20150021431 - Method for accelerated powered self push back of an aircraft: A method for accelerated power push back of an aircraft equipped with a pilot-controlled engines-off taxi system that drives the aircraft without reliance on the aircraft's main engines or tugs is provided. An aircraft is quickly and efficiently moved out of a gate where it is positioned in a nose-in... Agent:
20150021442 - Solar relay aircraft powered by ground based solar concentrator mirrors in dual use with power towers: A solar relay aircraft system includes a solar relay aircraft having an upper surface, and a lower surface, and equipped with a solar radiation receiver on said lower surface and capable of converting solar energy to electrical energy. An electric motor in electrical connection with said solar radiation receiver to... Agent:
20150021443 - Method and apparatus for minimizing dynamic structural loads of an aircraft: A method for dynamically alleviating loads generated on an aircraft by a disturbance of gust involves automatically detecting a disturbance due to gust on a flight of the aircraft. When a disturbance due to gust is detected, control commands for control surfaces are automatically generated and the control commands are... Agent: Eads Deutschland Gmbh
20150021432 - Control box: safety actuation means (23) for causing the shaft to slide from the rest position in which anti-rotation means (27, 28) prevent the shaft from turning to the active position in which the anti-rotation means (27, 28) leave the shaft free to turn under drive from the rotary drive means (15).... Agent: Messier-bugatti-dowty
20150021434 - Self-orienting aircraft landing gear: An aircraft landing gear self-orients so to align itself within a plane parallel to the plane defined by the aircraft's roll and yaw axis. A nose gear of a tricycle landing gear configuration includes the ability to not only caster 360 degrees but also self-orient itself to be aligned parallel... Agent: Icon Aircraft, Inc.
20150021435 - Apparatus for causing an aircraft wheel to rotate: A rotator assembly for rotating an aircraft landing wheel by the action of the airstream flowing thereby has a circular plate mounted on the wheel and a plurality of independently movable cone shape connected to the outer surface of the plate in circumferentially spaced relation. Each cone shape member has... Agent:
20150021436 - Wing mount adjustment: A mounting apparatus includes a fixed mounting structure that is fixed relative to a vehicle wing, the fixed mounting structure including a first fixed fitting and a second fixed fitting. The mounting apparatus further includes a rotatable mounting structure having a swivel fitting configured to engage the first fixed fitting... Agent: Sikorsky Aircraft Corporation
20150021437 - Monobeam seat with housing receptacle: A seat-floor assembly for a vehicle comprises a floor element and at least one monobeam seat fixed to the floor element by a beam. A seat cushion and a seat backrest fixed to the beam. The floor element comprises a stiffened panel structure, one face of which forms a top... Agent:
20150021438 - Drainage mast of the compartment of an aircraft subjected to a negative pressure: A drainage mast able to drain effectively the liquid contained in the compartment of an aircraft when the pressure within the compartment is lower than the outside pressure without using any pressure control active device and without causing any significant perturbation to the aerodynamic behavior of the aircraft. The drainage... Agent:
20150021439 - Space vehicle with electric propulsion and solid propellant chemical propulsion: A space vehicle (1), in particular a satellite or a probe, capable of executing high-thrust maneuvers or high specific impulse maneuvers. According to the invention, the space vehicle (1) includes at least one solid-propellant chemical thruster (10-14) and at least one electric thruster (20-24).... Agent:
20150021440 - Debris management system and method of operation thereof: A debris management system for use in space and a method of controlling space debris is disclosed. In one embodiment, the system includes: (1) a frame, (2) a plurality of material sections, coupled to the frame, that cooperate to form a material structure when deployed from the frame and (3)... Agent:
20150021441 - Redundant current-sum feedback actuator: A system and methods for redundant current-sum feedback control of an actuator system is presented. An actuator comprises actuation coils configured to actuate the actuator, and an actuation coil current sensor senses a measured total coil current comprising a sum of coil currents of each of the actuation coils. Actuator... Agent:01/15/2015 > 13 patent applications in 11 patent subcategories.
20150014475 - Vertical takeoff and landing (vtol) air vehicle: A flight control apparatus for fixed-wing aircraft includes a first port wing and first starboard wing, a first port swash plate coupled between a first port rotor and first port electric motor, the first port electric motor coupled to the first port wing, and a first starboard swash plate coupled... Agent:
20150014476 - Flexbeam rotor attachment to rotor blade: A rotor blade assembly includes a flex-beam member and a torque tube surrounding the flex-beam member and extending partially along a rotor blade assembly length. A rotor blade surrounds the flex beam member and extends from the torque tube to a blade tip. A connecting pin assembly secures the rotor... Agent:
20150014477 - Vibration reducing apparatus: A compact vibration reducing apparatus includes a dynamic mass; elastic member which apply elastic force to the dynamic mass so that the dynamic mass vibrates in a parallel to a vibration damping direction; a control mass; an actuator which move in parallel to a length change direction; and a motion... Agent:
20150014478 - Wing fold controller: Illustrative embodiments may provide for an apparatus and method of controlling the folding of a wing. The apparatus may include a sensor, an actuator, and a wing fold controller. The method may include receiving a status of at least one of an aircraft and a wing fold system of the... Agent:
20150014479 - Independent power generation in aircraft: A method includes generating thrust at one or more engines of an aircraft. The method includes generating first electricity at a first power unit concurrently with generating second electricity at a second power unit. The first power unit and the second power unit are independent of the one or more... Agent: The Boeing Company
20150014480 - Coupling mechanism between a manual flight control member and a trim actuator of an aircraft: A coupling mechanism between a control member (1′) that generates manual flight commands and a trim actuator (4) forming part of a mechanical transmission train for transmitting flight commands in an aircraft. The coupling mechanism comprises axial engagement means between a lever arm (3) mechanically connected to the control member... Agent:
20150014481 - Rail mounted beverage dispenser for commercial airplanes: A galley cart is suspended from a rail or track that extends along the length of an aircraft cabin above the aisle and rows of passenger seats of the aircraft. The galley cart is automated to move along the track above the aisle in response to movements of a flight... Agent:
20150014482 - Unmanned aerial vehicle (uav) with inter-connecting wing sections: An unmanned aerial vehicle (UAV) is described. The UAV may include a fuselage assembly and a plurality of inter-connecting wing sections. The inter-connecting wing section may include a connecting assembly on opposing lateral ends. The connecting assembly may be complementary on opposing ends. The fuselage assembly may include a complementary... Agent:
20150014483 - Connection assembly for aircraft door: A connection assembly for an emergency aircraft door. The assembly includes a first pair of non parallel links pivotally attached to the fuselage and a second pair of non parallel links attached to the door. One of the links of the first pair is pivotally connected to both links of... Agent: Bombardier Inc.
20150014484 - Apparatus and methods for joining composite structures of aircrafts: Apparatus and method for joining composite structures of aircrafts are disclosed. An example apparatus disclosed herein includes an inboard composite wing panel having a first end portion configured to be coupled to upper and lower inboard fittings composed of a metallic material and an outboard composite wing panel having a... Agent:
20150014485 - Suspension system for carrying an external load with an aircraft, and an aircraft: A suspension system (10) of an aircraft (1). The suspension system (10) comprises a fastener device (15) including a coupling member (20) suitable for carrying a load (5) with a sling (21). The suspension system (10) has a return device (30) that comprises a linkage (40) provided with a plurality... Agent:
20150014486 - Control system and control bar for a traction wing: A control system for a traction wing includes a control bar having first and second ends. A first fixing arm is connected to each end of the bar. Each fixing arm has a fixing point for attachment of a respective wing control line. At least one of the fixing arms... Agent: Neil Pryde Limited
20150014487 - Kite control bar with integrated line adjustment means: A hollow kite control bar is provided with means for sliding access to the bar for one or multiple lines or groups of lines. Each line has one end towards the kite and the other towards the bar. The length of each line between the kite and the bar can... Agent: Ocean Rodeo Sports IncPrevious industry: Winding, tensioning, or guiding
Next industry: Wire fabrics and structure
RSS FEED for 20150205:
Integrate FreshPatents.com into your RSS reader/aggregator or website to track weekly updates.
For more info, read this article.
Thank you for viewing Aeronautics patents on the FreshPatents.com website. These are patent applications which have been filed in the United States. There are a variety ways to browse Aeronautics patent applications on our website including browsing by date, agent, inventor, and industry. If you are interested in receiving occasional emails regarding Aeronautics patents we recommend signing up for free keyword monitoring by email.
Results in 0.37037 seconds