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公开(公告)号：US09587583B2
公开(公告)日：2017-03-07
申请号：US14173484
申请日：2014-02-05
申请人： AIRCELLE
发明人： Pierre Caruel , Patrick Gonidec , Patrick Boileau
摘要： A turbojet engine nacelle has a thrust reverser device and an actuating system for said thrust reverser device, and the thrust reverser device includes a moving cowl mounted translatably alternating between a closed position and an open position, and a jet nozzle section for gases that extends the moving cowl. In particular, the jet nozzle section includes a nozzle flap mounted movable between a closed position and an open position in which the nozzle flap opens a leakage passage toward the outside of the nozzle section. The actuating system has an actuator shared with the moving cowl and the nozzle flap to activate the translational movement of the moving cowl and to pivot the nozzle flap between three following positions: an idle position, an open position of the nozzle flap and an open position of the moving cowl.
摘要翻译： 涡轮喷气发动机发动机舱具有推力反向装置和用于所述推力反向装置的致动系统，并且推力反向装置包括可在可关闭位置和打开位置之间平移地交替安装的移动整流罩，以及用于气体的喷嘴部分， 移动整流罩 特别地，喷嘴部分包括安装在关闭位置和打开位置之间的喷嘴盖，喷嘴盖打开朝向喷嘴部分外部的泄漏通道。 致动系统具有与移动整流罩和喷嘴挡板共享的致动器，以启动移动整流罩的平移运动并使喷嘴阀瓣在三个以下位置之间枢转：空转位置，喷嘴挡板的打开位置和打开位置 的移动整流罩。
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2.发明申请LOCKING/UNLOCKING DEVICE FOR A THURST REVERSER WITH A SLIDING COVER AND ADAPTIVE NOZZLE FOR AIRCRAFT ENGINE NACELLE 有权用于具有滑盖的颠倒装置和用于飞机发动机的自适应喷嘴的锁定/解锁装置公开(公告)号：US20140000238A1
公开(公告)日：2014-01-02
申请号：US13801813
申请日：2013-03-13
申请人： AIRCELLE
IPC分类号： F02K1/76
CPC分类号： F02K1/766 , F02K1/09 , F02K1/72 , Y02T50/671
摘要： A locking/unlocking device for a thrust reverser with sliding cover and adaptive nozzle is provided that includes a fixed pin secured to a fixed structure of the reverser, a first sleeve secured to the sliding cover and able to accommodate the pin, a second sleeve slidabiy mounted on the first sleeve, a third sleeve secured to the adaptive nozzle and slidably mounted on the second sleeve, first locking means able to lock the first sleeve with respect to the pin, second locking means able to lock the second sleeve with respect to the first sleeve, and third locking means able to lock the third sleeve with respect to the second sleeve.
摘要翻译： 提供一种用于具有滑动盖和自适应喷嘴的推力反向器的锁定/解锁装置，其包括固定到反向器的固定结构的固定销，固定到滑动盖并能够容纳销的第一套筒，第二套筒可滑动 安装在第一套筒上，第三套筒固定到自适应喷嘴并可滑动地安装在第二套筒上，第一锁定装置能够相对于销锁定第一套筒，第二锁定装置能够相对于第二套筒锁定第二套筒 第一套筒和第三锁定装置能够相对于第二套筒锁定第三套筒。
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公开(公告)号：US09816301B2
公开(公告)日：2017-11-14
申请号：US14187770
申请日：2014-02-24
申请人： AIRCELLE
发明人： Patrick Gonidec
CPC分类号： E05C19/12 , B64D29/06 , E05B41/00 , E05C1/006 , Y10T292/0936
摘要： 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.
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公开(公告)号：US08764072B2
公开(公告)日：2014-07-01
申请号：US13867904
申请日：2013-04-22
申请人： Aircelle
发明人： Patrick Gonidec
CPC分类号： E05B83/243 , B64D29/06 , E05B15/022 , E05B17/2038 , E05B41/00 , E05B53/003 , E05B63/24 , E05B83/16 , E05C19/12 , Y10T292/0911 , Y10T292/0936 , Y10T292/0956 , Y10T292/1089
摘要： A locking device includes a bolt capable of engaging with a corresponding hook, the bolt being mounted against a resilient return spring that tends to return the bolt into a spaced apart position. The locking device further includes a detection linkage, which is moveable between a first position and a second position. In the first position, the linkage enables unlocking of the bolt and the hook. In the second position, the linkage engages with a portion of the locking pair so as to block the unlocking.
摘要翻译： 锁定装置包括能够与相应的钩接合的螺栓，所述螺栓抵靠弹性复位弹簧安装，所述弹性复位弹簧倾向于将螺栓返回到间隔开的位置。 锁定装置还包括可在第一位置和第二位置之间移动的检测连杆机构。 在第一位置，联动装置使得能够解锁螺栓和钩子。 在第二位置，连杆与锁定对的一部分相配合，以阻止解锁。
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5.发明授权Assembly including a reverse thrust device and system for actuating said device 有权组件包括用于致动所述装置的反推力装置和系统公开(公告)号：US09518535B2
公开(公告)日：2016-12-13
申请号：US13691160
申请日：2012-11-30
申请人： AIRCELLE
CPC分类号： F02K1/763 , F02K1/1207 , F02K1/72 , F02K1/766
摘要： A reverse thrust device and a system for actuating the reverse thrust device is provided by the present disclosure. The device includes at least one cowl that is translatably mounted in a direction substantially parallel to a longitudinal axis of a nacelle. The actuation system includes an actuation means that is capable of activating translational and rotational movement of the cowl and a panel of a nozzle. The actuation system also includes a downstream locking means for the nozzle and the cowl. The downstream locking means includes at least two reversible states, one of the states being a locked state in which the downstream locking means is suitable for locking the panel of the nozzle into a position for varying the section for outputting the nozzle with the cowl.
摘要翻译： 通过本公开提供了反推力装置和用于致动反推力装置的系统。 该装置包括至少一个整流罩，其可平移地安装在基本上平行于机舱的纵向轴线的方向上。 致动系统包括致动装置，其能够启动整流罩和喷嘴的面板的平移和旋转运动。 致动系统还包括用于喷嘴和整流罩的下游锁定装置。 下游锁定装置包括至少两个可逆状态，其中一个状态是锁定状态，其中下游锁定装置适于将喷嘴的面板锁定到用于改变用于输出具有整流罩的喷嘴的部分的位置。
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公开(公告)号：US09151225B2
公开(公告)日：2015-10-06
申请号：US14304555
申请日：2014-06-13
申请人： AIRCELLE
CPC分类号： F02C7/045 , B64D33/02 , B64D2033/0206 , B64D2033/0286
摘要： An air intake structure for a turbojet engine nacelle includes a substantially annular main structure having an internal wall, an external wall and an air intake lip structure connecting the external and internal walls upstream. The air intake structure also includes a first acoustic attenuation structure which has a holed acoustic skin, a cellular core and a solid rear skin with which the internal wall is equipped, and a second acoustic attenuation structure having a similar architecture fitted to a part of the air intake lip substantially near a junction with the internal wall. The rear skin of the first acoustic attenuation structure is aligned with the rear skin of the second acoustic attenuation structure, both of rear skins being structural.
摘要翻译： 用于涡轮喷气发动机机舱的进气结构包括具有连接外壁和内壁上游的内壁，外壁和进气口结构的基本上环形的主结构。 进气结构还包括第一声衰减结构，该第一声衰减结构具有孔声学皮肤，多孔芯和固定的后壁，内壁装有该第一声衰减结构，以及具有类似结构的第二声衰减结构， 进气口基本上在与内壁的接合处附近。 第一声衰减结构的后表皮与第二声衰减结构的后表皮对准，两个后皮都是结构的。
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7.发明申请ASSEMBLY INCLUDING A REVERSE THRUST DEVICE AND SYSTEM FOR ACTUATING SAID DEVICE 有权组装包括反转装置和用于致动装置的系统公开(公告)号：US20130263600A1
公开(公告)日：2013-10-10
申请号：US13691160
申请日：2012-11-30
申请人： Aircelle
IPC分类号： F02K1/76
CPC分类号： F02K1/763 , F02K1/1207 , F02K1/72 , F02K1/766
摘要： A reverse thrust device and a system for actuating the reverse thrust device is provided by the present disclosure. The device includes at least one cowl that is translatably mounted in a direction substantially parallel to a longitudinal axis of a nacelle. The actuation system includes an actuation means that is capable of activating translational and rotational movement of the cowl and a panel of a nozzle. The actuation system also includes a downstream locking means for the nozzle and the cowl. The downstream locking means includes at least two reversible states, one of the states being a locked state in which the downstream locking means is suitable for locking the panel of the nozzle into a position for varying the section for outputting the nozzle with the cowl.
摘要翻译： 通过本公开提供了反推力装置和用于致动反推力装置的系统。 该装置包括至少一个整流罩，其可平移地安装在基本上平行于机舱的纵向轴线的方向上。 致动系统包括致动装置，其能够启动整流罩和喷嘴的面板的平移和旋转运动。 致动系统还包括用于喷嘴和整流罩的下游锁定装置。 下游锁定装置包括至少两个可逆状态，其中一个状态是锁定状态，其中下游锁定装置适于将喷嘴的面板锁定到用于改变用于输出具有整流罩的喷嘴的部分的位置。
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公开(公告)号：US20130234447A1
公开(公告)日：2013-09-12
申请号：US13867904
申请日：2013-04-22
申请人： AIRCELLE
发明人： Patrick Gonidec
IPC分类号： E05C19/12
CPC分类号： E05B83/243 , B64D29/06 , E05B15/022 , E05B17/2038 , E05B41/00 , E05B53/003 , E05B63/24 , E05B83/16 , E05C19/12 , Y10T292/0911 , Y10T292/0936 , Y10T292/0956 , Y10T292/1089
摘要： A locking device includes a bolt capable of engaging with a corresponding hook, the bolt being mounted against a resilient return spring that tends to return the bolt into a spaced apart position. The locking device further includes a detection linkage, which is moveable between a first position and a second position. In the first position, the linkage enables unlocking of the bolt and the hook. In the second position, the linkage engages with a portion of the locking pair so as to block the unlocking.
摘要翻译： 锁定装置包括能够与相应的钩接合的螺栓，所述螺栓抵靠弹性复位弹簧安装，所述弹性复位弹簧倾向于将螺栓返回到间隔开的位置。 锁定装置还包括可在第一位置和第二位置之间移动的检测连杆机构。 在第一位置，联动装置使得能够解锁螺栓和钩子。 在第二位置，连杆与锁定对的一部分相配合，以阻止解锁。
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公开(公告)号：US20160040624A1
公开(公告)日：2016-02-11
申请号：US14797587
申请日：2015-07-13
申请人： AIRCELLE
CPC分类号： F02K1/06 , F01D25/24 , F02K1/09 , F02K1/38 , F02K1/46 , F05D2220/323 , Y02T50/671
摘要： A nacelle jet pipe is equipped with a device for regulating the pressure of a flow of air leaving the jet pipe. The device includes an annular element surrounding the downstream end of the jet pipe, and an adjuster to adjust the position of part of the annular element in relation to the downstream end of the jet pipe. In particular, the annular element forms, with the downstream end of the jet pipe, a constricted zone the widest part of which is situated upstream of the narrowest part and the profile of which can be varied according to the position of the annular element.
摘要翻译： 机舱喷射管配备有用于调节离开喷射管的空气流的压力的装置。 该装置包括围绕喷射管的下游端的环形元件和调节器，用于相对于喷射管的下游端调节环形元件的一部分的位置。 特别地，环形元件与喷射管的下游端形成收缩区，其最宽的部分位于最窄部分的上游，并且其轮廓可以根据环形元件的位置而变化。
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公开(公告)号：US20150210400A1
公开(公告)日：2015-07-30
申请号：US14678200
申请日：2015-04-03
申请人： AIRCELLE
CPC分类号： B64D15/16 , B64D15/04 , B64D15/12 , B64D29/06 , B64D33/02 , B64D2033/0233 , F01D25/005
摘要： The present disclosure concerns a component of an aircraft nacelle formed from at least one composite structure and one heating element. The nacelle includes frost protector, and the composite structure has a matrix reinforced by at least a material of which the heat conductivity at ambient temperature that is greater than or equal to 800 W·m−1·K−1, so as to provide transverse heat conductivity within the nacelle.
摘要翻译： 本公开涉及由至少一个复合结构和一个加热元件形成的飞机机舱的部件。 机舱包括防霜保护器，复合结构具有通过至少一种在环境温度下的导热率大于或等于800W·m-1·K-1的材料来增强的基体，从而提供横向 机舱内的导热系数。
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