公开(公告)号：US20130145836A1

公开(公告)日：2013-06-13

申请号：US13711572

申请日：2012-12-11

Applicant: THALES

Inventor： Jacques MANDLE

IPC: G01M9/06

CPC classification number: G01M9/06 ,  G01P5/16 ,  G01P13/025

Abstract: A probe for measuring a local angle of attack designed to be fixed to a wall and a method implementing the probe are provided. The probe comprises at least three pressure sampling ports disposed over a nose of the probe body, pressure measurement means associated with the pressure sampling ports and calculation means capable of determining an angle of attack of the flow with respect to the main direction of the probe body as a function of the pressures measured by the pressure measurement means. The calculation means are configured for choosing from amongst the pressure sampling ports those allowing the best measurement precision of the local angle of attack to be obtained and for calculating the local angle of attack with respect to the main direction using the pressure measurements carried out in the chosen pressure sampling ports.

Abstract translation: 提供了一种用于测量被设计为固定在墙壁上的局部迎角的探头和实现探头的方法。 探头包括设置在探针主体的鼻部上的至少三个压力采样端口，与压力采样端口相关联的压力测量装置和能够确定流动相对于探针主体的方向的迎角的计算装置 作为由压力测量装置测量的压力的函数。 计算装置被配置为从压力采样端口中选择能够获得局部迎角的最佳测量精度并且使用在主要方向上执行的压力测量来计算局部迎角， 选择压力采样端口。

公开(公告)号：US20160305977A1

公开(公告)日：2016-10-20

申请号：US15132978

申请日：2016-04-19

Applicant: THALES

Inventor： Gilles GENEVRIER ,  Jacques MANDLE ,  Cédric FLAVEN ,  Jean-Pierre SCHLOTTERBECK

IPC: G01P13/02 ,  G01C23/00 ,  B64D43/02 ,  G01S17/58

CPC classification number: G01P13/025 ,  B64D43/02 ,  G01C23/00 ,  G01P5/14 ,  G01P5/26 ,  G01P21/025 ,  G01S7/4813 ,  G01S17/023 ,  G01S17/58 ,  G01S17/95 ,  Y02A90/19

Abstract: A multifunction probe for primary references for an aircraft, an associated measuring system, aircraft and method for obtaining physical quantities are disclosed. In one aspect, the multifunction probe includes a base designed to be fastened on the cockpit of an aircraft, a plurality of static pressure taps arranged through the base and connected to pressure measuring devices and an optical window transparent to laser radiation and positioned in the base for the passage of laser radiation through the base. The multifunction probe further includes at least one laser anemometry optical head positioned to take laser anemometry measurements through the optical window and a static temperature probe mounted on the base.

Abstract translation: 公开了一种用于飞行器的主要参考的多功能探头，相关联的测量系统，用于获得物理量的飞行器和方法。 一方面，多功能探头包括被设计成紧固在飞行器的驾驶舱上的基座，多个静压抽头，其布置成穿过基座并连接到压力测量装置和对激光辐射透明并位于基座中的光学窗口 用于激光辐射通过基底。 多功能探头还包括至少一个激光测风光学头，其定位成通过光学窗口进行激光测风测量，以及安装在基座上的静态温度探头。

公开(公告)号：US20150168439A1

公开(公告)日：2015-06-18

申请号：US14608962

申请日：2015-01-29

Applicant: THALES

Inventor： Gilles GENEVRIER ,  Bernard LEDAIN ,  Jacques MANDLE ,  Jean-Pierre SCHLOTTERBECK

IPC: G01P5/14 ,  G01P5/02 ,  G01S17/58 ,  G01P5/26

CPC classification number: G01P5/14 ,  G01P5/02 ,  G01P5/26 ,  G01P21/025 ,  G01S7/4813 ,  G01S17/023 ,  G01S17/58 ,  G01S17/95 ,  Y02A90/19

Abstract: A probe system, mixed primary reference probe for an aircraft, associated aircraft and measuring method are disclosed. In one aspect, the probe system includes a base designed to be fastened on the cockpit of an aircraft, a plurality of regularly spaced static pressure taps, arranged through the base and designed to be connected to a pressure measurement device. The system includes at least one optical window transparent to laser radiation and inserted into the base.

Abstract translation: 公开了一种用于飞行器的探针系统，混合主参考探头，相关飞行器和测量方法。 在一个方面，探针系统包括被设计成紧固在飞行器的驾驶舱上的基座，多个规则间隔的静压抽头，布置在基座上并设计成与压力测量装置连接。 该系统包括至少一个对激光辐射透明并插入基座的光学窗口。

公开(公告)号：US20150012155A1

公开(公告)日：2015-01-08

申请号：US14323366

申请日：2014-07-03

Applicant: THALES

Inventor： Jacques MANDLE

IPC: B64D45/00 ,  G01C21/00

CPC classification number: G01C21/005 ,  B64D43/02 ,  G01P5/165 ,  G01P13/025

Abstract: The invention relates to an aircraft including a fuselage and a first measuring probe including means for measuring the local incidence, means for measuring the static pressure, and optionally means for measuring the total pressure. The fuselage includes at least one first zone where the pressure coefficient of the aircraft depends on the unique local incidence irrespective of the sideslip and incidence values of the aircraft, and the first measuring probe is arranged in said first zone

Abstract translation: 本发明涉及一种包括机身的飞行器和包括用于测量局部入射的装置的第一测量探头，以及用于测量静压力的装置，以及可选地用于测量总压力的装置。 机身包括至少一个第一区域，其中飞行器的压力系数取决于独特的局部入射，而与飞行器的侧滑和入射值无关，并且第一测量探针布置在所述第一区域

公开(公告)号：US20140245830A1

公开(公告)日：2014-09-04

申请号：US14189875

申请日：2014-02-25

Applicant: THALES

Inventor： Frederic MARTIN ,  Serge DESBIOLLES ,  Jacques MANDLE

IPC: G01P5/165

CPC classification number: G01P5/165

Abstract: A probe for measuring the total pressure of an airflow is intended to equip an aircraft and a method of using the probe. The probe comprises a Pitot tube, two separate heating wires supplied separately and allowing each one to heat an external part of the probe, and means of distribution of a given maximum power to each of the two heating wires as a function of the current temperature of each of the two parts. A method consists in giving priority to the reaching of a predefined minimum temperature of a first of the two parts of the probe by allocating to the first part of the probe a predefined share of the given maximum power for as long as the temperature of the first part is below a predefined minimum temperature.

Abstract translation: 用于测量气流总压力的探头旨在装备飞行器和使用探头的方法。 探针包括皮托管，分开供应的两根单独的加热线，并允许每一根加热线加热探头的外部部分，以及将给定的最大功率分配给两根加热线中的每一根的功能，作为当前温度的函数 这两个部分分别。 一种方法在于通过将探测器的第一部分的预定义份额分配给给定最大功率的预定份额来优先考虑达到探测器两部分中的第一部分的预定义的最低温度，只要第一 部分低于预定的最低温度。