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公开(公告)号：US20180208295A1
公开(公告)日：2018-07-26
申请号：US15878831
申请日：2018-01-24
Applicant: AIRBUS HELICOPTERS DEUTSCHLAND GMBH
Inventor： Sebastian MORES , Alessandro D'ALASCIO , Thomas KNEISCH , Klaus KICKER , Stefanie LINK , Uwe KIESEWETTER , Marius BEBESEL
CPC classification number: B64C11/001 , B64C11/48 , B64C27/08 , B64C27/20 , B64C2201/027 , B64C2201/162 , B64D25/00
Abstract: A thrust producing unit for producing thrust in a predetermined direction, comprising at least two rotor assemblies and a shrouding, each one of the at least two rotor assemblies, defining an associated rotor plane, wherein a first rotor assembly of the at least two rotor assemblies is provided for operating in a failure-free operating mode of the thrust producing unit and a second rotor assembly of the at least two rotor assemblies is provided for operating at least in case of a failure of the first rotor assembly, and wherein the shrouding accommodates at most one of the at least two rotor assemblies.
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102.发明申请公开(公告)号：US20180178899A1
公开(公告)日：2018-06-28
申请号：US15391700
申请日：2016-12-27
Inventor： Dongsoo HAR , Celso MORAES , Dongsuk KUM
CPC classification number: B64D27/24 , B64C3/385 , B64C5/02 , B64C11/001 , B64C13/50 , B64C29/02 , B64C39/024 , B64C2201/021 , B64C2201/042 , B64C2201/066 , B64C2201/088 , B64C2201/104 , B64C2201/108 , B64C2201/141 , B64C2201/146 , B64C2201/162 , B64C2201/165 , Y02T50/62
Abstract: An aircraft includes: a fuselage having opposing leading and trailing extremities along a vertical axis; a fixed wing airframe having opposed at least two main wings connected to the fuselage and extending on a horizontal axis; at least two electric coplanar main wing motors respectively attached to the main wings; a duct frame attach to the trailing extremity of the fuselage; at least two horizontal stabilizers connected to the duct frame and extending on the horizontal axis; an electric tail motor fitted an inner side of the duct frame; multiple battery packs installed inside the fuselage and suitable for supply power to the main wing motors and the tail motor; and support beams suitable for connecting the duct frame to the fuselage.
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公开(公告)号：US10007890B1
公开(公告)日：2018-06-26
申请号：US14752725
申请日：2015-06-26
Applicant: Amazon Technologies, Inc.
Inventor： Oliver Christoph Purwin , Andrew Stubbs
CPC classification number: G06Q10/087 , B64C39/024 , B64C2201/022 , B64C2201/128 , B64C2201/14 , B64C2201/162 , G08G5/0069
Abstract: The disclosed inventory systems and methods can be used to retrieve and transport items from one location in an inventory system to another. Specifically, an unmanned aerial vehicle (UAV) including passive buoyancy element, a thrust unit, and a retention feature, can be controlled by a management component to retrieve one or more items, transport the item or items, and deposit the item or items. For example, a UAV can be controlled to obtain an item at one location in a warehouse such as a first floor and lift said item to a second location in the warehouse such as a second floor, and deposit the item at the second location.
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公开(公告)号：US10000284B1
公开(公告)日：2018-06-19
申请号：US14752746
申请日：2015-06-26
Applicant: Amazon Technologies, Inc.
Inventor： Oliver Christoph Purwin , Andrew Stubbs
CPC classification number: B64C39/024 , B64B1/26 , B64B1/40 , B64C2201/022 , B64C2201/127 , B64C2201/128 , B64C2201/148 , B64C2201/162 , B64C2201/182
Abstract: The disclosed unmanned aerial vehicle (UAV) includes a buoyant airbag, a drive unit, a retention feature, and an onboard control module that can be configured to cause the drive unit to displace the UAV, cause the retention feature to retain one or more items for transport, and receive instructions to transfer items from one location to another. For example, a UAV can be controlled to obtain an item at one location in a warehouse such as a first floor, lift said item to a second location in the warehouse such as a second floor, and deposit the item at the second location.
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公开(公告)号：US09932111B2
公开(公告)日：2018-04-03
申请号：US15009829
申请日：2016-01-29
Applicant: The Boeing Company
Inventor： Charles Spinelli
CPC classification number: B64C39/024 , B64C2201/021 , B64C2201/104 , B64C2201/108 , B64C2201/12 , B64C2201/123 , B64C2201/141 , B64C2201/162 , G06K9/0063 , G06K9/00771 , G06K9/00791 , G08G5/0013 , G08G5/0056 , G08G5/0069 , G08G5/0086 , G08G5/0091 , H04L67/12
Abstract: A method and system for assessing a situation using an unmanned vehicle is disclosed. An unmanned vehicle receives a transmission indicating a situation at a designated location, and then navigates to the designated location. The unmanned vehicle may reach the designated location via air or ground travel, or a combination thereof. The unmanned vehicle receives signals from a first subset of sensors indicating information concerning an environment at the designated location and from a second subset of sensors indicating information concerning one or more objects associated with the situation. The unmanned vehicle then sends one or more transmissions based on the received signals, facilitating rapid determination of the situation.
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Patent Agency Ranking
公开(公告)号：US20180090040A1
公开(公告)日：2018-03-29
申请号：US15626181
申请日：2017-06-19
Applicant: Patrick Randall , Joeseph Bernstein
Inventor： Patrick Randall , Joeseph Bernstein
CPC classification number: G09F21/08 , B64C27/20 , B64C39/024 , B64C2201/027 , B64C2201/042 , B64C2201/108 , B64C2201/12 , B64C2201/141 , B64C2201/146 , B64C2201/162 , G09F9/30 , G09F9/33 , G09F21/10
Abstract: An unmanned aerial vehicle for providing digital messaging and observer interaction. The present invention relates to an unmanned aerial vehicle with displays attached thereto. In particular, an unmanned aerial display which is capable of flying under its own propulsion and power is programmed and/or controlled to deliver various content, messaging and advertising.
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107.发明授权公开(公告)号：US09919796B2
公开(公告)日：2018-03-20
申请号：US14908850
申请日：2014-08-07
Applicant: UNIT 1SRL
Inventor： Pietro Giovenga
CPC classification number: B64C29/0033 , B64C3/385 , B64C3/54 , B64C39/024 , B64C2201/021 , B64C2201/104 , B64C2201/108 , B64C2201/162 , B64D27/08 , Y02T50/14
Abstract: A convertiplane has the ability to take off like a helicopter and then fly horizontally like a conventional aircraft. The aircraft includes a variable incidence front wing of variable span located below the fuselage and mounted on a structure in the form of a venturi tube, a rear wing having two propellers for controlling the stability of the vehicle in pitch and roll installed therein, two counter-rotating, pivotally mounted ducted propellers equipped with four flaps orthogonal to each other provided on the sides of the cockpit, engines placed behind the cockpit close to the center of gravity, a static balancing system for controlling the center of gravity of the aircraft consisting of a weight placed in the lower part of the fuselage, self-propelled on the track rack longitudinally to the fuselage, and a digital flight control system.
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公开(公告)号：US09902494B2
公开(公告)日：2018-02-27
申请号：US15402784
申请日：2017-01-10
Applicant: MARTIN UAV, LLC
Inventor： Stephen Morris
CPC classification number: B64C29/02 , B64C11/001 , B64C39/024 , B64C2009/005 , B64C2201/021 , B64C2201/088 , B64C2201/162 , G05D1/0858 , G05D1/102
Abstract: 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 control the aircraft in a vertical flight mode, a horizontal flight mode, and transition the aircraft from the vertical flight mode to the horizontal flight mode.
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公开(公告)号：US09873508B2
公开(公告)日：2018-01-23
申请号：US15585743
申请日：2017-05-03
Applicant: Coriolis Games Corporation
Inventor： Jacob Apkarian
CPC classification number: B64C29/0033 , B64C27/20 , B64C27/52 , B64C39/024 , B64C2201/104 , B64C2201/108 , B64C2201/146 , B64C2201/162 , B64C2211/00 , B64F5/10
Abstract: An aerial vehicle is includes a wing, first and second rotors, and a movement sensor. The first and second multicopter rotors are rotatably coupled to the wing, the first multicopter rotor is rotatable relative to the wing about a first lateral axis, and the second multicopter rotor is rotatable relative to the wing about a second lateral axis. Each multicopter rotor is coupled to each other multicopter rotor, wherein the multicopter rotors are restricted to collective synchronous rotation relative to the wing between a multicopter configuration and a fixed-wing configuration. The movement sensor is coupled to the multicopter rotors, wherein the movement sensor is positioned to rotate relative to the wing when the multicopter rotors rotate relative to the wing between the multicopter and fixed-wing configurations.
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110.发明申请公开(公告)号：US20180009525A1
公开(公告)日：2018-01-11
申请号：US15071018
申请日：2016-03-15
Applicant: Selex Galileo Inc.
Inventor： Matthew Keegan , Stephen Leonard Engelson Wyatt
CPC classification number: B64C39/024 , B64C3/26 , B64C3/38 , B64C39/10 , B64C2201/021 , B64C2201/042 , B64C2201/121 , B64C2201/162 , G06F2221/2143 , H04K3/20
Abstract: A system and method for conducting electronic warfare on a target site includes the use of a small unmanned aircraft system (SUAS) having a fuselage and a Prandtl wing, wherein at least two electric ducted fans are positioned on the fuselage. A power system of the SUAS has a plurality of hydrogen fuel cells positioned within the Prandtl wing. An electronic warfare payload is carried by the fuselage, wherein the electronic warfare payload and the at least two electric ducted fans are powered by at least a portion of the plurality of hydrogen fuel cells. During an operation, the SUAS may launch near an IAD site and initiate an electronic warfare effect on an integrated air defense site with electronic warfare payload carried by the SUAS to interfere with at least one surface-to-air missile (SAM) system.
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