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Patent # Description
2019/0127092 BAG-MAKING AND PACKAGING APPARATUS
A bag-making and packaging apparatus creates one product per cycle by packaging articles in a bag made from a film. The bag-making and packaging apparatus...
2019/0127091 APPARATUS AND METHOD FOR DISPENSING SOLID SUBSTANCES
The invention relates to an apparatus and a method for dispensing solid substances, wherein the apparatus comprises a feeder section with a plurality of feeder...
2019/0127090 METHOD FOR THE PREPARATION OF CONTAINMENT UNITS OF BIOLOGICAL LIQUIDS
The method for the preparation of containment units of biological liquids, comprises the following stages of: furnishing a device (1) comprising a main body...
2019/0127089 SOLAR POWER GENERATOR, SOLAR ARRAY WING, AND SPACE STRUCTURE
A solar power generator overlies a solar power generator when stowed. A plurality of solar cells of the solar power generator includes first solar cells each...
2019/0127088 AIRCRAFT FUSELAGE ASSEMBLING JIG AND METHOD OF USING THE SAME
An aircraft fuselage assembling jig includes: a base provided with a plurality of frame indexes for positioning both ends of a plurality of aircraft fuselage...
2019/0127087 SYSTEMS AND METHODS FOR IN SITU MANUFACTURING OF MINIMALLY TOOLED STRINGERS
Provided are systems and apparatuses for manufacturing aircraft support structures. An example robotic end effector comprises a rotatable reel with a flat...
2019/0127086 METHODS AND SYSTEMS FOR SUPPLYING WATER TO AN AIRCRAFT
There are described methods and systems for supplying water to an aircraft. A water supply assembly is fluidly coupled to a water storage tank via a supply...
2019/0127085 PAYLOAD EXCHANGE FACILITATING CONNECTOR
A payload exchange facilitating connector module, comprises: a) a structure secured to a payload; b) a locking member operatively connected to said structure!...
2019/0127083 UNMANNED AERIAL VEHICLE AND METHOD FOR INDICATING A LANDING ZONE
An unmanned aerial vehicle (UAV) has: a body for carrying an article; at least one rotor; and a light source for generating a light beam to indicate the...
2019/0127082 FLIGHT INSTRUMENT WARNING DISPLAY
Embodiments are directed to flight instrument warnings that are configured to automatically adjust a low airspeed warning band on an airspeed indicator based...
2019/0127081 CONTROL STICK PIVOT
A control stick pivot (200) comprises a primary piv- ot bearing (210), a redundant pivot bearing (220), and a detection component for detecting malfunction of...
2019/0127080 SYSTEM AND METHOD FOR CONSOLIDATING, RATIFYING AND ESCALATION OF UNCERTIFIED APPLICATIONS NOTIFICATIONS
A method and system for alert notifications is disclosed. The method comprises collecting, in an alert management unit onboard a platform, one or more alerts...
2019/0127079 AIRCRAFT STALL WARNING/PROTECTION WITH TIME-VARYING MAXIMUM ANGLE OF ATTACK SETTINGS FOR ICING CONDITIONS
This non-limiting technology proposes to modify the maximum angle of attack setting (.alpha..sub.setting) of the Stall Protection or Stall Warning Systems...
2019/0127078 METHOD AND SYSTEM FOR IMPROVING AIRCRAFT FUEL EFFICIENCY
A method for improving inflight fuel efficiency of an aircraft includes sensing aircraft fuel weight in the aircraft fuel tanks and reading the fuel weight by...
2019/0127077 AIRCRAFT TAILCONE INCORPORATING AN APU ANNULAR AIR INTAKE
An aircraft tailcone comprising a tailcone fuselage, a turbomachine, for example an APU, housed inside the tailcone, a ram air intake on the tailcone fuselage...
2019/0127076 Methods and Aircraft for Optimized Reverse Thrust Operation During Landing
An example method of optimizing reverse thrust operation on an aircraft having two or more engines while landing the aircraft is described. The method includes...
2019/0127075 LATCH INDICATION SYSTEM AND METHOD FOR A FAN COWL OF AN AIR VEHICLE
There is provided a latch indication system for a fan cowl of an air vehicle. The system has a door movable between a closed position and an open position, and...
2019/0127074 PRIMARY SUPPORT STRUCTURE FOR AN AIRCRAFT POWER PLANT SUPPORT PYLON
A primary structure of an aircraft power plant support pylon is disclosed having a bottom stringer and two lateral walls formed in a single piece or welded so...
2019/0127073 PRIMARY SUPPORT STRUT STRUCTURE FOR AN AIRCRAFT
A primary support strut structure and a method of manufacturing thereof for an aircraft power plant is disclosed having a first half-shell including a first...
2019/0127072 HIGH VOLUME FLOW MANAGEMENT OF COOLING AIR
A flow management system for delivering air to a heat load of an aircraft includes a cover having an opening for receiving and directing an airflow, and a duct...
2019/0127071 Lie-Flat Passenger Seat Configurations For Transportation
Example lie-flat passenger seat configurations for transportation are described. A non-elevated passenger seat includes a seat base and a seatback pivotably...
2019/0127070 Slouching Divan with Damped Motion
A slouching aircraft divan transitions between discrete upright, slouched, and berthed configurations. The divan has a seatpan including rollers which travel...
2019/0127069 GAP COVERING BETWEEN CABIN MONUMENTS, IN PARTICULAR FOR A PASSENGER CABIN OF AN AIRCRAFT
A cabin monument arrangement for a passenger cabin of an aircraft, has at least two cabin monuments arranged next to each other, aligned substantially parallel...
2019/0127068 DUAL URINAL LAVATORY MONUMENT
A lavatory monument configured to be positioned in an aircraft interior that includes an enclosure that includes first, second, third and fourth walls, and...
2019/0127067 Autonomous aerial vehicle
Autonomous aerial vehicles and methods of operating the same. An unmanned aerial vehicle in accordance with various embodiments may receive a defined flight...
2019/0127066 REMOTE-CONTROLLED UNMANNED FOLDABLE AIRCRAFT
A remote-controlled unmanned foldable aircraft comprises at least two motors that allow the aircraft to fly, and at least one support structure for supporting...
2019/0127065 BLADELESS UNMANNED AERIAL VEHICLE
A bladeless unmanned aerial vehicle includes a body and two or more thruster assemblies coupled to the body. The thruster assemblies each includes a ducted fan...
2019/0127064 DRONE-BASED PAINTING SYSTEM
A painting system that makes use of drones such as modified quadrotors. The drone includes a support arm that carries a paint nozzle configured for pan and...
2019/0127063 THREE DIMENSIONAL SCALABLE AND MODULAR AIRCRAFT
A three-dimensionally scalable, modular and customizable aircraft composed of stably flyable plurality of planar unitary systems which provides a coordinated...
2019/0127062 Airplane without wings
This aircraft without wings is designed to allow unmanned flight to any place on earth by simplified construction. This is accomplished by turning the gas...
2019/0127061 TILTWING MULTICOPTER WITH FOLDABLE AND NON-FOLDABLE PROPELLERS
An aircraft includes a tiltwing where the tiltwing is a single wing to which starboard-side and non-foldable outer propeller, a port-side and non-foldable...
2019/0127060 FLIGHT VEHICLE
Method and apparatus for a flight vehicle including a wing having a high aspect ratio and first and second rotors having a high aspect ratio, with a ratio of...
2019/0127059 ROTORCRAFT ANTI-TORQUE SYSTEM
There is provided a rotorcraft, including a body, including a front portion and a tail portion; a main rotor system coupled to the front portion of the body,...
2019/0127058 SWASH PLATE SYSTEM FOR A HELICOPTER ROTOR
A device for controlling a collective pitch and a cyclic pitch of rotor blades of a rotoreraft of a direct turbine driven type and. contra-rotating coaxial...
2019/0127057 EMERGENCY COLLECTIVE ACTUATOR AND METHOD FOR A HELICOPTER
A helicopter includes a rotor system having a rotor with an adjustable pitch that is controlled at least in part by a pilot using a collective control and...
2019/0127056 COMPOUND MULTI-COPTER AIRCRAFT
A compound aircraft embodies an array of rotors for vertical flight positioned on support booms and wing elements for cruise flight coupled to a central...
2019/0127055 Apparatus for Using Aircraft Active Vibration Control System as Pilot Cueing Aid
Systems and methods for cueing a helicopter pilot when a flight parameter (such as rotor-induced vibration level, airspeed, bank angle, icing accumulation,...
2019/0127054 Compact Design of a Liquid Inertia Vibration Elimination System
A piston for use in a liquid inertia vibration elimination ("LIVE") system. The piston includes a port that extends from a first end of the piston to an...
2019/0127053 AIRCRAFT UNDERCARRIAGE WITH BRAKED AND MOTOR-DRIVEN WHEELS
The invention relates to an aircraft undercarriage provided at its bottom end with a rocker arm (2) carrying at least two axles (4, 5), including one in front...
2019/0127052 SYSTEMS AND METHODS OF AIRCRAFT WALKING SYSTEMS
An unmanned aerial vehicle (UAV) includes a central body and a plurality of landing gears that are extendable from and movable relative to the central body....
2019/0127051 AIRCRAFT CONTROL SYSTEM, AIRCRAFT CONTROL METHOD, AND AIRCRAFT
An aircraft control system includes a flow control device and a control circuit. The flow control device is configured to control a flow of air around an...
2019/0127050 FLIGHT CONTROL SYSTEMS AND METHODS
A high-integrity, redundant flight control system includes a plurality of flight control computers each having a back-up inertial sensor embedded therein. At...
2019/0127049 ADAPTIVE FEEDBACK CONTROL OF FORCE FIGHTING IN HYBRID ACTUATION SYSTEMS
Systems for compensating for force fighting in multi-actuator systems are provided. A drive controller unit comprises a first feedforward controller in...
2019/0127048 FLAP ACTUATING SYSTEM FOR USE IN AN AIRCRAFT
A flap actuating system for use in an aircraft comprises a carriage for supporting and guiding a flap which is engageable with and translationally movable...
2019/0127047 CARRIAGE FOR SUPPORTING AND GUIDING A FLAP AND AIRFOIL FLAP SYSTEM FOR USE IN AN AIRCRAFT
A carriage for supporting and guiding an aircraft flap translationally moveable along a linear slide bearing comprises a drive element connectable to an...
2019/0127046 THREE-AXIS CONTROL STICK
There is provided a control stick module (10) comprising: a first shaft (100); a second shaft (110); a joint (140) connecting the first and second shafts; and...
2019/0127045 ROTATING FRONT PART OF AN AIRCRAFT TURBOMACHINE INTAKE, OF IMPROVED DESIGN PERMITTING REPEATED REMOVAL OF THE...
The invention relates to a rotating front part of an aircraft turbomachine intake comprising bolts for attaching a cone tip to an internal support, each bolt...
2019/0127044 Mechanical Droop for Spoiler Operation
A system for mechanical operation of an aircraft wing includes a torque tube rotatable at a first rate of rotation to cause a downward rotation of a control...
2019/0127043 WING SEGMENT AND AIRCRAFT HAVING A WING SEGMENT
A wing segment for an aircraft includes a first skin element with a material having anisotropic characteristics and a rib element arranged between leading and...
2019/0127042 Fluid Systems That Include a Co-flow Jet
Fluid systems are described herein. An example embodiment of a fluid system has a first body portion, a second body portion, a plurality of supports, a...
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