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| Patent # | Description |
|---|---|
| 2018/0370674 |
PARTIALLY COLLAPSIBLE FLUID DISPENSING CONTAINER The present invention relates to a partially collapsible dispensing container (100) extending along a longitudinal axis (110) between a first end and second... |
| 2018/0370673 |
LAMINATION SEPARABLE CONTAINER A delaminatable container, including: a container body; and a press-fit cap mounted to the container body. The container body is configured to include a... |
| 2018/0370672 |
PRESSURE CONTAINER WITH DIFFERENTIAL VACUUM PANELS A plastic container (1) has a first set of flex panels (2) and a second set of flex panels (3) one set being adapted to react to pressure changes within the... |
| 2018/0370671 |
DOUBLE-WALLED CONTAINER A double-walled container includes a plurality of ribs. The plurality of ribs include at least one expanded diameter part rib whose upper end is disposed... |
| 2018/0370670 |
VACUUM BLOOD COLLECTION TUBE LABELING MACHINE AND CONVEYING AND LABELING
METHOD FOR VACUUM BLOOD COLLECTION TUBE A vacuum blood collection tube labeling machine and a conveying and labeling method for a vacuum blood collection tube. The machine includes: a loading part of... |
| 2018/0370669 |
HOUSEHOLD VACUUM SEALER AND BAG-CUTTING SEALING METHOD The present invention discloses a household vacuum sealer and a bag-cutting sealing method. In the household vacuum sealer, at least one cutter device is... |
| 2018/0370668 |
BOXING APPARATUS Provided is a boxing apparatus that pushes a plurality of articles into a box, whose opening may face sideways, from the side and, thereafter, change the... |
| 2018/0370667 |
PACKAGING SYSTEM WITH FLEXIBLE OBJECT A packaging system configured to hold objects therein may include a tray that includes a cavity and a set of lugs on an inner surface of the cavity. A first... |
| 2018/0370666 |
METHOD AND APPARATUS FOR ASSEMBLING A DOUBLE-WALLED CONTAINER An assembly system for wrapping an outer wrapper to an inner sleeve to form an outer wall of a double-wall container can include a moveable suction arm. The... |
| 2018/0370665 |
METHOD, DEVICE AND SYSTEM FOR FILLING PHARMACEUTICAL CONTAINERS In one general aspect, a method for filling multiple containers with a pharmaceutical product is disclosed, which comprises decontaminating sealed nested... |
| 2018/0370664 |
SYSTEM FOR LOADING ITEMS INTO A CONTAINER-DEFINING SHEET A system for loading items into a container-defining sheet. The system includes a support for receiving the container-defining sheet, the support having a top... |
| 2018/0370663 |
TIP FILLING METHOD AND IMPROVEMENTS A device for filling a container, such as a dispensing tip, with a powdered or liquid material, and methods of use of the device are disclosed. The device... |
| 2018/0370662 |
THERMAL MANAGEMENT SYSTEM WITH SUBLIMATOR AND ADSORBENT BED A thermal management system includes a sublimator that has a porous plate, a water feed line connected with the sublimator for delivering feed water to the... |
| 2018/0370661 |
ARTIFICIAL GRAVITY SYSTEM HAVING GRAVITY CHAMBERS WITH RIGID SIDE WALLS
THAT ARE EXTENDIBLE A habitation module that provides an artificial gravity environment. In one embodiment, the habitation module includes a rotating structure that rotates about... |
| 2018/0370660 |
Magnetic Shield System for spacecraft, space station and planetary
habitation units A magnetic shield system for providing human occupants of spacecraft with protection from cosmic and solar radiation using electromagnets or solenoids for... |
| 2018/0370659 |
HIGH THRUST TO POWER MICRO CATHODE ARC THRUSTER A thruster for a micro-satellite is disclosed. The thruster includes a cathode composed of a propellant material and an anode composed of ablative material.... |
| 2018/0370658 |
SATELLITE CONSTELLATION FORMING METHOD AND FORMING DEVICE 1. A satellite constellation forming method comprises a satellite deployment step S2, a spacecraft acceleration step S4, a spacecraft orbiting step S5 and... |
| 2018/0370657 |
HIGH CAPACITY COMMUNICATION SATELLITE A spacecraft includes a structural interface adapter for mating to a launch vehicle, an aft surface disposed proximate thereto, and a forward surface disposed... |
| 2018/0370656 |
METHOD OF MEASURING AIRCRAFT BRAKE DISK WEAR The present disclosure relates to a method of measuring wear of a disk in an aircraft brake having a wear indicator that is movably mounted on a stationary... |
| 2018/0370655 |
SYSTEM FOR TRANSPORTING AND INSTALLING AN INSULATION BLANKET AND
ASSOCIATED METHOD A tool for transporting and installing an insulation blanket in a single piece on a component, for example of an aircraft. The component can have a... |
| 2018/0370654 |
MULTIPLE ENERGY SOURCE GUIDANCE SYSTEM AND METHOD FOR DRONES When a first laser beam and a second laser beam are directed to the volume of space, an aerial drone is configured to lock onto the first laser beam using a... |
| 2018/0370653 |
TAKEOFF AND LANDING ASSIST APPARATUS FOR FLIGHT VEHICLE, AND FLIGHT DEVICE A takeoff and landing assist apparatus for a flight vehicle with rotor blades causes the flight vehicle to take off from or be landed on a target point. The... |
| 2018/0370652 |
PORTABLE DRONE LANDING PLATFORM The present invention provides a portable landing platform for a multi-rotor drone, comprising: a landing surface, the landing surface comprising two sections... |
| 2018/0370651 |
ENGINE AND ELECTRICAL MACHINE HEALTH MONITORING Systems and methods for estimating engine and electrical machine health are provided. The systems and methods therefore include features that provide for... |
| 2018/0370650 |
FUEL TANK INERTING SYSTEM A fuel tank inerting module, a fuel tank inerting system for an aircraft, and a method of providing fuel tank inerting systems for aircraft are disclosed. The... |
| 2018/0370649 |
AIRCRAFT FUEL SYSTEM An aircraft fuel system including at least one fuel tank, a source of inerting gas, an inlet for introducing the inerting gas into the at least one fuel tank,... |
| 2018/0370647 |
EXHAUST STUB FOR AN AIRCRAFT ENGINE ASSEMBLY An aircraft engine assembly can include an engine having an exhaust turbine with drive shaft and exhaust collector, a propeller rotationally coupled to the... |
| 2018/0370646 |
PROPULSION SYSTEM FOR AN AIRCRAFT A hybrid-electric propulsion system includes a turbomachine and an electric machine coupled to the turbomachine. A method for operating the hybrid-electric... |
| 2018/0370645 |
Aid Method for Controlling the Energy Situation of An Aircraft, Associated
Computer Program Product and Aid... This aid method for controlling the energy situation of an aircraft includes steps for determining (120) an energy meeting point corresponding to a constraint... |
| 2018/0370644 |
METHOD FOR RATING A PROPULSION UNIT COMPRISING A MAIN ENGINE AND AN
AUXILIARY ENGINE The invention relates to the rating (S) of a propulsion unit (2) comprising a main engine (3) providing main thrust assisted by an auxiliary engine (4)... |
| 2018/0370643 |
VIBRATION ISOLATION DEVICE, ESPECIALLY FOR AIRCRAFT APPLICATIONS A vibration isolation device comprises a frame for mounting on an engine casing, an axis to be mounted to an external component to isolate, a resilient member... |
| 2018/0370642 |
MOTOR AND PROPULSION DEVICE As one embodiment of this motor, the motor is mounted in a multicopter and is provided with: a rotating section that rotates around a rotation axis that... |
| 2018/0370641 |
HYBRID ELECTRIC PROPULSION SYSTEM FOR AN AIRCRAFT A propulsion system for an aircraft includes a propulsor; a turbomachine mechanically coupled to the propulsor for driving the propulsor during a combustion... |
| 2018/0370640 |
AIRCRAFT An aircraft includes: a plurality of rotor units each including a propeller and a motor that drives the propeller; a bag-shaped body including a chamber; and... |
| 2018/0370639 |
HELICOPTER ROTOR ICING DETECTION SYSTEM AND METHOD A system includes a signal monitor to monitor a time rate of change of a revolutions per minute (RPM) trim signal that is received from an RPM command path to... |
| 2018/0370638 |
METHOD OF FABRICATING ROTARY EQUIPMENT FOR A ROTARY WING, PROVIDED WITH A
DEICER, SAID ROTARY EQUIPMENT, AND A... A piece of rotary equipment for a drone, the rotary equipment having a rotary assembly including at least one blade. The rotary assembly includes at least one... |
| 2018/0370637 |
ELECTROTHERMAL ICE PROTECTION SYSTEMS WITH CARBON ADDITIVE LOADED
THERMOPLASTIC HEATING ELEMENTS Pre-fabric, flexible and thermally stable plastic sheets are loaded with carbon additives such as carbon nanotubes (CNTs), graphene, nano carbon fibers,... |
| 2018/0370636 |
Aircraft cabin environmental control system and method and aircraft
equipped with such control system The invention relates to a system for environmental control of an aircraft cabin (5), comprising a device for bleeding compressed air from at least one... |
| 2018/0370635 |
Transport seat system A transport seat system, in particular aircraft seat system, includes at least one first seat, with at least one mounting module that is configured, for the... |
| 2018/0370634 |
Airliner overhead meals delivery Abundant space above an airliner's ceiling lends itself well for replacement of a single food cart blocking aisles with overhead conveyance of passengers'... |
| 2018/0370633 |
LOGISTIC PANEL A novel logistic panel is disclosed. The logistic panel is adapted for use within cargo containers and enables vertical mounting tracks of a cargo beam and... |
| 2018/0370632 |
Unmanned Aerial Vehicle Used in Fishing The present disclosure discloses an unmanned aerial vehicle (UAV), comprising a housing having a top part and a bottom part, a plurality of arms arranged on... |
| 2018/0370631 |
Unmanned Aerial Vehicle for Fishing The present disclosure discloses an unmanned aerial vehicle (UAV), comprising a housing having a top part and a bottom part, a plurality of arms arranged on... |
| 2018/0370630 |
METHOD AND DEVICE FOR CONTROLLING FLIGHT, CONTROL TERMINAL, FLIGHT SYSTEM
AND PROCESSOR A method for controlling flight includes displaying prompt information in a picture received from an aerial vehicle, dividing the picture into at least two... |
| 2018/0370629 |
TILT-ROTOR VERTICAL TAKEOFF AND LANDING AIRCRAFT The present disclosure provides an aircraft system in the tilt-rotor category with four propulsion units where the tilt angle and thrust of each unit is... |
| 2018/0370628 |
TECHNOLOGIES FOR MANAGING DATA CENTER ASSETS USING UNMANNED AERIAL
VEHICLES Technologies for managing assets of a data center include a unmanned aerial vehicle (UAV) communicatively coupled to a remote computing device. The UAV is... |
| 2018/0370627 |
CONFIGURATION FOR VERTICAL TAKE-OFF AND LANDING SYSTEM FOR AERIAL VEHICLES A vehicle, includes a main body. A fluid generator is coupled to the main body and produces a fluid stream. At least one tail conduit is fluidly coupled to the... |
| 2018/0370626 |
VARIABLE PITCH PROPELLER APPARATUS AND VARIABLE THRUST AIRCRAFT USING SAME A variable pitch propeller apparatus enables a propeller to have different pitch angles in one revolution about the drive shaft. The propellers are coupled to... |
| 2018/0370625 |
CONVERTIBLE ROTOR AIRCRAFT A convertible rotor aircraft (CRA) able to convert between airplane and helicopter flight modes during flight, comprising: at least one tillable proprotor... |
| 2018/0370624 |
ROTARY WING VTOL WITH FIXED WING FORWARD FLIGHT MODE An aircraft's two wings and joined thruster propellers or turbines serve as rotary wings in helicopter mode and as fixed wings in airplane mode. The thrusters... |
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