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Patent # Description
2019/0061974 TRANSIENT VOLTAGE SUPPRESSION PROTECTION CIRCUIT INCLUDING BUILT IN TESTING AND ENABLE - DISABLE FUNCTIONALITY
An aircraft electrical system includes a controller system having a self-testing system configured to test an operability of a transient voltage suppression...
2019/0061973 ACTUATOR MONITORING SYSTEM USING INERTIAL SENSORS
Sensor data is received from an inertial measurement unit on a vehicle. An observed attitude and an observed attitude rate of the vehicle are determined based...
2019/0061972 INTERACTIVE ANALYSIS OF STRUCTURAL HEALTH DATA
A system and method includes a structural body, a plurality of structural health monitoring (SHM) sensors, and first and second computer systems. The...
2019/0061971 Flight Management System Having Customized Performance Database
A flight management system which has access to customized information concerning the actual characteristics of a specific airplane or a specific fleet of...
2019/0061970 MULTI-ROTOR AERIAL DRONE WITH THERMAL ENERGY HARVESTING
Some features pertain to a quad-rotor or other aerial drone having a thermoelectric generator (TEG) for harvesting waste heat from a processor of the drone....
2019/0061969 VARIABLE GEOMETRIES TRANSIENT CONTROL LOGIC
Herein provided are methods and systems for controlling an engine having a variable geometry mechanism. A power level difference between a requested engine...
2019/0061968 HYBRID VTOL FIXED-WING DRONE
A long-distance drone is disclosed having a canard body style with a main body, a left main wing, a right main wing, a left forewing, and a right forewing. The...
2019/0061967 SAFETY MAINTENANCE PANEL FOR A THRUST REVERSER
A safety maintenance panel for a thrust reverser is provided. The thrust reverser may comprise one or more doors configured to actuate from a closed position...
2019/0061966 HIGH-MOUNTED AIRCRAFT NACELLE
A nacelle mounted above a wing of an aircraft. A support structure on the nacelle above the pylon resists forces in different directions, and includes door...
2019/0061965 TURBINE ENGINE WITH SINGLE WALL CANTILEVERED ARCHITECTURE
An apparatus and method for mounting a turbine engine to an aircraft can include an engine core for the turbine engine including a compressor section, a...
2019/0061964 Operation of a Vertical Takeoff and Landing Aircraft
A method is provided for operating a propulsion system of a vertical takeoff and landing aircraft, the propulsion system including a turbomachine, an electric...
2019/0061963 HYBRID AIRCRAFT PROPULSORS HAVING ELECTRICALLY-DRIVEN AUGMENTOR FANS
Hybrid aircraft propulsors having electrically-driven augmentor fans are disclosed. An example apparatus includes a turbofan having a core engine and a ducted...
2019/0061962 PROPULSION AND ELECTRIC POWER GENERATION SYSTEM
A propulsion and electric power generation system includes a dual-spool turbofan gas turbine engine and an electrical generator. The dual-spool turbofan gas...
2019/0061961 AIRCRAFT PROPULSION SYSTEM AND METHOD
An aircraft propulsion system includes a boundary layer ingestion (BLI) fan system disposed at an aft end of an aircraft. The BLI fan system includes a fan...
2019/0061960 ENERGETIC EVACUATION SLIDE
An evacuation system may comprise an evacuation slide comprising an inflatable portion; and a reactant packet disposed within the inflatable portion including...
2019/0061959 METHOD AND APPARATUS FOR PREDICTING CONDITIONS FAVORABLE FOR ICING
A method and apparatus for predicting conditions favorable for icing, includes sensing a value indicative of a thermal cycling period, comparing, the sensed...
2019/0061958 METHOD OF MAKING A MAGNETOSTRICTIVE OSCILLATOR ICE RATE SENSOR PROBE
A method of improving the measurement accuracy of a digital ice rate sensor by providing an enhanced surface finish on a magnetostrictive oscillator detector...
2019/0061957 AIRCRAFT CABIN CLIMATE CONTROL USING DATA FROM MOBILE ELECTRONIC DEVICES
Methods, apparatus, systems, and articles of manufactures for aircraft cabin temperature control using temperature data from mobile electronic devices are...
2019/0061956 PROTECTION DEVICE WITH MODULABLE DIMENSIONS FOR AN EQUIPMENT ANCHORING RAIL
The invention relates to a device for protecting a detachable equipment anchoring rail having adjustable dimensions, which is lockable, tamper-proof, reusable...
2019/0061955 PASSENGER SEAT PRIVACY HEADREST
In an illustrative embodiment, a privacy headrest assembly is configured to provide privacy to a passenger in an aircraft passenger seat, including a headrest...
2019/0061954 DEPLOYABLE TABLE ASSEMBLY
The present invention provides a deployable table assembly 10 comprising a deployable table 20, and a support arm 30, the deployable table is moveably mounted...
2019/0061953 Tray Table with Personal Entertainment Device Holder
In an illustrative embodiment, a two-piece folding tray table includes a personal electronic device (PED) support member connected to a tray section such that,...
2019/0061952 CIRCULAR MAGNETIC JACK
According to an aspect of the present invention, there is provided an electrical connector socket comprising a housing having a front face configured to mate...
2019/0061951 STOWABLE SEAT WITH PIVOTING SEAT PAN FOR ADVANCED COMFORT
A stowable seat is provided. The stowable seat may comprise a housing and a first track coupled to the housing. A backrest may be slidably coupled to the first...
2019/0061950 SLIDE EXTRACTOR BRAKING SYSTEM
Embodiments of the present disclosure relate generally to improved braking systems for slide extractors. Slide extractors are generally used in aircraft...
2019/0061949 EMERGENCY EQUIPMENT FOR AN AIRCRAFT COMPRISING A RESPIRATORY MASK
An emergency equipment for an aircraft comprising: --a respiratory mask (5) comprising a harness (6), the respiratory mask (5) being adapted to be applied in a...
2019/0061948 CONFORMABLE TANK FABRICATED USING ADDITIVE MANUFACTURING
A conformable tank includes a body with a plurality of walls defining a cavity in the body, and an internal support connected to an internal surface of one of...
2019/0061947 CONFORMABLE TANK WITH SANDWICH STRUCTURE WALLS
A conformable tank includes a body with a plurality of composite walls formed around a cavity, and an internal support connected to one of the plurality of...
2019/0061946 INTELLIGENT LOCK FOR CARGO HANDLING SYSTEM
A cargo handling system for restraining a unit load device includes a structural channel having a hollow interior, and a locking mechanism associated with the...
2019/0061945 SYSTEM AND METHOD FOR RESTRAINING CARGO
An aircraft cargo restraint system includes an attenuator member fixed at two first attachment locations within a cargo storage compartment of a fuselage of an...
2019/0061944 AERIAL VEHICLE IMPLEMENT HITCH ASSEMBLY
A hitch mount assembly for an unmanned aerial vehicle is shown and described. The hitch mount assembly may include a mount body operatively engagable with an...
2019/0061943 Aircraft Mounted Hoist System Having a Multi-Stranded Wire Rope Cable
A hoist system includes a wire rope cable having a first end and a second end. The wire rope cable further including multiple strands twisted into a helical...
2019/0061942 METHOD AND SYSTEM FROM CONTROLLING AN UNMANNED AERIAL VEHICLE
A method is provided. An unmanned aerial vehicle (UAV) can be operated in an autonomous mode, performing course corrections from sensor data using an object...
2019/0061941 AUTONOMOUS SELF-STABILIZING AERIAL SYSTEM AND METHOD
An aerial system includes a body, a propeller coupled to the body, and a motor coupled to the propeller. The motor is configured to rotate the propeller in a...
2019/0061940 UAV, SYSTEM AND METHOD FOR DETERMINING LANDING STATUS OF UAV
An unmanned aerial vehicle (UAV), a system and a method for determining a landing status of the UAV are provided. The UAV system includes a UAV, a landing...
2019/0061939 Managing Package Deliveries by Robotic Vehicles
Various methods for performing package deliveries by a robotic vehicle may include determining whether an individual at a package delivery location is a...
2019/0061938 RADIO FREQUENCY STEALTHY TETHERED AIRCRAFT
A tethered aircraft is provided in which the conductive tether is broken into two or more sections and where at least one section is an RF-isolating section...
2019/0061937 COUPLING DEVICE FOR COUPLING MODULES WITH EACH OTHER, AIRCRAFT COMPRISING THE COUPLING DEVICE, METHOD FOR THE...
A coupling device for coupling modules with each other, comprising: a coupling surface, a primary coupling member and at least two secondary coupling members....
2019/0061936 VERTICAL TAKE OFF AND LANDING (VTOL) AIRCRAFT WITH VECTORED THRUST HAVING CONTINUOUSLY VARIABLE PITCH ATTITUDE...
The presently disclosed embodiments relate to vertical takeoff and landing (VTOL) aircraft that have the capability of hovering in both a "nose forward" and a...
2019/0061935 AIR VEHICLE AND METHOD AND APPARATUS FOR CONTROL THEREOF
An air vehicle comprising a main body and a pair of opposing wing members extending substantially laterally from the main body, at least a first propulsion...
2019/0061934 SYSTEMS AND METHODS FOR WINGED DRONE PLATFORM
Various techniques are provided for a winged drone platform. In one example, a drone can be provided. The drone can include a drone body, a plurality of wings,...
2019/0061933 UNMANNED AERIAL VEHICLES CAPABLE OF ENVIRONMENTAL INTERACTION
An unmanned aerial vehicle (UAV) system is disclosed. The UAV system includes a chassis, a plurality of propeller assemblies configured to provide vertical...
2019/0061932 VERTICAL TAKEOFF AND LANDING AIRCRAFT
There is provided a vertical takeoff and landing aircraft (VTOL), having a main propulsion unit (GT engine) with high-pressure and low-pressure turbine shafts...
2019/0061931 Vibration Control with Active Lag Damper
A rotor system includes a hub assembly, a first, second, and third rotor blade rotatably attached to the hub assembly, a first, second, and third damper...
2019/0061930 GEODESIC COMPOSITE STRUCTURES
In one embodiment, a method may comprise coupling a plurality of reinforcement fibers to a plurality of spherical components; inserting the plurality of...
2019/0061929 Rotor Assembly with High Lock-Number Blades
An aircraft rotor assembly has a central yoke and a plurality of rotor blades coupled to the yoke for rotation with the yoke about an axis, each blade having a...
2019/0061928 AN ELASTIC FLAPPING HINGE FOR CONNECTING A ROTOR BLADE TO A ROTOR HUB OF A ROTARY WING AIRCRAFT
An elastic flapping hinge for connecting a rotor blade to a rotor hub of a rotary wing aircraft, comprising an elastic flapping hinge member arrangement that...
2019/0061927 ADAPTABLE ROTOR CONTROL SYSTEM FOR A VARIABLE NUMBER OF BLADES
In one embodiment, a rotor hub comprises a yoke for attaching a plurality of rotor blades, a constant velocity joint to drive torque from a mast to the yoke...
2019/0061926 LOW MOMENT ROTOR HUB
In one embodiment, a rotor hub comprises a hub body, and a plurality of blade grips configured for attaching a plurality of rotor blades. The rotor hub further...
2019/0061925 Cargo Transportation System having Perimeter Propulsion
A cargo transportation system includes a cargo platform having an upper surface and a perimeter. A propulsion system is disposed about the perimeter of the...
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