公开(公告)号：US20150139802A1

公开(公告)日：2015-05-21

申请号：US14536954

申请日：2014-11-10

Applicant: SNECMA

Inventor： Augustin CURLIER ,  Gilles Alain Charier

IPC: B64C11/38 ,  F01D7/00 ,  B64C11/30

CPC classification number: B64C11/38 ,  B64C11/306 ,  B64D2027/005 ,  F01D7/00 ,  F01D25/16 ,  F01D25/162 ,  F01D25/18 ,  F01D25/246 ,  F02C7/06 ,  F05D2260/70 ,  F16H57/04 ,  F16H57/0423 ,  F16H57/046 ,  Y02T50/66

Abstract: Device for supplying oil under pressure to a linear actuator of a turbine engine, this actuator comprising an internal fixed portion and an external movable portion and means for regulating and supplying oil to chambers of the actuator, these regulating means being mounted radially outside the movable portion of the actuator, and the fixed portion of the actuator comprising on its upstream end portion oil passage channels of which the outlets open radially outwards, the device further comprising an oil distribution ring which is mounted on the upstream end portion of the fixed portion and which comprises internal conduits of which the inlets communicate with the outlets of the channels of the fixed portion and the outlets open axially downstream and are connected to the regulating means.

Abstract translation: 用于在压力下将油供应到涡轮发动机的线性致动器的装置，该致动器包括内部固定部分和外部可移动部分，以及用于调节和供应致动器腔室的装置的装置，这些调节装置径向地安装在可动部分的外部 所述致动器的固定部分包括在其上游端部分，其出口径向向外开口的油通道通道，该装置还包括安装在固定部分的上游端部分上的分油环， 包括内部管道，入口与固定部分的通道的出口连通，并且出口沿轴向下游开口并连接到调节装置。

公开(公告)号：US20160326964A1

公开(公告)日：2016-11-10

申请号：US15110001

申请日：2014-12-24

Applicant: SNECMA

Inventor： Augustin CURLIER ,  Julien AUSTRUY ,  Tewfik BOUDEBIZA ,  Gilles Alain CHARIER

IPC: F02C7/36 ,  F16H1/28 ,  F16D3/223 ,  F02K3/072

CPC classification number: F02C7/36 ,  F02K3/072 ,  F05D2260/40311 ,  F16D3/223 ,  F16H1/28 ,  Y02T50/671

Abstract: An epicyclic gear device for driving rotation of a first blade set of a turbine engine, the device: including a sunwheel centered on a longitudinal axis of the turbine engine and connected to a rotor of the engine in order to be driven in rotation; at least one planet meshing with the sunwheel; a planet carrier rotatably carrying the planet and connected to a first blade set in order to drive it in rotation; and a ring meshing with the planet; the sunwheel being connected to the rotor via a first constant velocity ball transmission joint.

Abstract translation: 一种用于驱动涡轮发动机的第一叶片组的旋转的行星齿轮装置，该装置包括：以涡轮发动机的纵向轴线为中心并连接到发动机的转子的阳光，以便旋转驱动; 至少有一个行星与太阳轮啮合; 行星架可旋转地承载行星并连接到第一叶片组以驱动其旋转; 和与地球啮合的环; 太阳轮通过第一等速球传动接头连接到转子。

公开(公告)号：US20160299019A1

公开(公告)日：2016-10-13

申请号：US15100838

申请日：2014-12-02

Applicant: SNECMA

Inventor： Augustin CURLIER ,  Gilles LA GOUELLEC ,  Alexis KUNAKOVITCH

IPC: G01L3/10 ,  G01L25/00

CPC classification number: G01L3/104 ,  G01L1/165 ,  G01L3/102 ,  G01L25/003

Abstract: The present invention relates to a torque-measurement device for a turbine engine shaft (1) including a proof body (7) capable of being mounted on the shaft, characterised in that the proof body (7) forms a mounting for at least one acoustic-wave strain gauge (20) and is magnetised such as to allow the torque to be measured by magnetostrictive effect. The invention also relates to a method for calibrating the torque-measurement system including a first step of calibrating said device, the device being mounted on a shaft but outside of the engine, by applying reference torques to the shaft with the device and by establishing a rule regarding the relationship between the strain measured by said strain gauge and the actual torque applied, a step of mounting the shaft with the device inside the turbine engine together with placement of the magnetostrictive measurement system, the calibration of the first step being optionally reset with the engine stopped, and a step of establishing a calibration rule regarding the relationship between the torque measured by magnetostrictive effect and the reference torque provided by the strain gauges.

Abstract translation: 本发明涉及一种用于涡轮发动机轴（1）的转矩测量装置，其包括能够安装在轴上的检验体（7），其特征在于，所述检验体（7）形成用于至少一个声学 波应变仪（20），并被磁化，以允许通过磁致伸缩效应来测量转矩。 本发明还涉及一种用于校准扭矩测量系统的方法，该方法包括：校准所述装置的第一步骤，所述装置安装在轴上且在发动机外部，通过使用所述装置将参考扭矩施加到所述轴上，并且通过建立 关于由所述应变仪测量的应变与所施加的实际扭矩之间的关系的规则，将所述轴与所述装置一起安装在所述涡轮发动机内部以及所述磁致伸缩测量系统的放置的步骤，所述第一步骤的校准可选地重置为 发动机停止，并且建立关于由磁致伸缩效应测量的扭矩与由应变计提供的参考扭矩之间的关系的校准规则的步骤。

公开(公告)号：US20150217854A1

公开(公告)日：2015-08-06

申请号：US14612661

申请日：2015-02-03

Applicant: SNECMA

Inventor： Jean-Christophe DUFFET ,  Tewfik BOUDEBIZA ,  Augustin CURLIER

IPC: B64C11/30

CPC classification number: B64C11/306 ,  B64C11/308 ,  B64D2027/005 ,  F02C3/067 ,  F02C6/206 ,  Y02T50/66 ,  Y02T50/672

Abstract: The turbine engine includes respective systems for changing the pitch of the propeller blades, the system (22) for the upstream propeller including a linear actuator (23) and a transmission mechanism (24) connecting the actuator to the blades in order to transform the sliding of the actuator into a rotation of the blades, said upstream propeller (2) including a rotatable housing (19) rigidly connected to a rotatable shaft (17) supported in a static housing (27) of the turbine engine by a bearing (29) upstream of the system, and by a bearing (30) downstream of the system. Advantageously:the rotatable housing (19) of the upstream propeller includes a support (36) rigidly connected to said rotatable housing and surrounding the static housing (27),the actuator (23) is annular and fixed to the support (36) of the rotatable housing, outside the support, and the transfer mechanism comprises connecting rods (33) and rotatable radial arms (34) traversing the gaseous flow path in order to control the pitch of the blades, andthe downstream bearing (30) is provided between the static housing (27) and the support (36), inside said support (36).

Abstract translation: 涡轮发动机包括用于改变螺旋桨叶片间距的相应系统，用于上游螺旋桨的系统（22）包括线性致动器（23）和将致动器连接到叶片的传动机构（24），以便将滑动 所述上游螺旋桨（2）包括通过轴承（29）刚性地连接到支撑在所述涡轮发动机的静态壳体（27）中的可旋转轴（17）的可旋转壳体（19） 在系统的上游，以及系统下游的轴承（30）。 有利地：上游螺旋桨的可旋转壳体（19）包括刚性地连接到所述可旋转壳体并围绕静态壳体（27）的支撑件（36），致动器（23）是环形的并且固定到支撑件（36） 可旋转壳体，支撑件外部，并且传送机构包括连接杆（33）和横穿气体流动路径的可旋转的径向臂（34），以便控制叶片的间距，并且下游轴承（30）设置在 静止壳体（27）和支撑件（36）。