公开(公告)号：US10001082B2

公开(公告)日：2018-06-19

申请号：US14560218

申请日：2014-12-04

Applicant: AIRCELLE

Inventor： Olivier Conet ,  Rémi Pujol ,  Michel Jean ,  Jean-Francois Thouement

IPC: F02K1/76 ,  B64D29/06

CPC classification number: F02K1/766 ,  B64D29/06

Abstract: An assembly for a turbojet engine includes a pylon, a nacelle supported by the pylon, and a locking device interposed between the pylon and a cowl of the nacelle. The cowl slides between operating and maintenance positions. The locking device is movable between active and inhibited positions, and the device allows an operation mode in the active position and a maintenance mode in the inhibited position. In particular, the locking device comprises a rocker to maintain the cowl to the pylon, and the rocker includes an inhibiting lever and an activation lever. The inhibiting and activation levers are mounted on a switching shaft of the locking device. The inhibiting lever is set in rotation through an actuator, providing direct access from a bypass flow duct in the active position while the activation lever is set in rotation from the bypass duct in the inhibited position.

公开(公告)号：US09915269B2

公开(公告)日：2018-03-13

申请号：US14161595

申请日：2014-01-22

Applicant: AIRCELLE

Inventor： Romain Billault

IPC: F04D29/40 ,  F01D25/24 ,  F02K1/80

CPC classification number: F04D29/403 ,  F01D25/243 ,  F02K1/80

Abstract: A device for connecting a front frame of a turbojet engine nacelle to a fan casing includes a locking pin connected to a first assembly flange and a retaining flange that is movably mounted and has at least one opening. In particular, the locking pin has a shank passing through an orifice of a second assembly flange secured to the fan casing. The opening is crossed through by the shank of the locking pin and interacts with an end groove of said locking pin. When the retaining flange is in the unlocking position, the opening has dimensions larger than those of the shank of the locking pin, and when the retaining flange is in the locking position, the opening has dimensions larger than a thickness of the locking pin at its groove but smaller than an overall thickness of the shank of the orifice of the second flange.

公开(公告)号：US09834313B2

公开(公告)日：2017-12-05

申请号：US14633269

申请日：2015-02-27

Applicant: AIRCELLE

Inventor： Xavier Cazuc ,  Jean-Philippe Joret

IPC: F02C6/00 ,  B64D29/06 ,  F02K1/72 ,  F01D25/28 ,  F02K1/70

CPC classification number: B64D29/06 ,  F01D25/28 ,  F02K1/70 ,  F02K1/72 ,  F05D2300/603 ,  Y02T50/672

Abstract: The present disclosure relates to a front frame for an aircraft nacelle comprising a turbojet mounted on a suspension strut, said nacelle comprising a thrust reverser including an actuator designed to open a thrust reversal cowling. The front frame comprises a tubular torsion box, a first straight attachment edge intended to attach the box to a turbojet casing and a second straight attachment edge intended to attach the box to air flow diversion means. The front frame is arranged to transmit tensile and compressive loads between the turbojet casing and the air flow diversion means and torsion loads absorbed by the suspension strut. The front frame is characterized in that the tubular torsion box has a semi-elliptical or elliptical cross-section.

公开(公告)号：US09816301B2

公开(公告)日：2017-11-14

申请号：US14187770

申请日：2014-02-24

Applicant: AIRCELLE

Inventor： Patrick Gonidec

IPC: E05C5/00 ,  E05C19/12 ,  B64D29/06 ,  E05B41/00 ,  E05C1/00

CPC classification number: E05C19/12 ,  B64D29/06 ,  E05B41/00 ,  E05C1/006 ,  Y10T292/0936

Abstract: A locking device includes a locking pair having a bolt to engage with a retainer and a detection linkage. The bolt is movably mounted against a spring which tends to return the bolt to a position spaced apart from the retainer. The detection linkage is also movably mounted between an unlocked position where the detection linkage allows unlocking of the bolt and the retainer. In particular, a portion of the bolt then engages with the detection linkage by means of a detecting part of the detection linkage to block a possible return of the detection linkage towards a locked position where the detection linkage engages with the portion of the bolt so as to oppose to unlocking of the bolt. The detecting part irreversibly drives the detection linkage to its unlocked position even when one locking pair is unlocked.

公开(公告)号：US09797829B2

公开(公告)日：2017-10-24

申请号：US15098895

申请日：2016-04-14

Applicant: AIRCELLE

Inventor： Andre Baillard ,  Odile Lefeu ,  Frederic Joubert ,  Emmanuel Piel

IPC: G01N21/3563 ,  G01N25/72 ,  G01J3/28 ,  G01N33/32 ,  G01N21/84 ,  G01N21/88 ,  G01N21/95

CPC classification number: G01N21/3563 ,  G01J3/28 ,  G01J2003/2859 ,  G01N21/8422 ,  G01N21/8851 ,  G01N21/95 ,  G01N25/72 ,  G01N33/32 ,  G01N2021/8427 ,  G01N2021/8472

Abstract: A method for assessing damage to a composite material covered with a polyurethane-type paint is provided. Two separate criteria are measured on a spectrogram obtained by infrared spectrometry, thereby characterizing thermal ageing of the paint, each separate criteria being a measurement on a curve of a spectrum of the spectrogram of a height of a particular peak, thereby giving two independent assessments of the thermal ageing. Then, the two separate criteria are combined together in order to obtain a result of a level of the damage.

公开(公告)号：US09789556B2

公开(公告)日：2017-10-17

申请号：US14883994

申请日：2015-10-15

Applicant: AIRCELLE

Inventor： Philippe Bienvenu ,  Helene Malot ,  Francisco Caneque

IPC: B23K31/02 ,  B23K3/08 ,  B21D26/033 ,  B23K1/008 ,  F02K1/82 ,  F02K1/80 ,  B23K1/00 ,  B23K101/00

CPC classification number: B23K3/087 ,  B21D26/033 ,  B23K1/0014 ,  B23K1/0018 ,  B23K1/008 ,  B23K2101/001 ,  F02K1/80 ,  F02K1/827 ,  F05D2230/23 ,  F05D2230/237 ,  F05D2250/283 ,  F05D2300/502

Abstract: A method for assembling a set including an inner wall, a shrouded outer wall and an intermediate element, each presenting substantially circular sections, the shrouded outer wall presenting a shape substantially complementary to a shape of outer and inner surfaces of the intermediate element, and whose inner surface covers the outer surface of the intermediate element. In particular, the method includes a step of placing a brazing sheet, whose melting temperature is lower than melting temperatures of other elements of the set, over an assembly surface in contact with another assembly surface, and a step of heating, by a furnace, a set including the outer or inner walls and the intermediate element between which is interposed a brazing sheet so as to fix the outer or inner wall by brazing on the intermediate element.

公开(公告)号：US09587584B2

公开(公告)日：2017-03-07

申请号：US14578110

申请日：2014-12-19

Applicant: AIRCELLE

Inventor： Hakim Maalioune ,  Alain Nourrisson

IPC: H02P7/06 ,  F02K1/76 ,  B64D41/00 ,  B64D33/04

CPC classification number: F02K1/763 ,  B64D33/04 ,  B64D41/00 ,  B64D2221/00 ,  F02K1/76 ,  F05D2260/901 ,  F05D2270/62 ,  H02P7/06 ,  Y02T50/44 ,  Y02T50/671

Abstract: A thrust reverser device for an aircraft includes at least two thrust reversers, and each of them includes a movable cowl movably actuated by an actuator driven by an electric motor. The electric motor is powered by a single power-conversion module including at least one autotransformer which is supplied with an alternating electric voltage and connected to at least one rectifier stage converting the alternating electric voltage into a direct voltage. The rectifier stage is connected to a current balancing stage and a current smoothing stage, supplying with the direct voltage the electric motor of the electric actuator of the movable cowl.

Abstract translation: 用于飞行器的推力反向装置包括至少两个推力反向器，并且它们中的每一个包括由由电动机驱动的致动器可移动地致动的可动外罩。 电动机由单个功率转换模块供电，所述单个功率转换模块包括至少一个自耦变压器，该自耦变压器被提供有交流电压并且连接到将交流电压转换为直流电压的至少一个整流器级。 整流器级连接到电流平衡级和电流平滑级，向可动罩的电致动器的电动机提供直流电压。

公开(公告)号：US09562595B2

公开(公告)日：2017-02-07

申请号：US14166524

申请日：2014-01-28

Applicant: AIRCELLE

Inventor： Pierre Caruel ,  Pierre Moradell-Casellas

IPC: F02K1/62 ,  F16H25/12 ,  F02K1/72 ,  F02K1/76 ,  F16H25/20

CPC classification number: F16H25/12 ,  F02K1/625 ,  F02K1/72 ,  F02K1/763 ,  F16H25/20 ,  F16H2025/2059 ,  F16H2025/2075 ,  Y02T50/671 ,  Y10T74/18576

Abstract: The present disclosure relates to a double-acting linear actuator for moving an inner part and an outer part of a cowl relative to a fixed frame. The linear actuator includes a first tubular body housing a first drive shaft and a second tubular body housing a second drive shaft. In particular, the first and second tubular bodies are mounted in series by the second drive shaft which is mounted on the first tubular body. The second drive shaft translates the second tubular body relative to the first tubular body when a lock of the first tubular body is in a locked position, and the first drive shaft translates both the first tubular and second tubular bodies when the lock is in an unlocked position.

Abstract translation: 本发明涉及一种用于使整流罩的内部部分和外部部分相对于固定框架移动的双作用线性致动器。 线性致动器包括容纳第一驱动轴的第一管状体和容纳第二驱动轴的第二管状体。 特别地，第一和第二管状体通过安装在第一管状体上的第二驱动轴串联安装。 当第一管状体的锁定处于锁定位置时，第二驱动轴相对于第一管状体转动第二管状体，并且当锁处于解锁状态时，第一驱动轴平移第一管状体和第二管状体 位置。

公开(公告)号：US20170022935A1

公开(公告)日：2017-01-26

申请号：US15283591

申请日：2016-10-03

Applicant: AIRCELLE

Inventor： HUE Corentin ,  Rodolphe DENIS ,  Denis GUILLOIS ,  Sarah TISSOT

IPC: F02K1/76 ,  F02K1/62

CPC classification number: F02K1/766 ,  F02K1/60 ,  F02K1/62 ,  F02K1/70 ,  F02K1/763 ,  F05D2220/323 ,  F05D2260/52

Abstract: The present disclosure relates to a system for locking the position of the flaps of a thrust reverser of a turbojet nacelle, said flaps being controlled by actuators, each one swinging about a tranverse pivot in order to partially close off the air stream so as to guide it forwards, further including locks for locking the flaps in an intermediate opening position, between the closed position and the open position.

Abstract translation: 本公开涉及一种用于锁定涡轮喷气发动机舱的推力反向器的翼片的位置的系统，所述翼片由致动器控制，每个翼片围绕横向枢轴摆动以部分地关闭空气流，以便引导 其进一步包括用于将襟翼锁定在中间打开位置中的锁定件，在关闭位置和打开位置之间。

公开(公告)号：US20170016412A1

公开(公告)日：2017-01-19

申请号：US15281569

申请日：2016-09-30

Applicant: AIRCELLE

Inventor： Patrick BOILEAU ,  Olivier KERBLER

IPC: F02K1/62 ,  F01D25/24 ,  F02K1/76

CPC classification number: F02K1/625 ,  F01D25/24 ,  F02K1/72 ,  F02K1/763 ,  F05D2220/32 ,  F05D2250/34 ,  F05D2250/90

Abstract: A thrust reverser of a bypass turbojet engine nacelle is disclosed, which includes movable cowls that move backwards with respect to a fixed front structure to uncover thrust reverser cascades and a variable secondary nozzle connected to the movable cowls by guide means allowing an axial sliding of the system which controls the movement of this variable secondary nozzle, wherein it includes cylinders bearing on the front structure for controlling reversal means of the displacement direction connected to the movable cowls, which move the variable secondary nozzle backwards when these cylinders output a forward stroke, as well as blocking devices which connect the secondary nozzle to the movable cowls when this nozzle is deployed.

Abstract translation: 公开了旁路涡轮喷气发动机机舱的推力反向器，其包括相对于固定前部结构向后移动的可动罩，以揭开推力反向器级联，以及通过引导装置连接到可动罩的可变次级喷嘴，允许轴向滑动 系统，其控制该可变二次喷嘴的运动，其中它包括在前结构上支撑的气缸，用于控制连接到可动罩的位移方向的反转装置，当这些气缸输出向前冲程时向后移动可变二次喷嘴，如 以及当该喷嘴被部署时将二次喷嘴连接到可动罩的阻挡装置。