公开(公告)号：EP2092286B1

公开(公告)日：2011-11-16

申请号：EP07869574.9

申请日：2007-12-19

Applicant: Rosemount Aerospace Inc.

Inventor： SANDNAS, Mathew L. ,  AUSTIN, Glenn ,  BUENZ, Mark J. ,  TEIGEN, Daniel ,  WILLIAMS, Wade

IPC: G01K13/02

CPC classification number: G01K13/02 ,  G01K13/028

Abstract: A total air temperature sensor includes a probe secured to a first side of a vehicle surface. The probe includes an air inlet and a temperature sensing element. Air flows into the air inlet and passes by the temperature sensing element. The temperature sensing element produces a temperature sensing element electrical signal as a function of a temperature of the air. The total air temperature sensor also includes an electronics package secured to a second side of the vehicle surface. Electronics in the electronics package receive the temperature sensing element electrical signal from the temperature sensing element and determine a total air temperature as a function of the temperature sensing element electrical signal.

公开(公告)号：EP1663675B1

公开(公告)日：2011-07-27

申请号：EP04816823.1

申请日：2004-08-24

Applicant: ROSEMOUNT AEROSPACE INC.

Inventor： BUENZ, Mark J. ,  NORLIEN, John A. ,  KUNIK, William G. ,  WILLIAMS, Wade W. ,  MYHRE, Douglas C.

IPC: B60C23/04

CPC classification number: G01P3/44 ,  B60C23/0428 ,  B60C23/043 ,  B60C2200/02 ,  G01P3/48

Abstract: A wireless tire pressure sensing system for an aircraft comprises: dual resonant circuits mounted to a wheel of the aircraft, each resonant circuit comprising: a variable capacitance sensor (16) and a wire loop (12) of a predetermined inductance coupled thereto, one capacitance sensor for monitoring the pressure of a tire mounted to the wheel, and the other capacitance sensor operative as a reference to the one capacitance sensor; an interrogating circuit (18) magnetically coupleable to the dual resonant circuits and operative to induce magnetically a variable frequency current in the dual resonant circuits, the one resonant circuit responding to the induced current with an E-field signal at a first resonant frequency commensurate with the capacitance of the one sensor, and the other resonant circuit responding to the induced current with an E-field signal at a second resonant frequency commensurate with the capacitance of the other sensor; a receiving circuit (20) E-field coupleable to the dual resonant circuits and operative to receive the E-field signals at the first and second resonant frequencies and to generate first and second signals representative thereof; and a processing circuit coupled to the receiving circuit for processing the first and second signals to generate a compensated pressure reading of the tire. The pressure sensing system may be modified to provide and/or include wheel speed sensing.

公开(公告)号：EP2092286A2

公开(公告)日：2009-08-26

申请号：EP07869574.9

申请日：2007-12-19

Applicant: Rosemount Aerospace Inc.

Inventor： SANDNAS, Mathew L. ,  AUSTIN, Glenn ,  BUENZ, Mark J. ,  TEIGEN, Daniel ,  WILLIAMS, Wade

IPC: G01K13/02

CPC classification number: G01K13/02 ,  G01K13/028

Abstract: A total air temperature sensor includes a probe secured to a first side of a vehicle surface. The probe includes an air inlet and a temperature sensing element. Air flows into the air inlet and passes by the temperature sensing element. The temperature sensing element produces a temperature sensing element electrical signal as a function of a temperature of the air. The total air temperature sensor also includes an electronics package secured to a second side of the vehicle surface. Electronics in the electronics package receive the temperature sensing element electrical signal from the temperature sensing element and determine a total air temperature as a function of the temperature sensing element electrical signal.

公开(公告)号：EP1663675A2

公开(公告)日：2006-06-07

申请号：EP04816823.1

申请日：2004-08-24

Applicant: ROSEMOUNT AEROSPACE INC.

Inventor： BUENZ, Mark J. ,  NORLIEN, John A. ,  KUNIK, William G. ,  WILLIAMS, Wade W. ,  MYHRE, Douglas C.

IPC: B60C23/04

CPC classification number: G01P3/44 ,  B60C23/0428 ,  B60C23/043 ,  B60C2200/02 ,  G01P3/48

Abstract: A wireless tire pressure sensing system for an aircraft comprises: dual resonant circuits mounted to a wheel of the aircraft, each resonant circuit comprising: a variable capacitance sensor (16) and a wire loop (12) of a predetermined inductance coupled thereto, one capacitance sensor for monitoring the pressure of a tire mounted to the wheel, and the other capacitance sensor operative as a reference to the one capacitance sensor; an interrogating circuit (18) magnetically coupleable to the dual resonant circuits and operative to induce magnetically a variable frequency current in the dual resonant circuits, the one resonant circuit responding to the induced current with an E-field signal at a first resonant frequency commensurate with the capacitance of the one sensor, and the other resonant circuit responding to the induced current with an E-field signal at a second resonant frequency commensurate with the capacitance of the other sensor; a receiving circuit (20) E-field coupleable to the dual resonant circuits and operative to receive the E-field signals at the first and second resonant frequencies and to generate first and second signals representative thereof; and a processing circuit coupled to the receiving circuit for processing the first and second signals to generate a compensated pressure reading of the tire. The pressure sensing system may be modified to provide and/or include wheel speed sensing.

Abstract translation: 提供了一种用于飞机的无线轮胎压力和车轮速度感测系统。 该系统包括以下部件。 谐振电路安装在飞行器的车轮上，用于监测安装在所述车轮上的轮胎的压力。 谐振电路包括预定电感的导线回路。 询问电路可磁耦合到所述谐振电路，并且可操作地在所述谐振电路的导线环中以磁性方式感应可变频率电流。 谐振电路响应于所述感应电流产生相应的可变频率电场。 可变频率电场包括与所述轮胎的压力相称的共振频率。 提供了一种磁场改变装置，用于交替所述线环与所述询问电路之间的磁耦合，以使所述可变频率电场的幅度调制速率与所述车轮速度相称。 接收电路E场可耦合到所述谐振电路，并用于接收所述谐振电路的幅度调制的可变频率电场并产生代表其的信号。 第一处理电路耦合到所述接收电路，用于处理该信号以基于其谐振频率产生所述轮胎的压力读数。 第二处理电路被耦合到所述接收电路，用于处理所述信号，以基于其幅度调制率来产生车轮速度读数。