公开(公告)号：US20040023056A1

公开(公告)日：2004-02-05

申请号：US10461400

申请日：2003-06-16

Applicant: SNECMA MOTEURS ,  SNECMA SERVICES

Inventor： Frederic Braillard ,  Philippe Perruchaut ,  Didier Ribot ,  Joel Vigneau

IPC: B32B015/00

CPC classification number: C22C32/0089 ,  B22F3/11 ,  B22F2003/1106 ,  C04B38/00 ,  C23C24/08 ,  F01D5/28 ,  F01D11/122 ,  F04D29/026 ,  F04D29/086 ,  F05D2230/20 ,  F05D2300/17 ,  F05D2300/20 ,  F05D2300/2282 ,  F05D2300/509 ,  F05D2300/609 ,  Y10T428/12181 ,  Y10T428/12667 ,  Y10T428/24355 ,  Y10T428/24372 ,  Y10T428/249953 ,  Y10T428/25 ,  C04B35/10 ,  C04B35/583 ,  C04B35/48 ,  C04B35/522 ,  C04B35/565

Abstract: The present invention concerns: a metallic material that can be worn away by abrasion, principally consisting of a metal alloy based on nickel and/or cobalt which is (quasi) free of oxide or of a ceramic and having in its volume, particles of solid lubricant and/or closed pores and/or surface recesses; parts, in particular plates, formed from said material; casings the inner surface of which is at least partially covered with said plates; a process for producing said material.

Abstract translation: 本发明涉及：可以被磨损磨损的金属材料，主要由基于镍和/或钴的金属合金组成，所述金属合金（准）不含氧化物或陶瓷，其体积为固体颗粒 润滑剂和/或封闭的孔和/或表面凹槽; 由所述材料形成的部件，特别是板; 壳体的内表面至少部分被所述板覆盖; 一种生产所述材料的方法。

公开(公告)号：US20030200835A1

公开(公告)日：2003-10-30

申请号：US10411227

申请日：2003-04-11

Applicant: SNECMA SERVICES

Inventor： Andre Malie ,  Pascal Etuve ,  Christian Michel ,  Frederic Jacquot

IPC: B23K035/32

CPC classification number: B23K1/0018 ,  B23K35/0244 ,  B23K35/3033 ,  B23K35/3046 ,  B23K35/3053 ,  B23K2101/001

Abstract: A diffusion-brazing filler powder for a part made of a nickel-, cobalt- or iron-based alloy A comprising particles of a defined alloy material B having specific functional properties tailored to the area of application of said part. The particles are substantially spherical and carry, on their surfaces, in the form of incrustations, add-ons comprising at least one fluxing element taken from the group: boron and silicon, these encrusted add-ons also being present in a free state in said powder.

Abstract translation: 用于由镍，钴或铁基合金A制成的部分的扩散钎焊填料粉末，其包含具有针对所述部件的施加区域具有特定功能特性的限定合金材料B的颗粒。 颗粒基本上是球形的，并且在其表面上以结垢的形式携带，包含至少一种取自硼和硅的助熔元素的附加物，这些被包覆的附加物也以所述的自由状态存在于所述 粉末。

公开(公告)号：US20040231155A1

公开(公告)日：2004-11-25

申请号：US10709211

申请日：2004-04-21

Applicant: SNECMA SERVICES, FRENCH LIMITED COMPANY

Inventor： Jacques Le Saint ,  Alain Verrieres ,  Francois Ponsen ,  Yannick Hamel

IPC: B23P006/00

CPC classification number: B23P6/002 ,  B23C2226/27 ,  B23C2250/04 ,  B29C63/0069 ,  B29C63/28 ,  B29C63/34 ,  B29C63/481 ,  B29C2063/485 ,  F01D11/122 ,  F01D25/285 ,  F05D2230/80 ,  Y02T50/672 ,  Y10T29/49318 ,  Y10T29/49719 ,  Y10T29/49728 ,  Y10T29/4973 ,  Y10T29/49732 ,  Y10T29/49764

Abstract: A simple and low cost method of replacing an abradable portion on the fan casing of a turbojet includes an inside heating belt together with holding sectors therefor are put into place against the abradable portion, each holding sector including an inflatable bladder, and the abradable portion and the inside heating belt being sandwiched in full between the fan casing and the bladders, the holding sectors themselves being held in place by a plurality of straps attached to the fan casing by fixing points.

Abstract translation: 更换涡轮喷气发动机的风扇壳体上的可磨损部分的简单且低成本的方法包括内部加热带及其保持部分，以抵靠可磨损部分就位，每个保持部分包括可充气气囊，以及可磨损部分， 内部加热带全部夹在风扇壳体和气囊之间，保持扇区本身通过固定点附接到风扇壳体的多个带固定在适当位置。

公开(公告)号：US20040133396A1

公开(公告)日：2004-07-08

申请号：US10687995

申请日：2003-10-20

Applicant: HISPANO-SUIZA ,  SNECMA SERVICES

Inventor： Christian Bregaint ,  Patrice Cheminot ,  Jean-Marc Druesne ,  Roger Menguy

IPC: G06F011/30

CPC classification number: G05B19/128 ,  G05B2219/49302

Abstract: In order to enable the information contained in an identification connector to be read in a manner that is more reliable, faster, and without risk of damage, the invention provides a reader appliance for reading identification connectors for airplane engines, the connector comprising a plurality of contacts connected to a decoding circuit, each contact corresponding to a binary digit, one or more of the binary digits corresponding to information relating to characteristics of the engine. The reader appliance comprises connection means suitable for receiving at least one identification connector, the connection means being connected to processor means responding to control members in order to display on a display device the information contained in the connector.

Abstract translation: 为了使识别连接器中包含的信息以更可靠，更快速的方式被读取并且没有损坏的风险，本发明提供一种读取器装置，用于读取用于飞机发动机的识别连接器，该连接器包括多个 连接到解码电路的触点，对应于二进制数字的每个触点，对应于与发动机的特性有关的信息的一个或多个二进制数字。 读取器设备包括适于接收至少一个识别连接器的连接装置，连接装置连接到响应于控制构件的处理器装置，以便在显示装置上显示包含在连接器中的信息。

公开(公告)号：US20040060347A1

公开(公告)日：2004-04-01

申请号：US10445935

申请日：2003-05-28

Applicant: SNECMA MOTEURS ,  SNECMA SERVICES

Inventor： Patrick Comperat ,  Philippe Even

IPC: G01M001/00

CPC classification number: G01H1/006 ,  F01D21/045 ,  F01D25/04 ,  G01M15/12 ,  G01M15/14

Abstract: The invention relates to detecting damage to the rotor of an aircraft engine that includes means for measuring vibration and speed in order to acquire data relating to the speed of the rotor and also to the amplitude and the phase of rotor vibration during a determined flight. The method comprises the following steps: reading said acquired data; calculating a mean vibration vector over a determined rotor speed range on the basis of said acquired data; calculating a vector difference between the mean vibration vector of said determined flight and the mean vibration vector of a reference flight for said rotor speed range; comparing the modulus of said vector difference with a predetermined threshold value; and issuing a warning signal when the modulus of said vector difference exceeds said predetermined threshold value, said steps being performed after said determined flight has been completed.

Abstract translation: 本发明涉及检测飞机发动机的转子的损坏，其包括用于测量振动和速度的装置，以便获得与转子速度有关的数据，以及在确定的飞行期间转子振动的振幅和相位。 该方法包括以下步骤：读取所述获取的数据; 基于所述获取的数据计算确定的转子速度范围上的平均振动矢量; 计算所述确定的飞行的平均振动矢量与所述转子速度范围的参考飞行的平均振动矢量之间的矢量差; 将所述矢量差的模量与预定阈值进行比较; 以及当所述矢量差的模量超过所述预定阈值时发出警告信号，所述步骤在所述确定的飞行完成之后执行。

公开(公告)号：US20030231975A1

公开(公告)日：2003-12-18

申请号：US10441008

申请日：2003-05-20

Applicant: SNECMA MOTEURS ,  SNECMA SERVICES

Inventor： Frederic Braillard ,  Claude Mons ,  Philippe Perruchaut ,  Didier Ribot ,  Joel Vigneau

IPC: B22F003/02

CPC classification number: B22F1/0077 ,  B22F1/0059 ,  B22F3/1025 ,  B22F3/225 ,  B22F2998/00 ,  B22F2999/00 ,  C22C33/0228 ,  F16N15/00 ,  B22F1/0096

Abstract: The present invention provides: a material, which is dense, with a density of null90%, bulk dry self-lubricating, with a coefficient of friction of

Abstract translation: 本发明提供：密度为> 90％的本体干燥自润滑的材料，摩擦系数<0.3，由赋予其合适强度的基体构成，具有Rm 在300℃的中等至高温范围内> 400MPa。<=θ= 600℃。 所述基质包括其体积中的固体润滑剂颗粒; 由所述材料形成的机械部件; 一种制造所述材料的方法。