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Patent # Description
2017/0297723 SEAT RAIL COVER FOR COVERING A SEAT RAIL IN A VEHICLE FLOOR AND METHOD FOR MANUFACTURING A SEAT RAIL COVER
A seat rail cover includes a retaining section, configured to be introduced at least partially into a part of the seat rail, and a cover section, configured to...
2017/0297722 ARMREST FOR AIRCRAFT SEAT, ASSOCIATED SEAT AND PROCESS
Armrest for aircraft seat, associated seat and process are provided. The armrest includes a stationary part (12) intended to be connected to the seat, a moving...
2017/0297721 ROTATIONAL BRAKE ASSEMBLY FOR A SEAT LOCKING MECHANISM
A rotational brake assembly comprises: a swivel disc having an outer diameter and a plurality of locking holes proximate the outer diameter; a cam having an...
2017/0297720 OVERRIDE BYPASS ASSEMBLY FOR A SEAT LOCKING MECHANISM
An override bypass assembly comprises a cable and a pulley wheel operably connected to the cable. The cable in operation rotates the pulley wheel when tension...
2017/0297719 PAIRED HERRINGBONE HIGH DENSITY BUSINESS CLASS SEATING ARRANGEMENT
Described are seating arrangements having at least one set of columns that include an aisle column of seating units positioned adjacent a wall column of...
2017/0297718 INTEGRATED SINK AND DISPOSAL UNIT
Embodiments of the present invention provide systems and methods for disposal of liquid and food into a sink basin. The disclosed system cooperates with and...
2017/0297717 CONVERTIBLE CHILLED STOWAGE COMPARTMENT IN AN AIRCRAFT
An aircraft includes a cabin wall defining a cabin and a convertible monument in the cabin adjacent the cabin wall. The convertible monument has a plurality of...
2017/0297716 CONDENSATE REMOVAL SYSTEM OF AN AIRCRAFT COOLING SYSTEM
An aircraft includes a cooling compartment and an evaporative chiller configured to cool the cooling compartment. The evaporative chiller includes a...
2017/0297715 TOILET SYSTEM AND METHOD OF ASSEMBLING
A toilet system that includes a waste receptacle including an outlet configured to channel waste therethrough. The system also includes a conveyor assembly...
2017/0297714 AIRCRAFT CEILING LINER ELEMENT WITH A CARRIER PLATFORM
An aircraft ceiling liner element comprises a load-bearing carrier platform, configured to form a part of an aircraft ceiling liner, and a mounting mounted on...
2017/0297713 Vehicle Body and Method for Assembling a Vehicle Body
A vehicle body includes a primary vehicle structure and interior vehicle fittings as well as a coupling device for fastening the interior vehicle fittings to...
2017/0297712 SMALL UAVS WITH RADAR RECEIVERS TO BE USED AS BISTATIC RADAR LAUNCHED FROM TACTICAL FIGHTER JETS
A system for bistatic radar target detection employs an unmanned aerial vehicle (UAV) having a radar antenna for bistatic reception of reflected radar pulses....
2017/0297711 UAV CAPTURE OF MICRO CARGO ALOFT
A system of transporting micro-cargo incorporates an unmanned aerial vehicle (UAV) having a tether capture device. A tether is connected to and suspends a...
2017/0297710 METHOD AND APPARATUS FOR ARTIFICIAL DISTRIBUTION OF INSECTS OR SPRAY
A diffuser for distributing spray or insects from an aircraft is mounted on an aircraft and comprises a distribution tube connected to an insect source at a...
2017/0297709 MULTI- MODULAR AERIAL FIREFIGHTING CONTROL METHOD AND APPARATUS
A multi-modular aerial firefighting control method and apparatus for use by firefighters to control fire. The multi-modular aerial firefighting control method...
2017/0297708 Methods for improvements of the box wing aircraft concept and corresponding aircraft configuration
Aircraft configuration by applying the following method steps for improving the conventional box wing aircraft concept: dividing both the backward swept front...
2017/0297707 UNMANNED AIRCRAFT SYSTEM (UAS) WITH ACTIVE ENERGY HARVESTING AND POWER MANAGEMENT
A method of harvesting and managing energy from air currents, by small unmanned aircraft systems (UAS) having a plurality of powered and unpowered rotors, to...
2017/0297706 HAND-LAUNCHED UNMANNED AERIAL VEHICLE
The invention discloses a hand-launched unmanned aerial vehicle, and belongs to the technical field of unmanned aerial vehicles. The hand-launched unmanned...
2017/0297705 Multi-Rotor Aircraft Control
Flight control method and apparatus for multi-rotor aircraft that is programmed for varied control commands and conditions in the control of the aircraft in...
2017/0297704 Remote Controlled Aircraft
A remote controlled aircraft includes an aircraft that may be flown. A plurality of light emitters is coupled to the aircraft. A plurality of fans is coupled...
2017/0297703 ELECTRONIC SPEED CONTROLLER ARM FOR VEHICLE
According to various embodiments, an unmanned aerial vehicle (UAV) is provided. The UAV may include a motor controller. The UAV may further include a motor...
2017/0297702 VIBRATION CONTROL METHOD FOR FLAPPING-WING MICRO AIR VEHICLES
The present invention provides a method for controlling the oscillation of flapping-wing air vehicle, which comprises the following steps: calculating the...
2017/0297701 KITE WITH CONTROLLABLE TRAILING EDGE
A kite comprises: a wing; upper and lower flaps located along at least a portion of an edge of the wing that forms the trailing edge of the wing when the wing...
2017/0297700 VERTICAL TAKE OFF AIRCRAFT
An aircraft includes a fuselage, a wing, a ducted fan and a controller. The wing and the ducted fan are coupled to the fuselage. The controller is operable to...
2017/0297699 QUAD ROTOR TAIL-SITTER AIRCRAFT WITH ROTOR BLOWN WING (RBW) CONFIGURATION
A tail-sitter aircraft is provided and includes a fuselage having first and second axisymmetric sides, first collectively controllable prop-rotors, which are...
2017/0297698 TILTWING AIRCRAFT
An aircraft includes a fuselage defining an aircraft attitude axis. The fuselage houses an engine fixed relative to the aircraft attitude axis. A rotor...
2017/0297697 ROTORCRAFT CONFIGURATION AND METHOD OF ROTORCRAFT DESIGN
A rotorcraft is provided and includes a fuselage. The fuselage includes drag generating portions, a main rotor assembly and an auxiliary propulsor having an...
2017/0297696 AIRCRAFT MAIN ROTOR DRAG TO AIRFRAME DRAG
An aircraft includes an airframe having an extending tail and a counter rotating, coaxial main rotor assembly disposed at the airframe including an upper rotor...
2017/0297695 SYSTEM AND METHOD FOR ASSISTING IN ROTOR SPEED CONTROL
A method of assisting in rotor speed control in a rotorcraft can include measuring a rotor speed with a sensor; detecting a droop in the rotor speed beyond a...
2017/0297694 ROTOR SPEED MANAGEMENT
A flight control system for a rotorcraft includes a controller configured to receive input indicative of ambient conditions, determine a threshold rotor blade...
2017/0297693 FEED-FORWARD COMPENSATION FOR GYROSCOPIC LOADS IN A COAXIAL ROTOR
A system and method for counteracting a rotor moment of one or more rotors of a coaxial rotor helicopter includes receiving signals with a processor indicative...
2017/0297692 ROTARY WING AIRCRAFT
A rotary wing aircraft includes an airframe, one or more engines supported by the airframe, and a plurality of rotor blades operatively connected to the one or...
2017/0297691 CYLINDRICAL ELASTOMERIC BEARING WITH TAPERED SHIMS
A cylindrical elastomeric bearing including a plurality of elastomeric layers arranged about a central bore. The elastomeric layers are characterized by a...
2017/0297690 HUB SEPARATION IN DUAL ROTOR ROTARY WING AIRCRAFT
An aircraft includes an airframe; an extending tail; a counter rotating, coaxial main rotor assembly including an upper rotor assembly and a lower rotor...
2017/0297689 ELECTRIC PROPULSION SYSTEM FOR A ROTARY WING AIRCRAFT
A rotary wing aircraft includes an airframe, a stationary mast fixedly engaged to the airframe and extending along a first axis, and an electric motor. The...
2017/0297688 INTEGRATED MAIN ROTOR HUB AND SHAFT
A main rotor system for a rotary wing aircraft is provided including a lower rotor hub to which lower rotor blades are attachable. The lower rotor hub rotates...
2017/0297687 Tandem Rigid Rotor System and Method
A tandem rigid rotor system has a first rigid rotor system and a second rigid rotor system connected by a fuselage. The fuselage has at least one framing...
2017/0297686 ANTI-VIBRATION MOMENT GENERATING AIRCRAFT ACTUATION SYSTEM
An aircraft is provided and includes an airframe, an engine, a drive portion driven by the engine, a rotor apparatus, which includes a rotor rotatable relative...
2017/0297685 Rotor Hub Vibration Attenuator
A vibration attenuator for an aircraft has at least one weight mounted in a rotating system of a rotor hub of the aircraft, each weight being rotatable about...
2017/0297684 ACTIVE LANDING GEAR DAMPER
An active landing gear damping system and method for decelerating a vehicle during a terrain impact event, such as an aircraft landing or crash. The system...
2017/0297683 NOSE GEAR STEERING APPARATUS FOR SHIPBOARD OPERATIONS
A steering assembly includes a movable anchor. Movement of the anchor in a first direction is restricted. A first linkage is coupled to the anchor and a second...
2017/0297682 Emergency Landing Stability System for Aircraft
An aircraft emergency landing stability system includes an aircraft a fuselage and landing gear, and a landing stability apparatus coupled to the fuselage,...
2017/0297681 FLYING MACHINE, METHOD FOR USING FLYING MACHINE, AND FLYING MACHINE FRAME
A flying machine includes a flying machine body including a rotor blade; a frame including a frame body supporting the flying machine body, and a pressing...
2017/0297680 Thermally Controlled Active Flow Control System
A method and apparatus are presented. An active flow control system comprises a flow control valve, a manifold, and a temperature control system. The flow...
2017/0297679 Interconnect Drive System
An interconnect drive system for an aircraft has a driveline and clutch control system. The driveline comprises a shaft for each propulsion assembly, each...
2017/0297678 BLADE FOLD SYSTEM USING FLAP HINGE
A rotor system of a tail-sitter aerial vehicle configured to rotate about an axis of rotation is provided including a rotor hub which rotates about the axis of...
2017/0297677 PROPELLER ASSEMBLY WITH AT LEAST TWO PROPELLER BLADES
A propeller assembly with at least two propeller blades that are interconnected by associated connection means, the associated connection means defining a...
2017/0297676 HAT SECTION DOOR FRAME WITH INTEGRAL GUSSETS
A door frame for an aircraft includes first and second beams, each having a first end and a second end. The second beam is substantially parallel to the first...
2017/0297675 HELICOPTER WITH A FUSELAGE AND A COMPOSITE TAIL BOOM
A helicopter with a fuselage and a composite tail boom. The composite tail boom has at least a tubular tail boom cone and a composite attachment ring segment...
2017/0297674 FIBRE-REINFORCED METAL COMPONENT FOR AN AIRCRAFT OR SPACECRAFT AND PRODUCTION METHODS FOR FIBRE-REINFORCED...
Production methods for producing a fibre-reinforced metal component having a metal matrix which is penetrated by a plurality of reinforcing fibres are...
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