公开(公告)号：US20220380020A1

公开(公告)日：2022-12-01

申请号：US17745534

申请日：2022-05-16

申请人： AIRBUS HELICOPTERS

发明人： Guillaume RAYNAUD ,  Nicolas CALMES

IPC分类号： B64C13/02 ,  B64C1/00 ,  B64D35/08 ,  B64C27/00 ,  B64D45/08

摘要： A method for assisting the piloting of a rotorcraft including at least two engines capable of transmitting engine torque to at least one main rotor, the assistance method comprising the following steps: periodically determining a current position of the rotorcraft; making a first periodic comparison between the current position and a decision point; identifying an engine failure; making a second periodic comparison between the current position of the rotorcraft and a touchdown point; periodically determining an emergency landing profile, the emergency landing profile being generated at least depending on a result of the second periodic comparison; and periodically generating control orders to pilot the rotorcraft according to the emergency landing profile.

公开(公告)号：US11492110B2

公开(公告)日：2022-11-08

申请号：US16499690

申请日：2019-07-23

申请人： LG ELECTRONICS INC.

发明人： Seokhee Yi ,  Nakyeong Kim ,  Jeongkyo Seo ,  Kwangho An ,  Beomseok Chae

IPC分类号： B64C39/02 ,  H04W4/80 ,  B64D27/24 ,  B64D45/08 ,  B64D47/02 ,  B64D47/08 ,  G05D1/00 ,  H04W72/14

摘要： A station recognition and a landing method are disclosed. More specifically, an unmanned aerial robot includes a camera sensor configured to capture a first pattern that is marked on a station cover and is used for a station identification and a second pattern that is marked inside a station and is used for a precision landing; a transceiver configured to transmit and receive a radio signal; and a processor functionally connected to the camera sensor and the transceiver, wherein the processor is configured to determine a landing station for landing based on the first pattern captured by the camera sensor, control the transceiver to transmit a radio signal that indicates the landing station to open the station cover, and perform the precision landing at the landing station based on the second pattern of the landing station.

公开(公告)号：US20220348317A1

公开(公告)日：2022-11-03

申请号：US17731768

申请日：2022-04-28

申请人： Airbus Operations Limited ,  Airbus (SAS)

发明人： George HOWELL ,  Andrea LARUELO-FERNANDEZ

IPC分类号： B64C25/42 ,  B64D45/08 ,  B64D43/00

摘要： An aircraft landing event system including a processor communicatively coupled with memory storing aircraft landing event data. The processor is configured to receive environment information representative of an environmental condition of a runway approached by an aircraft and receive retardation information representative of a retardation demand of the aircraft during an anticipated landing event of the aircraft on the runway. The processor is further configured to select aircraft landing event data from the memory based on the environment information and the retardation information and determine a performance indicator for the landing event based on the aircraft landing event data selected by the processor. The processor is further configured to communicate the performance indicator to a landing system of the aircraft.

公开(公告)号：US20220340299A1

公开(公告)日：2022-10-27

申请号：US17859652

申请日：2022-07-07

申请人： HotaluX, Ltd.

发明人： Norimasa MIZOBE

IPC分类号： B64F1/20 ,  F21V29/503 ,  F21V29/51 ,  F21V29/71 ,  B64D45/08 ,  F21S10/06 ,  F21V5/04 ,  F21V15/01

摘要： A runway-embedded flash lighting device, includes a body configured to be embedded in a runway; a ceiling member including a flash emission window and disposed in an upper opening of the body and configured to be exposed to a runway surface when the body is embedded in the runway; a light guide member disposed in the flash emission window; an LED flash light source disposed inside the body and configured to emit a flash toward the light guide member; and a heat conducting member, wherein the light guide is configured to allow the flash emitted from the LED flash light source to be emitted from the flash emission window, the heat conducting member is disposed inside the body and includes a first part in contact with the LED flash light source, and a second part in contact with the ceiling member.

公开(公告)号：US11450219B2

公开(公告)日：2022-09-20

申请号：US16834241

申请日：2020-03-30

申请人： BOMBARDIER INC.

发明人： Olivier Lebegue ,  Benoit Ouellette

IPC分类号： G08G5/02 ,  B64D45/08 ,  G08G5/00

摘要： Methods and systems for assisting a pilot during flight of an aircraft are disclosed. The method includes receiving data indicative of a current location of the aircraft during flight and data indicative of a flight boundary, and determining that the flight boundary is relevant to the aircraft. The method also includes causing a display device to display a surface representing the flight boundary relative to the current location of the aircraft.

公开(公告)号：US11383858B2

公开(公告)日：2022-07-12

申请号：US17287604

申请日：2019-08-21

申请人： HotaluX, Ltd.

发明人： Norimasa Mizobe

IPC分类号： F21V29/503 ,  B64F1/20 ,  B64D45/08 ,  F21S10/06 ,  F21V15/01 ,  F21Y115/10 ,  F21W111/06

摘要： A runway-embedded flash lighting device includes: a body configured to be embedded in a runway; a ceiling member including a flash emission window, disposed in an upper opening of the body and configured to be exposed to a runway surface when the body is embedded in the runway; a light guide member disposed in the flash emission window; an LED flash light source disposed inside the body and configured to emit a flash toward the light guide member; and a bottom cover member disposed on and covering the lower opening of the body and including on an outer surface thereof on a side opposite to the body, a support portion protruding from the outer surface of the bottom cover member.

公开(公告)号：US11318859B2

公开(公告)日：2022-05-03

申请号：US15943581

申请日：2018-04-02

申请人： Asylon, Inc.

发明人： Damon C. Henry ,  Adam I. Mohamed ,  Brent McLaughlin ,  David Dones

IPC分类号： B60L53/80 ,  B64F1/00 ,  B64F1/20 ,  B60L53/36 ,  B60L53/35 ,  B64C39/02 ,  B64D45/08 ,  B64F1/12 ,  B64F1/36 ,  G05D1/06 ,  G05D1/00

摘要： A reconfigurable system capable of autonomously exchanging material from unmanned vehicles of various types and sizes. The system comprises an environmental enclosure, a landing area, a universal mechanical system to load and unload material from the unmanned vehicle, and a central processor that manages the aforementioned tasks. The landing area may comprise a one or more visible or non-visible markers/emitters capable of generating composite images to assist in landing the unmanned vehicle upon the reconfigurable, autonomous system.

公开(公告)号：US20210362876A1

公开(公告)日：2021-11-25

申请号：US16637393

申请日：2017-08-08

申请人： NEC CORPORATION

发明人： Tetsuo INOSHITA

IPC分类号： B64D45/08 ,  H04N5/765 ,  G06K9/00 ,  G06K9/62 ,  G06T7/20 ,  H04N5/91 ,  G06K9/46 ,  G08G5/02 ,  B64D47/08 ,  G05D1/10 ,  G05D1/08

摘要： To more reliably land a flying body at a desired point, a flying body includes a determiner that determines whether the flying body is taking off and ascending from a takeoff point or descending to land, a camera mounted in the flying body, a recorder that records a lower image captured by the camera if it is determined that the flying body is taking off and ascending and a guider that, if it is determined that the flying body is descending to land, guides the flying body to the takeoff point while descending using a lower image recorded in the recorder during takeoff/ascent and a lower image captured during the descent.

公开(公告)号：US11167862B2

公开(公告)日：2021-11-09

申请号：US16319665

申请日：2017-01-01

申请人： Ahmed Hassan Fouad Ahmed Mostafa

发明人： Ahmed Hassan Fouad Ahmed Mostafa

IPC分类号： B64D45/08 ,  B64D45/00 ,  B64D47/08 ,  G07C5/00 ,  G07C5/08

摘要： It is an integrated system that (RECORD) registers the events on the plane (video/audio) and stored on the hard disk to get to know the truth of what happened on the aircraft in emergency situations and disasters and we can also get a live broadcasting of the events WHILE THE FLIGHT in an emergency by using (wifi) satellite internet or data over hf (wbhf) technology with ad hoc.

公开(公告)号：US20210276728A1

公开(公告)日：2021-09-09

申请号：US17179957

申请日：2021-02-19

申请人： HONEYWELL INTERNATIONAL INC.

发明人： Michael Mast ,  Yuta Morioka ,  Martin Jezek ,  Jeffrey Glenn

IPC分类号： B64D45/00 ,  G08G5/02 ,  G08G5/00 ,  B64D43/02 ,  B64D45/08 ,  G05D1/10

摘要： Flight guidance systems and methods that provide an airport selection in response to an EO condition in a single engine plane. The airport selection takes into consideration factors such as optimal approach type, runway length, weather, terrain, remaining battery time, and the like. Additionally, various also generate and display a visual indication of a remaining glide range when the EO condition is happening; the remaining glide range determination is based, at least in part, on terrain.