-
公开(公告)号：WO2023091235A2
公开(公告)日：2023-05-25
申请号：PCT/US2022/044730
申请日：2022-11-22
申请人： BETA AIR, LLC
摘要： The present invention is a system and methods for preconditioning a power source of an electric aircraft. The system may include a sensor attached to a power source of an electric aircraft, where the sensor is configured to detect a condition datum of an operating component of the power source, and a flight controller communicatively connected to the sensor, the flight controller configured to determine if there is a divergent element of an operating state of the power source and, if so, initiate a power source modification to correct the divergent element.
-
公开(公告)号：WO2023067651A1
公开(公告)日：2023-04-27
申请号：PCT/JP2021/038413
申请日：2021-10-18
申请人： 日本電信電話株式会社
摘要： 飛行体（Ｖ１）とプラットホーム（５１）との離間距離を検出する距離取得部（１１５）と、駆動バッテリ（１６）の残量を取得する残量取得部（１１３）と、通信部（１２）で受信される受信信号の電波強度を取得する電波強度取得部（１１４）と、駆動バッテリ（１６）の残量が、離間距離により決められる下限残量を下回った場合、及び電波強度が下限強度を下回った場合、の少なくとも一方の場合に飛行体（Ｖ１）をプラットホーム（５１）に帰還させる制御を行う帰還制御部（１１２）と、を備える。
-
公开(公告)号：WO2023064188A1
公开(公告)日：2023-04-20
申请号：PCT/US2022/046110
申请日：2022-10-07
摘要： The disclosed invention describes a method for determining a current state of a gas cell in an airship, particularly the lift. A computing device receives depth measurements of the interior of the gas cell using a lidar sensor positioned outside the cell and uses these depth measurements to create a mesh, segment a space within the mesh into geometric shapes, calculate the volume of the shapes, and use the calculated volume to estimate the total volume of the space within the mesh, representing the volume of gas within the gas cell. The computing device then uses the estimated volume to calculate the lift of the gas cell and sends the calculated lift to a control module of the airship.
-
公开(公告)号：WO2023057198A1
公开(公告)日：2023-04-13
申请号：PCT/EP2022/076011
申请日：2022-09-20
IPC分类号： B64D45/00 , H02J50/12 , H02J50/80 , B64D2045/001 , B64D45/0005 , G01M13/023
摘要： A signal transmitter apparatus configured for use in an aircraft moveable element monitoring system. The signal transmitter apparatus comprising a signal transmitter circuit. The signal transmitter circuit comprises: a first electrical path between a voltage input and a first node, the first electrical path comprising an inductor; a second electrical path between the first node and a second node, the second electrical path comprising a signal transmitter coil and a first capacitor, wherein the signal transmitter coil is electrically connected in series with the first capacitor; a third electrical path between the first node and the second node, the third electrical path comprising a second capacitor, such that the second capacitor is electrically connected in parallel to the signal transmitter coil and the first capacitor; and a fourth electrical path between the second node and the voltage input.
-
公开(公告)号：WO2023274914A1
公开(公告)日：2023-01-05
申请号：PCT/EP2022/067485
申请日：2022-06-27
发明人： FLEDDERMANN, Andreas , VAN BRUGGEN, Jan Arend , KOHLÖFFEL, Christian , HARTMANN, Tobias , VAN BALEN, Elko
IPC分类号： B64C13/50 , B64D45/00 , B64F5/60 , B64C13/40 , B64D2045/0085
摘要： In order to reduce maintenance work and to improve long-time reliability, the invention provides a health monitoring method for checking a functionality of a flight control surface driving apparatus (104) using at least one load sensor (110) for sensing a load imposed on a control surface drive device (106), the method comprising at least one of the steps: a) blocking movement of the transmission device (108) by means of a brake device (118), b) commanding the control surface drive device (106) to apply a load on the blocked transmission device (108), and c) determining whether at least one load sensor output signal (62) of the at least one load sensor (110) is within a predetermined range. Further, a flight control surface drive apparatus (104), a flight control system (100) and an aircraft (10) comprising a control device (112) configured to automatic command conduct of such health monitoring method are described.
-
公开(公告)号：WO2023272489A1
公开(公告)日：2023-01-05
申请号：PCT/CN2021/103134
申请日：2021-06-29
申请人： 深圳市大疆创新科技有限公司
摘要： 一种螺旋桨及无人飞行器，其中，螺旋桨包括桨毂(10)；桨叶(20)，与所述桨毂(10)连接，所述桨叶(20)包括与所述桨毂(10)连接的连接端，以及远离所述桨毂(10)的末端；桨叶保护装置(30)，至少部分包围所述桨叶(20)的末端，且所述桨叶保护装置(30)能够跟随所述桨叶(20)同步转动。本技术方案提供的螺旋桨及无人飞行器，能够有效防止桨叶的末端划伤用户或者末端撞击到其他物体，提高了无人飞行器的使用安全性。
-
公开(公告)号：WO2022263365A1
公开(公告)日：2022-12-22
申请号：PCT/EP2022/066008
申请日：2022-06-13
申请人： OTONOMY AVIATION
摘要： L'invention concerne un système embarqué de détection d'impacts sur le fuselage (110) d'un aéronef (100), comportant : une pluralité de capteurs d'impact (2) disposés sur une pluralité de zones du fuselage, chaque capteur (2) étant apte à détecter un impact sur le fuselage (110) au niveau de sa position, un module de détection (5) d'un véhicule au voisinage de l'aéronef, le module de détection étant apte à estimer la vitesse d'un véhicule détecté, et un calculateur (4) agencé pour, lors de la détection d'un impact sur le fuselage par un capteur d'impact, enregistrer dans une mémoire du système embarqué une information relative à la vitesse d'un véhicule détecté par le module de détection.
-
公开(公告)号：WO2022217262A1
公开(公告)日：2022-10-13
申请号：PCT/US2022/071607
申请日：2022-04-07
发明人： BUDAMPATI, Ramakrishna , ROLCHIGO, Philip , KHADILKAR, Mohan , TANNER, John , BROWN, Edward , DZINDO, Azur
IPC分类号： G01M99/00 , B64F5/60 , F15B19/00 , F04D15/00 , F04D29/66 , B64D45/00 , F04B49/00 , F04B49/06
摘要： A pump health monitoring system is provided. Such a system includes one or a plurality of data capture devices that together collect a multiple variable data set relating to a device being monitored such as a water pump device for a pool or spa and/or an underwater submerged pump device. A programmable processor receives the multiple variable data set, retrieves a set of processing rules that are specific to the identity of the pump and processes the operating details with the set of processing rules to identify a current operational status or health status of the device.
-
公开(公告)号：WO2022154429A1
公开(公告)日：2022-07-21
申请号：PCT/KR2022/000465
申请日：2022-01-11
摘要： 본 발명은 강, 바다, 호수와 같은 수상에 설치되어 수시로 위치가 변동되는 수상 부유식 태양광 발전소에 설치된 태양광 패널의 고장 진단에 필요한 드론 비행경로 정보를 수상 부유식 태양광 발전소의 위치 변동에 상관없이 자동으로 생성하는 수상 부유식 태양광 패널 진단용 드론 비행경로 정보 생성 방법에 관한 발명으로서, 1 단계(S100), 제2 단계(S200), 제3 단계(S300), 제4 단계(S400), 제5 단계(S500), 제6 단계(S600), 제7 단계(S700)를 포함하는 것을 특징으로 한다.
-
">
公开(公告)号：WO2022130334A1
公开(公告)日：2022-06-23
申请号：PCT/IB2021/061957
申请日：2021-12-17
发明人： BALDI, Andrea , MARIANI, Ugo , MEZZANZANICA, Daniele , TANELLI, Mara , ZINNARI, Francesco , CORAL, Giovanni , BRAGHIN, Francesco , CAZZULANI, Gabriele
摘要： Method implemented through a computer (12) for detecting the execution, by an aircraft (3), of a manoeuvre belonging to a macrocategory among a plurality of macrocategories (MC), including: receiving a data structure (205) with a plurality of time series of values of quantities relating to a flight of the aircraft (3); for each time duration (TW'p) among a plurality of predetermined time durations (TW'), selecting (310) a corresponding subset of the data structure (205) and extracting (320) a corresponding feature vector (FVXkp); on the basis of the feature vectors (FVXkp), generating (330,335;500,510;720;820) a corresponding input macrovector (MPVX'k; MPVX"k, MPVX'''k; MFVXk) and applying (338;520;730;830) to the input macrovector (MPVX'k," MPVX"k, MPVX'''k;MFVXk) an output classifier (151;251;561;721) to generate estimates indicative of the probability that the aircraft (3) was performing manoeuvres belonging to the macrocategories (MC).
-
-
-
-
-
-
-
-
-
搜索结果
768 条记录 (耗时 0.035 秒)
