公开(公告)号：EP3378018A1

公开(公告)日：2018-09-26

申请号：EP16798217.2

申请日：2016-11-21

Applicant: Ocado Innovation Limited

Inventor： CLARKE, Paul ,  INGRAM-TEDD, Andrew, John

IPC: G06Q10/08 ,  G06Q50/28

CPC classification number: G06Q10/087 ,  A47G29/14 ,  A47G29/141 ,  B60P3/007 ,  G01C21/3453 ,  G05D1/0094 ,  G05D1/0202 ,  G05D1/021 ,  G06Q10/08 ,  G06Q10/083 ,  G06Q30/0207 ,  G06Q50/28

Abstract: An autonomous delivery device can make unattended deliveries of customer orders to predetermined locations. The device includes a plurality of compartments containing portions of the order or all of the order or a number of separately deliverable orders. The device includes a compartment opening such that on arrival at the predetermined location the contents of the or each compartment may be automatically dispensed.

公开(公告)号：EP3306432A4

公开(公告)日：2018-06-20

申请号：EP16799373

申请日：2016-05-27

Applicant: XIAOMI INC

Inventor： ZHANG PENGFEI ,  CAI WEI ,  XIA YONGFENG ,  YE HUALIN

IPC: G05D1/10 ,  B64C39/02 ,  G05D1/00

CPC classification number: B64C39/024 ,  G05D1/0011 ,  G05D1/0016 ,  G05D1/0033 ,  G05D1/0038 ,  G05D1/0202

Abstract: The embodiments of the present disclosure relate to a flight control method and apparatus, and an electronic device. The method includes: a relative position relationship between an aircraft and a control device is determined; a polar coordinate system with the control device as an origin is determined according to the relative position relationship; a flight direction control instruction sent by the control device is received, the flight direction control instruction being generated on the basis of the polar coordinate system; and according to coordinate information about the aircraft in the polar coordinate system, the aircraft is driven to fly in accordance with the flight direction control instruction.

公开(公告)号：EP3201711A4

公开(公告)日：2018-06-20

申请号：EP15846360

申请日：2015-09-30

Applicant: SIKORSKY AIRCRAFT CORP

Inventor： LUSZCZ MATTHEW T ,  EADIE WILLIAM J ,  ELLER EREZ ,  LEONE ADAM

IPC: G05D1/08

CPC classification number: B64C27/82 ,  B64C1/0009 ,  B64C7/00 ,  B64C11/48 ,  B64C11/50 ,  B64C13/04 ,  B64C13/18 ,  B64C13/50 ,  B64C13/503 ,  B64C19/00 ,  B64C27/001 ,  B64C27/008 ,  B64C27/08 ,  B64C27/10 ,  B64C27/12 ,  B64C27/14 ,  B64C27/16 ,  B64C27/32 ,  B64C27/322 ,  B64C27/33 ,  B64C27/467 ,  B64C27/473 ,  B64C27/48 ,  B64C27/51 ,  B64C27/52 ,  B64C27/54 ,  B64C27/57 ,  B64C27/78 ,  B64C27/80 ,  B64C2027/004 ,  B64C2027/8209 ,  B64C2027/8227 ,  B64C2027/8236 ,  B64C2027/8263 ,  B64C2027/8272 ,  B64C2027/8281 ,  B64C2201/024 ,  B64D35/06 ,  B64D39/00 ,  B64D39/06 ,  B64D45/02 ,  B64D2045/0085 ,  F02C9/28 ,  F05D2220/329 ,  F05D2270/021 ,  F16D13/52 ,  F16D13/72 ,  F16D13/74 ,  F16H37/02 ,  G05D1/0077 ,  G05D1/0202 ,  G05D1/0204 ,  G05D1/08 ,  G05D1/0816 ,  G05D1/0858 ,  G06F19/00

Abstract: A method of controlling a rotary wing aircraft includes accelerating the aircraft in a fore direction independently of cyclic control of the main rotor and pitch of the aircraft.

公开(公告)号：EP3201084A4

公开(公告)日：2018-06-13

申请号：EP15847201

申请日：2015-09-30

Applicant: SIKORSKY AIRCRAFT CORP

Inventor： KOESSICK MAXIMILIAN AUGUST ,  KOSTOSS MICHAEL J ,  NUSSENBLATT ERIC LUCIEN ,  THOMAS JUSTIN ,  BUTLER CHRIS PAUL ,  CERGE BRANDON MICHAEL

IPC: B64C27/10

CPC classification number: B64C27/82 ,  B64C1/0009 ,  B64C7/00 ,  B64C11/48 ,  B64C11/50 ,  B64C13/04 ,  B64C13/18 ,  B64C13/50 ,  B64C13/503 ,  B64C19/00 ,  B64C27/001 ,  B64C27/008 ,  B64C27/08 ,  B64C27/10 ,  B64C27/12 ,  B64C27/14 ,  B64C27/16 ,  B64C27/32 ,  B64C27/322 ,  B64C27/33 ,  B64C27/467 ,  B64C27/473 ,  B64C27/48 ,  B64C27/51 ,  B64C27/52 ,  B64C27/54 ,  B64C27/57 ,  B64C27/78 ,  B64C27/80 ,  B64C2027/004 ,  B64C2027/8209 ,  B64C2027/8227 ,  B64C2027/8236 ,  B64C2027/8263 ,  B64C2027/8272 ,  B64C2027/8281 ,  B64C2201/024 ,  B64D35/06 ,  B64D39/00 ,  B64D39/06 ,  B64D45/02 ,  B64D2045/0085 ,  F02C9/28 ,  F05D2220/329 ,  F05D2270/021 ,  F16D13/52 ,  F16D13/72 ,  F16D13/74 ,  F16H37/02 ,  G05D1/0077 ,  G05D1/0202 ,  G05D1/0204 ,  G05D1/08 ,  G05D1/0816 ,  G05D1/0858 ,  G06F19/00

Abstract: A method of controlling a rotary wing aircraft includes accelerating the aircraft in a fore direction independently of cyclic control of the main rotor and pitch of the aircraft.

公开(公告)号：EP3201082A4

公开(公告)日：2018-03-28

申请号：EP15846472

申请日：2015-09-29

Applicant: SIKORSKY AIRCRAFT CORP

Inventor： HUNTER DAVID H ,  CHASEN SCOTT A ,  CERGE BRANDON MICHAEL ,  KOESSICK MAXIMILIAN AUGUST ,  KOSTOSS MICHAEL J ,  NUSSENBLATT ERIC LUCIEN ,  THOMAS JUSTIN ,  BUTLER CHRISTOPHER P

IPC: B64C27/10

CPC classification number: B64C27/82 ,  B64C1/0009 ,  B64C7/00 ,  B64C11/48 ,  B64C11/50 ,  B64C13/04 ,  B64C13/18 ,  B64C13/50 ,  B64C13/503 ,  B64C19/00 ,  B64C27/001 ,  B64C27/008 ,  B64C27/08 ,  B64C27/10 ,  B64C27/12 ,  B64C27/14 ,  B64C27/16 ,  B64C27/32 ,  B64C27/322 ,  B64C27/33 ,  B64C27/467 ,  B64C27/473 ,  B64C27/48 ,  B64C27/51 ,  B64C27/52 ,  B64C27/54 ,  B64C27/57 ,  B64C27/78 ,  B64C27/80 ,  B64C2027/004 ,  B64C2027/8209 ,  B64C2027/8227 ,  B64C2027/8236 ,  B64C2027/8263 ,  B64C2027/8272 ,  B64C2027/8281 ,  B64C2201/024 ,  B64D35/06 ,  B64D39/00 ,  B64D39/06 ,  B64D45/02 ,  B64D2045/0085 ,  F02C9/28 ,  F05D2220/329 ,  F05D2270/021 ,  F16D13/52 ,  F16D13/72 ,  F16D13/74 ,  F16H37/02 ,  G05D1/0077 ,  G05D1/0202 ,  G05D1/0204 ,  G05D1/08 ,  G05D1/0816 ,  G05D1/0858 ,  G06F19/00

Abstract: An aircraft is provided including an airframe, an extending tail, and a counter rotating, coaxial main rotor assembly including an upper rotor assembly with an upper blade and a lower rotor assembly with a lower blade. A first antenna in one of upper blade and the lower blade, and a second antenna in the other of the upper blade and the lower blade. An oscillator to apply an excitation signal to the first antenna. A blade proximity monitor to monitor a magnitude of the excitation signal and an output signal from the second antenna to determine a distance between the upper blade and the lower blade.

公开(公告)号：EP3201085A4

公开(公告)日：2018-03-21

申请号：EP15846784

申请日：2015-09-25

Applicant: SIKORSKY AIRCRAFT CORP

Inventor： ELLER EREZ ,  LUSZCZ MATTHEW T ,  EADIE WILLIAM J ,  WEINER STEVEN D

IPC: B64C27/22

CPC classification number: B64C27/82 ,  B64C1/0009 ,  B64C7/00 ,  B64C11/48 ,  B64C11/50 ,  B64C13/04 ,  B64C13/18 ,  B64C13/50 ,  B64C13/503 ,  B64C19/00 ,  B64C27/001 ,  B64C27/008 ,  B64C27/08 ,  B64C27/10 ,  B64C27/12 ,  B64C27/14 ,  B64C27/16 ,  B64C27/32 ,  B64C27/322 ,  B64C27/33 ,  B64C27/467 ,  B64C27/473 ,  B64C27/48 ,  B64C27/51 ,  B64C27/52 ,  B64C27/54 ,  B64C27/57 ,  B64C27/78 ,  B64C27/80 ,  B64C2027/004 ,  B64C2027/8209 ,  B64C2027/8227 ,  B64C2027/8236 ,  B64C2027/8263 ,  B64C2027/8272 ,  B64C2027/8281 ,  B64C2201/024 ,  B64D35/06 ,  B64D39/00 ,  B64D39/06 ,  B64D45/02 ,  B64D2045/0085 ,  F02C9/28 ,  F05D2220/329 ,  F05D2270/021 ,  F16D13/52 ,  F16D13/72 ,  F16D13/74 ,  F16H37/02 ,  G05D1/0077 ,  G05D1/0202 ,  G05D1/0204 ,  G05D1/08 ,  G05D1/0816 ,  G05D1/0858 ,  G06F19/00

Abstract: An aircraft is provided including an airframe, an extending tail, and a counter rotating, coaxial main rotor assembly including an upper rotor assembly with an upper blade and a lower rotor assembly with a lower blade. A first antenna in one of upper blade and the lower blade, and a second antenna in the other of the upper blade and the lower blade. An oscillator to apply an excitation signal to the first antenna. A blade proximity monitor to monitor a magnitude of the excitation signal and an output signal from the second antenna to determine a distance between the upper blade and the lower blade.

公开(公告)号：EP3170166A1

公开(公告)日：2017-05-24

申请号：EP15750127.1

申请日：2015-07-17

Applicant: The University Of Malta ,  Quaero Ltd.

Inventor： CHIRCOP, Kenneth ,  ZAMMIT-MANGION, David ,  MUSCAT, Alan

IPC: G08G5/00 ,  G01C23/00

CPC classification number: G08G5/0039 ,  G01C23/00 ,  G01C23/005 ,  G05D1/0202 ,  G08G5/0008 ,  G08G5/0013 ,  G08G5/0021 ,  G08G5/0026 ,  G08G5/0034

Abstract: A method and system and tools for optimizing an aircraft flight trajectory that determine an advantageous flight profile that takes into account developing operational conditions, air traffic constraints and aircraft performance in a timely manner that can allow tactical flight plan changes to be incorporated without unduly introducing operational or financial penalties to the operator.

Abstract translation: 一种用于优化飞机飞行轨迹的方法，系统和工具，其确定有利的飞行剖面，其以适时的方式考虑到发展中的操作条件，空中交通限制和飞机性能，其可以允许并入战术飞行计划变更而不过度地引入操作 或对经营者的经济处罚。

公开(公告)号：EP3089632A1

公开(公告)日：2016-11-09

申请号：EP14837087.7

申请日：2014-12-31

Applicant: Blacknight Holdings, LLC

Inventor： WALSH, Ryan ,  FALESCH, Alexander J.

IPC: A47G29/14

CPC classification number: B64F1/32 ,  A01M29/16 ,  A47G29/14 ,  B64C39/024 ,  B64C2201/027 ,  B64C2201/128 ,  B64C2201/145 ,  B64F1/04 ,  G05D1/0202

Abstract: A landing pad receives and stores packages delivered from an aerial vehicle are awaiting pickup from an aerial vehicle. The landing pad can be placed outside of a window and can contain a transmitter for sending out an identification signal via radio frequency to aid aerial vehicles in finding the landing pad. The landing pad contains a landing platform with a trapdoor that leads to a storage compartment. The trapdoor can be configured to only open when it receives a signal from an authorized aerial vehicle. The storage compartment can be accessed via a storage compartment door which can contain a locking mechanism. The storage compartment can be climate controlled. The landing pad can also have a transmitter that emits sounds to discourage animals from nesting on or near the landing pad. The landing pad can also include a solar power generator as a source of electrical energy.

公开(公告)号：EP2909689B1

公开(公告)日：2016-10-05

申请号：EP13785582.1

申请日：2013-10-22

Applicant: BCB International Limited ,  Torquing Group Ltd.

Inventor： REEDMAN, Ivan ,  DAVIES, Barry

IPC: G05D1/10

CPC classification number: B64C39/024 ,  B64C19/00 ,  B64C39/028 ,  B64C2201/00 ,  B64C2201/14 ,  B64C2201/141 ,  B64C2230/00 ,  B64C2230/02 ,  G01S15/06 ,  G01S15/88 ,  G01S15/89 ,  G01S15/8913 ,  G01S15/8929 ,  G01S15/8993 ,  G01S15/93 ,  G05D1/0088 ,  G05D1/0202 ,  G05D1/101 ,  G05D1/102 ,  Y10S367/909

公开(公告)号：EP3032518A3

公开(公告)日：2016-06-29

申请号：EP15195782.6

申请日：2015-11-23

Applicant: The Boeing Company

Inventor： SCHARL, Julien Emile Sebastien ,  MYERS, David M. ,  HARALDSDOTTIR, Aslaug

IPC: G08G5/00 ,  G08G5/02

CPC classification number: G08G5/0039 ,  G01C21/20 ,  G05D1/0202 ,  G05D1/0808 ,  G08G5/0021 ,  G08G5/0047 ,  G08G5/0052 ,  G08G5/025

Abstract: A method and apparatus of turning an aircraft for interval management. Interval management information identifying a desired spacing between the aircraft and a target aircraft is received. Turn information is determined using a performance gain factor. The turn information identifies a turn point for the aircraft. The performance gain factor identifies a desired portion of achieving the desired spacing due to turning the aircraft at the turn point and a desired portion of achieving the desired spacing due to changing speed of the aircraft. The turn information is used to turn the aircraft at the turn point.