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1. 发明申请

WO2015054449A1 METHOD FOR EXPANDING AIRCRAFT CENTER OF GRAVITY LIMITATIONS 审中-公开
标题翻译：扩大航空器重心限制中心的方法
公开(公告)号：WO2015054449A1
公开(公告)日：2015-04-16
申请号：PCT/US2014/059821
申请日：2014-10-09
申请人： NANCE, C., Kirk
发明人： NANCE, C., Kirk
IPC分类号： G01G19/07
CPC分类号： G01M1/125 , B64D45/00 , B64D2045/008
摘要： A method which creates a justification basis to expand an aircraft's (1) Center of Gravity (27) limitations, which are established by the aircraft designer; relating to aircraft landing gear strength assumptions. Strut load sensors such as pressure sensors (79) are mounted in relation to each of the landing gear struts to monitor, measure and record aircraft landing gear strut compression loads. A history of measured, landing gear load values is compiled and related to any assumed landing gear loads, which define the life-cycle limit of the landing gear, allowing relief from existing aircraft Center of Gravity limitation caused by landing gear strength assumptions to further expanded CG Limitations beyond current limits, based on measured landing gear loads.
摘要翻译：一种为航空器设计人员建立的（1）重心（27）限制而扩展飞机的理由的方法; 涉及飞机起落架强度假设。支撑负载传感器（例如压力传感器（79））相对于每个起落架支柱安装以监测，测量和记录飞机起落架支柱压缩载荷。测量的起落架载荷值的历史编纂并与任何假定的起落架载荷相关联，这些起落架载荷限定了起落架的生命周期限制，从而可以减轻起落架强度假设造成的现有飞机重心限制中心进一步扩大基于测量的起落架载荷，超出限制的CG限制。

2. 发明申请

WO01092836A1 AUTOMATIC FLAT RATE SETTING SYSTEM FOR FREIGHT FEEDER AIRCRAFT AND METHOD OF SETTING OF ENGINE FLAT RATE 审中-公开
标题翻译：用于货物进给机的自动平均速度设定系统及发动机平均速比设定方法
公开(公告)号：WO01092836A1
公开(公告)日：2001-12-06
申请号：PCT/US2001/017200
申请日：2001-05-29
IPC分类号： G01G19/07 , G01G19/415
CPC分类号： G01G19/415 , G01G19/07
摘要： A system and method of automatically setting a flat rate engine power setting of an aircraft determines the weight of loaded cargo containers to determine the total gross weight of the aircraft prior to take-off, determines, from the total gross weight, the required flat rate engine power for the aircraft, such as by inputting the stored value into a look-up table, and automatically sets the flat rate setting of the aircraft's engines to correspond to the determined required engine power, prior to take-off, by sending the obtained required flat rate engine power as a command signal to an engine control system.
摘要翻译：自动设定飞机的平衡发动机功率设定的系统和方法确定装载货物集装箱的重量，以确定起飞前飞机的总重量，从总毛重确定所需的统一费率例如通过将存储的值输入到查找表中，并且在起飞之前通过发送所获得的飞行器的引擎来自动设置飞机发动机的统一速率设置以对应于所确定的所需发动机功率所需的发动机功率作为发动机控制系统的指令信号。

3. 发明申请

WO01090707A1 METHOD OF PRE-PLANNING THE LOADING OF AIRCRAFT 审中-公开
标题翻译：预先规划飞机装载的方法
公开(公告)号：WO01090707A1
公开(公告)日：2001-11-29
申请号：PCT/US2001/040376
申请日：2001-03-26
IPC分类号： B64D9/00 , G01G19/07 , G01M1/12
CPC分类号： B64D9/00 , G01G19/07 , G01M1/125 , Y02T50/46
摘要： A method of pre-planning and loading of aircraft before physically loading pallets on the aircraft is disclosed. An identifier (28) is entered into a processor (22) to identify an aircraft to be loaded. Based on the identifier (28), a data file relating to the loading limitations of the aircraft to be loaded is retrieved from the database (30). Data regarding the amount of fuel upon departure is entered, as well as the weights of pallets to be loaded into pallet positions. A user selects a first option for calculating within the processor the optimum location of pallets and pallet positions to obtain the optimum center of gravity balance of the aircraft, or the user selects a second option for determining if the center of gravity of the aircraft based on the entered location of pallets and pallet positions are within the center of gravity limits of the aircraft.
摘要翻译：披露了在飞机上物理装载托盘之前预先规划和装载飞机的方法。将标识符（28）输入到处理器（22）中以识别要加载的飞行器。基于标识符（28），从数据库（30）检索与要加载的飞机的加载限制有关的数据文件。输入关于出发时的燃料量的数据，以及要装载到托盘位置的托盘的重量。用户选择用于在处理器内计算托盘和托盘位置的最佳位置以获得飞行器的最佳重心平衡的第一选项，或者用户选择第二选项来确定飞机的重心是否基于托盘和托盘位置的输入位置在飞机的重心极限的范围内。

4. 发明申请

WO2018000087A1 LOCATION FOR UNMANNED AERIAL VEHICLE LANDING AND TAKING OFF 审中-公开
标题翻译：无人机空中着陆和停飞的位置
公开(公告)号：WO2018000087A1
公开(公告)日：2018-01-04
申请号：PCT/CA2017/050777
申请日：2017-06-27
申请人： DRONE DELIVERY CANADA CORP.
发明人： DI BENEDETTO, Paul , COLACITTI, Gregory
IPC分类号： B64F1/32 , B64F1/22 , E01F13/00 , E04H6/44 , G01G19/07
摘要： An unmanned aerial vehicle (UAV) system, location and method, for operation with a flight management system, has a controlled access UAV zone for at least one of: UAV landing, UAV loading, and UAV take-off. A sensor can be in communication with a control panel and/or a lock to govern access to the UAV zone. The zone can have a barrier with closure secured by the lock, and controlled by a flight management system. Separate access codes can be provided for departure and destination locations, to enable personnel associated with a delivery request to access those locations, to effect delivery of an article. The codes can be generated and supplied when the flight management system receives a valid delivery request.
摘要翻译：用于与飞行管理系统一起操作的无人飞行器（UAV）系统，位置和方法具有用于以下至少一项的受控进入无人机区域：无人机着陆，无人机装载和无人机取出 -off。传感器可以与控制面板和/或锁进行通信以管理对无人机区域的访问。该区域可以有一个关闭的障碍物，并由飞行管理系统控制。可以为出发地和目的地提供单独的访问代码，以使与交付请求相关联的人员能够访问这些地点，以实现物品的交付。这些代码可以在飞行管理系统收到有效的送达请求时生成和提供。

5. 发明申请

WO2015106408A1 MANAGING A DISTRIBUTION OF A PAYLOAD FOR A FLIGHT 审中-公开
标题翻译：管理飞行员付费的分配
公开(公告)号：WO2015106408A1
公开(公告)日：2015-07-23
申请号：PCT/CN2014/070659
申请日：2014-01-15
申请人： HEWLETT-PACKARD DEVELOPMENT COMPANY, L.P. , CREACY, Chet R. , JAYAPAL, Anthony Samy , COLEGROVE, Matthew , CUI, Hao , EVANS, John Martin , BANNING, David Brook , MCHODGKINS, Don , THANIKACHALAM, Rammohan , RANGEEN, Carrie , TRUITT, Laura C. , GOULD, David Woodman , PEREZ, David , SCRIFFINY, Mark J. , DAUM, Michelle Lynn Hill
发明人： CREACY, Chet R. , JAYAPAL, Anthony Samy , COLEGROVE, Matthew , CUI, Hao , EVANS, John Martin , BANNING, David Brook , MCHODGKINS, Don , THANIKACHALAM, Rammohan , RANGEEN, Carrie , TRUITT, Laura C. , GOULD, David Woodman , PEREZ, David , SCRIFFINY, Mark J. , DAUM, Michelle Lynn Hill
IPC分类号： G01G19/07
CPC分类号： G01G19/07
摘要： Managing a payload distribution for a flight includes specifying a flight with a payload distribution to be managed, obtaining, based on a flight timed event, historical payload data to determine a maximum takeoff weight limit for the flight, retrieving, based on the flight timed event, all planned payload values to determine an estimated takeoff weight for the flight, and obtaining, based on the flight timed event, actual payload values to manage the distribution of the payload for the flight.
摘要翻译：管理航班的有效载荷分配包括指定具有要管理的有效载荷分布的飞行，基于飞行定时事件获得历史有效载荷数据，以确定飞行的最大起飞重量限制，基于飞行定时事件检索，所有计划的有效载荷值以确定飞行的估计起飞重量，并且基于飞行时间事件获得实际有效载荷值以管理飞行的有效载荷的分布。

6. 发明申请

WO2015019068A1 METHOD AND APPARATUS FOR DETERMINING THE MASS OF A BODY 审中-公开
标题翻译：用于确定身体质量的方法和装置
公开(公告)号：WO2015019068A1
公开(公告)日：2015-02-12
申请号：PCT/GB2014/052382
申请日：2014-08-04
申请人： LACSOP LIMITED , MORRIS, Gordon A
发明人： MORRIS, Gordon A
IPC分类号： G01G19/07 , G06F15/18
CPC分类号： G01G19/07 , G01G9/00 , G01G19/086
摘要： A method for determining the mass of a body is described. The method comprises the application and measurement of a first motive force to the body to move the body in a first state of motion. The acceleration of the body is also measured at this time. This methodology is repeated for a second state of motion. The measured motive forces and accelerations are then used to calculate the mass, and hence the weight of the body. An accelerometer may be employed to measure the accelerations. The methods may be adapted so as to correct for the angle θ of the ground across which the body is moved and or the tilt angle α of the accelerometer relative to the ground. The methods may employ a novel surface angle measuring device that does not require contact with the ground and which does not require the body to be stationary.
摘要翻译：描述了用于确定身体质量的方法。该方法包括向身体施加和测量第一动力以使身体在第一运动状态下移动。此时也测量身体的加速度。对于第二运动状态重复该方法。然后测量的动力和加速度用于计算体重，从而计算身体的重量。可以使用加速度计来测量加速度。这些方法可以被调整以便校正角度和角度; 身体移动的地面和加速度计相对于地面的倾斜角α。这些方法可以采用新颖的表面角度测量装置，其不需要与地面接触并且不需要身体静止。

7. 发明申请

WO2006074908A1 VORRICHTUNG UND VERFAHREN ZUR KONTROLLE DES BE- UND/ODER ENTLADEPROZESSES EINES FLUGZEUGS 审中-公开
标题翻译：装置和方法用于检查装载和/或飞机放电过程
公开(公告)号：WO2006074908A1
公开(公告)日：2006-07-20
申请号：PCT/EP2006/000174
申请日：2006-01-11
申请人： RHEINMETALL DEFENCE ELECTRONICS GMBH , TIETJEN, Ronald , EILTS, Torsten , ZISCHOW, Ekkehard , PALUBITZKI, Norbert
发明人： TIETJEN, Ronald , EILTS, Torsten , ZISCHOW, Ekkehard , PALUBITZKI, Norbert
IPC分类号： G01M1/12 , G01G19/07 , B64D9/00
CPC分类号： B64D9/00 , G01G19/07 , G01G23/3728 , G01M1/125
摘要： Die Erfindung betrifft eine Vorrichtung sowie ein Verfahren zur Kontrolle des Be- und/oder Entladeprozesses eines Flugzeugs, wobei ein in das Flugzeug eingebrachtes Frachtstück identifiziert wird, dem Frachtstück ein Gewicht zugeordnet wird, die Position des Frachtstücks innerhalb des Flugzeugs verfolgt wird und das Gesamtgewicht und/oder der Schwerpunkt des Flugzeugs aus bereitgestellten Flugzeuginformationen sowie den Gewichten und Positionen der Frachtstücke berechnet wird.
摘要翻译：本发明涉及一种装置和用于控制飞行器，其特征在于，在所述飞机货舱块的块货运的与权重相关联的引入被识别的装载和/或卸载进程的方法，所述货物项目的位置是在飞机和总重量中跟踪和或提供，以及所述权重和所述包的位置从飞行器信息飞行器的重心被计算/。

8. 发明申请

WO00039542A1 LOAD MEASUREMENT 审中-公开
标题翻译：负载测量
公开(公告)号：WO00039542A1
公开(公告)日：2000-07-06
申请号：PCT/GB1999/004383
申请日：1999-12-22
IPC分类号： B64D45/04 , G01G19/07 , G01L1/22
CPC分类号： G01G19/07 , B64D2045/008 , F16C11/045 , F16C17/24
摘要： A method of measuring load applied to a pin bearing and a pin bearing arrangement for use on an aircraft landing gear are provided. Relieving one or more of two adjacent bushes (4, 5, 6) bearing on a pin (1) of the pin bearing to create a zone of constant shear stress enables measurement of load and avoids cutting the pin.
摘要翻译：提供了一种测量施加到用于飞机起落架上的销轴承和销轴承布置的载荷的方法。卸下支承销轴承的销（1）上的两个相邻衬套（4,5,6）中的一个或多个以产生恒定剪切应力的区域，可以测量负载并避免切割销。

9. 发明申请

WO2023091788A1 METHOD AND SYSTEM FOR INCREASING THE ACCURACY OF AIRCRAFT WEIGHT AND ASSOCIATED CENTER OF GRAVITY DETERMINATIONS 审中-公开
公开(公告)号：WO2023091788A1
公开(公告)日：2023-05-25
申请号：PCT/US2022/050729
申请日：2022-11-22
申请人： NANCE, C., Kirk
发明人： NANCE, C., Kirk
IPC分类号： G01G19/07 , G01M1/12 , B64C25/60 , B64F5/60
摘要： The methods and systems provide for increasing the accuracy of aircraft (1) weight and center of gravity determination through the use of filtered strut pressure measurements. Aircraft (1) vertical and horizontal accelerations are determined as the aircraft (1) is taxiing, and used to identify and reduce the number of significantly distorted pressure measurements, to allow the lesser distorted pressure measurements to be averaged, and a lesser number of distorted pressure measurements to be averaged; further identifying the aircraft (1) in near-neutral acceleration and strut pressure values near-neutral of strut seal friction distortions. Pressure sensors (23, 25), accelerometers (16, 17) and an inclinometer (15) are mounted in relation to landing gear struts (5) to monitor, measure and record strut pressure as related to strut (5) telescopic movement, rates of strut (5) telescopic movement and aircraft vertical and horizontal accelerations; experienced by landing gear struts (5), as the aircraft proceeds through typical ground and taxi operations.

10. 发明申请

WO2022034001A1 VERFAHREN ZUM BETREIBEN EINES VERTIKAL STARTENDEN UND LANDENDEN LUFTFAHRZEUGS UND VERTIKAL STARTENDES UND LANDENDES LUFTFAHRZEUG 审中-公开
公开(公告)号：WO2022034001A1
公开(公告)日：2022-02-17
申请号：PCT/EP2021/072118
申请日：2021-08-09
申请人： VOLKSWAGEN AKTIENGESELLSCHAFT
发明人： KÄPPNER, Christoph
IPC分类号： G01G19/07 , B64C27/00 , B64C29/00 , B64D45/00
摘要： Die Erfindung betrifft ein Verfahren zum Betreiben eines vertikal startenden und landenden Luftfahrzeugs (1), wobei mittels einer Steuereinrichtung (2) eine Masse (m) des Luftfahrzeugs (1) bestimmt wird, wobei hierzu eine vertikale Schubkraft (F_v) eines Antriebs (5) des Luftfahrzeugs (1) bestimmt wird, und eine Masse (m) des Luftfahrzeugs (1) zumindest ausgehend von der bestimmten vertikalen Schubkraft (F_v) und einer Erdbeschleunigung (g) bestimmt wird, und wobei das Luftfahrzeug (1) in Abhängigkeit der bestimmten Masse (m) betrieben wird. Ferner betrifft die Erfindung ein vertikal startendes und landendes Luftfahrzeug (1).

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