公开(公告)号：US20160254576A1

公开(公告)日：2016-09-01

申请号：US15053391

申请日：2016-02-25

Applicant: AIRBUS DEFENCE AND SPACE GMBH

Inventor： Simon BURNS

IPC: H01M10/48 ,  B64G1/42 ,  B64D27/24 ,  H01M10/0525 ,  H01M10/42

CPC classification number: H01M10/482 ,  B64C2201/042 ,  B64D27/24 ,  B64D41/00 ,  B64G1/425 ,  H01M2/1077 ,  H01M2/34 ,  H01M2/348 ,  H01M10/052 ,  H01M10/0525 ,  H01M10/4235 ,  H01M10/425 ,  H01M10/486 ,  H01M10/625 ,  H01M10/658 ,  H01M2200/00 ,  H01M2200/10 ,  H01M2220/20 ,  Y02E60/122

Abstract: A battery arrangement is provided that includes battery cells that are electrically connected to one another, wherein each of the battery cells includes individual electrochemical cells. Each of the battery cells is thermally insulated from the further battery cells of the plurality of battery cells. Each of the individual electrochemical cells includes a monitoring device. The monitoring device is configured to electrically disconnect the battery cell from the further battery cells if at least one measured value that is to be monitored by the monitoring device lies outside a predetermined value range.

Abstract translation: 提供了一种电池装置，其包括彼此电连接的电池单元，其中每个电池单元包括单独的电化学电池。 每个电池单元与多个电池单元的其它电池单元热绝缘。 每个单独的电化学电池包括监测装置。 如果要由监视装置监视的至少一个测量值位于预定值范围之外，则监视装置被配置为将电池单元与其他电池单元电气断开。

公开(公告)号：US20190043373A1

公开(公告)日：2019-02-07

申请号：US16044844

申请日：2018-07-25

Applicant: AIRBUS DEFENCE AND SPACE GMBH

Inventor： Winfried LOHMILLER ,  Cristiano BIANCHI ,  Simon BURNS

IPC: G08G5/02 ,  G08G5/06 ,  G08G5/00 ,  G01S5/02 ,  G01S5/14 ,  G01S5/06

Abstract: A device for checking the consistency of a positioning includes: a transmitter, a receiver, a time measuring unit, a distance determining module and a check module. The transmitter emits at least one signal, and the receiver receives at least four response signals from at least four different response elements. A response element receives the at least one signal and, upon receipt, emits a response signal. The time measuring unit determines, for each response signal, a total delay time from a transmission time of the signal and a reception time of the respective signal. The distance determination module determines a distance to the respective response element based on each total delay time, and the check module performs a consistency check of a determination of a position based on distances to the different response elements. With the device, erroneous distance values may be detected in ground-based positioning systems.

公开(公告)号：US20160236789A1

公开(公告)日：2016-08-18

申请号：US15041424

申请日：2016-02-11

Applicant: AIRBUS DEFENCE AND SPACE GMBH

Inventor： Simon BURNS

IPC: B64D27/02 ,  B64C39/02 ,  B64C31/00

CPC classification number: B64D27/02 ,  B64C31/00 ,  B64C39/02 ,  B64C39/024 ,  B64C2201/00 ,  B64C2201/021 ,  B64C2201/042 ,  B64C2201/165

Abstract: An aircraft which has a supporting structure which has at least one fuselage, a wing structure and at least one drive apparatus. The drive apparatus has at least one propeller and a drive motor. The aircraft has at least one energy store for providing energy for operation of the drive apparatus. The at least one drive apparatus and the at least one energy store are mechanically connected to the supporting structure and/or the wing structure of the aircraft by a securing device.

Abstract translation: 具有至少一个机身，机翼结构和至少一个驱动装置的支撑结构的飞机。 驱动装置具有至少一个螺旋桨和驱动马达。 飞机具有至少一个能量存储器，用于为驱动装置的操作提供能量。 所述至少一个驱动装置和所述至少一个能量存储器通过固定装置机械连接到所述飞行器的支撑结构和/或机翼结构。