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Patent # Description
2018/0044045 PRODUCE PACK ARRANGEMENT APPARATUS
Provided is a produce pack arrangement system. The produce pack arrangement system comprises a produce supply station, a produce orientation and assembly...
2018/0044044 Packaging machine for fowls
PACKAGING MACHINE FOR FOWLS, for automatic packing of entire fowls or its parts, whose proposal is to provide packaging totally automated with inspiring...
2018/0044043 DEVICE FOR WRAPPING A STACK OF GOODS WITH A TUBULAR HOOD AND METHOD FOR CHANGING THE TUBULAR FILM STOCK IN AN...
The present invention relates to a device for wrapping a piece item stack, which is formed of a plurality of piece item parts that are disposed on top of one...
2018/0044042 AQUEOUS SOLUTION AND METHOD FOR USE THEREOF
Aqueous compositions contain hydrochloric acid at a concentration between 8 wt % and 28 wt % inclusive. The amino acid; hydrochloric acid mole ratio may be...
2018/0044041 Space Modular Reactor for Propulsion (SMR-P)
This invention serves as the fundamental design for a space-based, nuclear-powered spacecraft for deep space journeys. Nuclear energy is used as the motive...
2018/0044040 CIRCUITS AND METHODS FOR REDUCING FLICKER IN AN LED LIGHT SOURCE
Method and circuits for balancing a first waveform used to drive an LED are disclosed herein. The first waveform has a first cycle with a first amplitude and a...
2018/0044039 BOND FIXTURE FOR SHEATH ASSEMBLY OF ROTOR BLADE
A bond fixture includes a first fixture having a heater and a plurality of clamps. Each of the plurality of clamps includes a first member and a second member...
2018/0044038 MAIN ROTOR BLADE CUFF BOND FIXTURE
A bond fixture including a plurality of supports mounted about a surface. At least one of the plurality of supports includes a vertical member and a hand crank...
2018/0044037 BOND FIXTURE FOR LEADING EDGE ASSEMBLY
A bond fixture includes a frame defining a chamber for receiving a component. At least one bladder assembly is connected to the frame. The at least one bladder...
2018/0044036 BOND FIXTURE FOR COMPOSITE SPLICE CAP ASSEMBLY
A bond fixture for bonding a component includes a frame defining a chamber for receiving the component. A first pad and a second pad are mounted to the frame....
2018/0044035 ROCKET LANDING SYSTEM
A generally vertical rocket (2) flies generally horizontally into recovery line, cable or chain (3) suspended between towers (5, 7) of a catamaran landing ship...
2018/0044034 Auxiliary Security System for Aircraft Black Box System
A multifunction avionics server provide for the execution of both certified and uncertified applications in data-serving capacities in which one certified...
2018/0044033 SYSTEM AND APPARATUS FOR REFUELING AIRCRAFT FROM A WATERCRAFT
The invention is a watercraft to aircraft refueling system ("WARS"). A WARS is a refueling system based from a watercraft, such as a surface ship or submarine....
2018/0044032 METHOD FOR CONTROLLING A FUEL TANK INERTING SYSTEM AND AN INERTING SYSTEM FOR CARRYING OUT THE METHOD
A method for controlling an inerting system designed to inject a flow of inert gas into a fuel tank of an aircraft during a mission. The method includes:...
2018/0044031 TURBOFAN ENGINE COMPRISING AN OVERPRESSURE FLAP AT A FAIRING BEING LOCATED AT THE SECONDARY FLOW CHANNEL
A turbofan engine including a core engine and at least one fan by means of which fluid is guided to a primary flow channel for the core engine as well as to a...
2018/0044030 TURBOFAN ENGINE COMPRISING A FAIRING BEING LOCATED IN THE SECONDARY FLOW CHANNEL AND HAVING A SEPARATE END ELEMENT
A turbofan engine including a core engine and at least one fan by means of which fluid is guided to a primary flow channel for the core engine as well as to a...
2018/0044029 COAXIAL ALIGNED ELECTRIC MOTOR GROUP FOR PROPELLING AN UNMANNED AERIAL SYSTEM
A coaxial, aligned electric motor group for propelling an unmanned aerial system. The electric motor group includes a first electric motor having a first rotor...
2018/0044028 THRUST FORCE GENERATION DEVICE AND AIRCRAFT
The thrust force generation device is provided with: a turbo fan engine unit that includes a generator for generating power using a rotation force of a drive...
2018/0044027 DUAL MODE SUPPLEMENTAL STRUT AND DAMPER
A strut for mounting an engine in an aircraft includes a first member and a second member. A friction material is coupled to a surface of the first member and...
2018/0044026 ANNULAR OZONE CONVERTER WITH REPLACEABLE CORE
An ozone converter includes a toroidal shaped inlet housing and an outlet housing that is removably coupled to the inlet housing. The converter also includes a...
2018/0044025 SWIVEL BASE ASSEMBLY WITH FORE/AFT/ROTATIONAL MOVEMENT AND WARPING FEATURES
Systems and methods for swivel base assemblies for seats are provided. A swivel base assembly for an aircraft seat may comprise a swivel center beam, a swivel...
2018/0044024 MOLDED SIDEWALL ARMREST BETWEEN FUSELAGE FRAME BAYS
An armrest system may include an inner sidewall panel attached to a vehicle frame. The inner sidewall panel may abut at least two parallel frame members of the...
2018/0044023 AIRCRAFT GALLEY UNIT
In order to provide an aircraft galley which is equipped with a sink structure ensuring a work space for crews in a galley and a wide drainage region, an...
2018/0044022 PIVOT BIN ASSEMBLY WITH TWO PART PIVOT AXLE
An aircraft storage bin that includes an upper housing with first and second side panels, a bucket that includes a bottom and first and second sides, a first...
2018/0044021 CART STOWAGE PLACARD ENABLING PLATE
A retractable placard system for galley cart storage bays is provided. The placard system includes an outer plate and a placard. The outer plate is mounted...
2018/0044020 HOISTING CABLE FOR A HELICOPTER HOIST
A hoisting cable for a helicopter hoist includes at least one first electric conductor built into a non-conductive structure, and at least one second electric...
2018/0044019 ELECTROMAGNETIC SURVEY SYSTEM HAVING TOW ASSEMBLY WITH ATTITUDE ADJUSTMENT
A tow assembly for airborne geophysical surveying that comprises a frame incorporating geophysical surveying equipment; and a suspension assembly for...
2018/0044018 PACKAGE DELIVERY AND RECEPTION WITH DRONES
A computer program product for automatically delivering a physical mail includes receiving, by an unmanned aerial vehicle from an unmanned aerial vehicle...
2018/0044017 FOLLOW FOCUS DEVICES, AND REMOTE-CONTROL FOLLOW FOCUS SYSTEMS AND AERIAL VEHICLES WITH FOLLOW FOCUS DEVICES
A follow focus device includes a signal receiver, a controller electrically connected to the signal receiver, and a control interface electrically connected to...
2018/0044016 APPARATUS AND METHOD FOR CONTROLLING STABILITY OF UNMANNED AERIAL VEHICLE
The present invention provides an unmanned aerial vehicle that can maintain stability by changing positions of rotating rotors when one of the rotating rotors...
2018/0044015 UNMANNED AERIAL VEHICLES, CHARGING SYSTEMS FOR THE SAME AND METHODS OF CHARGING THE SAME
An unmanned aerial vehicle includes a body portion, a plurality of driving portions, a plurality of arms and first and second landing members. The body portion...
2018/0044014 SELF-MOVING APPARATUS AND COMPONENTS THEREOF
The present invention relates to SMAs (self-moving apparatuses) which use any type of propulsion means, including, without limitation, an FPGB (propeller-gear...
2018/0044013 APPARATUS AND METHOD FOR DIRECTING THRUST FROM TILTING CROSS-FLOW FAN WINGS ON AN AIRCRAFT
A variable thrust cross-flow fan system for an aircraft including a rotatable wing member having a first housing member; an actuator assembly operably coupled...
2018/0044012 AIRCRAFT WITH TILTING CROSS-FLOW FAN WINGS
An aspect provides an aircraft including a fuselage and a cross-flow fan system attached to the fuselage. The cross-flow fan system including a cross-flow fan...
2018/0044011 ROTOR-BLOWN WING WITH PASSIVELY TILTING FUSELAGE
An aircraft includes a wing where a first rotor and a second rotor are coupled to the wing at a fixed position relative to the wing. The aircraft also includes...
2018/0044010 AIRCRAFT TAIL WITH CROSS-FLOW FAN SYSTEMS
In one aspect, there is provided an aircraft, including a fuselage having a longitudinal axis extending from a front portion through an aft portion; first and...
2018/0044009 Rotorcraft Variable Thrust Cross-flow Fan Systems
In some embodiments, a rotorcraft includes a fuselage, a tailboom, a drive system and a variable thrust cross-flow fan system. The cross-flow fan system...
2018/0044008 CONTROL SYSTEM FOR CONTROLLING AT LEAST COLLECTIVE PITCH OF ROTOR BLADES OF A MULTI-BLADE ROTOR IN A...
A control system for controlling at least collective pitch of rotor blades, of a multi-blade rotor with a rotor shaft in a rotary-wing aircraft, the control...
2018/0044007 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...
2018/0044006 SPLICE CAP NICKEL ABRASION STRIP CAUL
A caul assembly includes a semi-rigid caul plate formed in a shape complementary to a portion of a component receivable therein and a heater located at an...
2018/0044005 APPARATUS FOR PROVIDING RAIL-BASED VERTICAL SHORT TAKEOFF AND LANDING AND OPERATIONAL CONTROL
Apparatus for vertical or short takeoff and landing, and operational control during flight. In one embodiment, the apparatus includes a main body assembly, the...
2018/0044004 SELECTIVELY THRUSTING PROPULSION UNITS FOR AERIAL VEHICLES
Aerial vehicles may include propulsion units having motors with drive shafts that may be aligned at a variety of orientations, propellers with variable pitch...
2018/0044003 FLIGHT DEVICE
A flight device includes a device body with a surface, a plurality of arm structures disposed in the device body and a plurality of rotor modules disposed to...
2018/0044002 CORE MATERIAL FOR BALANCED ROTOR BLADE
A method of forming a balanced rotor blade assembly includes measuring a weight of a plurality of sub-components of the rotor blade assembly excluding a core....
2018/0044001 AIRCRAFT LANDING GEAR COMPRISING A MAIN DAMPER AND AN ANTI-SHIMMY SECONDARY DAMPER
Aircraft landing gear (1) comprising: an axle shaft (2); a strut (3) extending along a main strut axis (Z) and having a first part (3a) carrying the said...
2018/0044000 GROUND MOVEMENT SYSTEM PLUGIN FOR VTOL UAVS
A ground movement plug-in (GMP) apparatus for providing ground propulsion to an unmanned aircraft vehicle (UAV). In an embodiment, the GMP apparatus includes a...
2018/0043999 AIRCRAFT TIRE
An aircraft tire includes a tire body forming an outer peripheral part of an aircraft wheel; and a protrusion with a pressure receiving surface configured to...
2018/0043998 REMOTE HYDRAULIC UTILITY SYSTEM FOR AN AIRCRAFT
A remote hydraulic system for an aircraft may provide hydraulic fluid to nose landing gear while being isolated from the main landing gear and other main...
2018/0043997 INLET ASSEMBLY FOR AN AIRCRAFT AFT FAN
The present disclosure is directed to a low-distortion inlet assembly for reducing airflow swirl distortion entering an aft fan mounted to a fuselage of an...
2018/0043996 INLET ASSEMBLY FOR AN AIRCRAFT AFT FAN
The present disclosure is directed to a low-distortion inlet assembly for reducing airflow swirl distortion entering an aft fan mounted to a fuselage of an...
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