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Locking device locking ring to hold the shovel in the axial direction, KNOT, DISC / ring of gas turbine engines, the rotor of gas turbine engines and gas turbine engines

机译：锁定装置锁定环，用于在轴向方向上固定铲子，燃气涡轮发动机的KNOT，DISC /环，燃气涡轮发动机的转子和燃气涡轮发动机

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摘要

1.the device u0441u0442u043eu043fu043eu0440u0435u043du0438u00a0 in rotation locking ring (20) of the blades (16) on the disk (10), a rotor gas turbine u0434u0432u0438u0433u0430u0442u0435u043bu00a0 essentially in the direction of u0443u043fu043eu043cu00a0u043du0443u0442u043eu0433u043e u0433u0430u0437u043eu0442u0443 u043eu0441u0435u0432u043eu043c u0440u0431u0438u043du043du043eu0433u043e u0434u0432u0438u0433u0430u0442u0435u043bu00a0 and u0443u043fu043eu043cu00a0u043du0443u0442u044bu0439 disk (10), a rotor equipped with hooks (6, 62, 64, 66) are implemented on its circumference and restricting cannelured (22) dl u00a0 installation u0443u043fu043eu043cu00a0u043du0443u0442u043eu0433u043e locking ring (20).u0441u043eu0441u0442u0430u0432u043bu00a0u044eu0449u0438u043cu0438 consistently the first locking hook (62), a second locking cam (64), and a third locking hook (66), with u0443u043fu043eu043cu00a0u043du0443u0442u044bu0439 second locking cam (64) u0440u0430u0441u043fu043eu043bu043e u0443u043fu043eu043cu00a0u043du0443u0442u044bu043cu0438) between the first and third u0441u0442u043eu043fu043eu0440u043du044bu043cu0438 hooks (62, 66), and u0443u043fu043eu043cu00a0u043du0443u0442u043eu0435 closing ring (20) includes a counter (24) and two protuberances (30) made of rings each side of the u0443u043fu043eu043cu00a0u043du0443u0442u043eu0433u043e slit (24).u043eu0442u043bu0438u0447u0430u044eu0449u0435u0435u0441u00a0 so that the protrusions (30) on the u0437u0430u043fu043eu0440u043du043eu043c ring (20) u043eu043fu0440u0435u0434u0435u043bu00a0u044eu0442 so that after installing the locking ring (20) in the slot (22) two speaking pa (30) were in the position of rest, respectively, in the first locking hook (62), and a third locking hook (66), a slit (24) u043fu0435u0440u0435u043au0440u044bu0432u0430u043bu0441u00a0 second shut-off hook (64).;2. the device u0441u0442u043eu043fu043eu0440u0435u043du0438u00a0 at rolling on p.1, u043eu0442u043bu0438u0447u0430u044eu0449u0435u0435u0441u00a0, first (62) and the third (66) are provided with stop hooks, each of u0431u043bu043eu043au0438u0440u043eu0432u043eu0447u043du0443u044e line (144) on the opposite side to the side, opposite to the u043du0430u0445u043eu0434u00a0u0449u0435u0439u0441u00a0 u0442u043eu0440u043eu0433u043e locking hook (64), and protrusions (30) of the stop ring (20) is provided, each of the contact line (32) directed toward the slit (24).and u0431u043bu043eu043au0438u0440u043eu0432u043eu0447u043du044bu0435 edge (144) interact with the contact u0433u0440u0430u043du00a0u043cu0438 (32) u0434u043bu00a0 u043fu0440u0438u0432u0435u0434u0435u043du0438u00a0 protrusions (30) in a position of rest in the first (62) and the third (66) provided with stop hooks.;3. the device u0441u0442u043eu043fu043eu0440u0435u043du0438u00a0 on any of the ap.1 and 2, u043eu0442u043bu0438u0447u0430u044eu0449u0435u0435u0441u00a0 what cannelured (22) has two sides, namely the inner wall that is closest to the disk (10), a rotor, and the outer wall, the most remote of the t disk (10), a rotor, and u043au0430u0436u0434u0430u00a0 u0431u043bu043eu043au0438u0440u043eu0432u043eu0447u043du0430u00a0 line (144) u043du0430u0445u043eu0434u0438u0442u0441u00a0 the u0441u0442u043eu043fu043eu0440u043du043eu043c hook (62, 66) and implemented in u043eu0441u0435u0432u043eu043c direction, u043du0430u0447u0438u043du0430u00a0 from freely floor surface u0443u043fu043eu043cu00a0u043du0443u0442u043eu0433u043e locking hook (62,66) to the inner wall of u0443u043fu043eu043cu00a0u043du0443u0442u043eu0433u043e circular groove (22).;4. the device u0441u0442u043eu043fu043eu0440u0435u043du0438u00a0 on one of the u043fu043f.2 and 3, u043eu0442u043bu0438u0447u0430u044eu0449u0435u0435u0441u00a0, u0431u043bu043eu043au0438u0440u043eu0432u043eu0447u043du044bu0435 edge (144) directed in the radial plane of the rotor disk (10).;5. the device u0441u0442u043eu043fu043eu0440u0435u043du0438u00a0 on one of the u043fu043f.2 and 3, u043eu0442u043bu0438u0447u0430u044eu0449u0435u0435u0441u00a0, u0431u043bu043eu043au0438u0440u043eu0432u043eu0447u043du044bu0435 edge (144) are designed to plane, inclined on the radial plane of the dis a rotor (10).;6.the node drive / ring (10, 20) gas turbine u0434u0432u0438u0433u0430u0442u0435u043bu00a0 containing a closing ring (20) containing section (24), and a disk rotor (10) equipped with hooks (6, 62, 64, 66), uniformly in u044bu043fu043eu043bu043du0435u043du043du044bu043cu0438 on its circumference and restricting cannelured (22) u0434u043bu00a0 installation u0443u043fu043eu043cu00a0u043du0443u0442u043eu0433u043e locking ring (20), u043eu0442u043bu0438u0447u0430u044eu0449u0438u0439u0441u00a0 so that the disk (10), a rotor contains pic u043bu0435u0434u043eu0432u0430u0442u0435u043bu044cu043du043e first locking hook (62).the second locking hook (64), and a third locking hook (66), with a closing ring (20) contains two protuberances (30) performed on one edge of each side of the incision. (24), and protrusions (30) on the u0437u0430u043fu043eu0440u043du043eu043c ring (20) u043eu043fu0440u0435u0434u0435u043bu00a0u044eu0442 thusafter the installation of stop rings (20) in a cannelured (22) both protuberances (30) are in the position of rest, respectively, in the first locking hook (62) and the third u0441u0442u043eu043fu043e u0440u043du044bu0439 hook (66), a slit (24) u043fu0435u0440u0435u043au0440u044bu0432u0430u043bu0441u00a0 second shut-off hook (64).;7. the node drive / ring (10, 20) for p.u043eu0442u043bu0438u0447u0430u044eu0449u0438u0439u0441u00a0 6, so that the first (62) and the third (66) are provided with stop hooks, each of u0431u043bu043eu043au0438u0440u043eu0432u043eu0447u043du0443u044e line (144) on its opposite side to side, u043du0430u0445u043eu0434u00a0u0449u0435u0439u0441u00a0 e.g. u043eu0442u0438u0432 second locking cams (64), the projections (30) of the stop ring (20) is provided, each of the contact line (32) directed toward the slit (24).and u0431u043bu043eu043au0438u0440u043eu0432u043eu0447u043du044bu0435 edge (144) interact with the contact u0433u0440u0430u043du00a0u043cu0438 (32) u0434u043bu00a0 u043fu0440u0438u0432u0435u0434u0435u043du0438u00a0 protrusions (30) in a position of rest in the first (62) and the third (66) provided with stop hooks.;8. rotor gas turbine u0434u0432u0438u0433u0430u0442u0435u043bu00a0, u043eu0442u043bu0438u0447u0430u044eu0449u0438u0439u0441u00a0 order that contains the device u0441u0442u043eu043fu043eu0440u0435u043du0438u00a0 on any of the u043fu043f.1 - 5 and / or node drive / ring (10, 20) for one of u043fu043f.6 and 7.;9. turboshaft, u043eu0442u043bu0438u0447u0430u044eu0449u0438u0439u0441u00a0 order that contains the device u0441u0442u043eu043fu043eu0440u0435u043du0438u00a0 on any of the u043fu043f.1 - 5 and / or node drive / ring (10, 20) for one of u043fu043f.6 and 7.;10. turboshaft on p.9, u043eu0442u043bu0438u0447u0430u044eu0449u0438u0439u0441u00a0, u00a0u0432u043bu00a0u0435u0442u0441u00a0 aviation engine.

机译：1.盘式燃气轮机（u0434）上的叶片（16）的旋转锁定环（20）中的装置 u0441 u0442 u043e u043f u043e u0440 u0435 u043d u0438 u00a0 u0432 u0438 u0433 u0430 u0442 u0435 u043b u00a0本质上是在 u0443 u043f u043e u043c u00a0 u043d u0443 u0442 u043e u0433 u0433 u043e u0433 u0430 u0430 u0437 u043e u0442 u0443 u043e u0441 u0435 u0432 u043e u043c u0440 u0431 u0438 u043d u043d u043d u043e u0433 u043e u0434 u0432 u0438 u0433 u0430 u0442 u0435 u00a0和 u0443 u043f u043e u043c u00a0 u043d u0443 u0442 u044b u0439磁盘（10），在其圆周上安装了一个带有钩子（6、62、64、66）的转子，并限制了带槽（ 22）dl u00a0安装 u0443 u043f u043e u043c u00a0 u043d u0443 u0442 u043e u0433 u043e锁紧环（20）。 u0441 u043e u0441 u0441 u0442 u0430 u0432 u043b u0040 u044e u0449 u0438 u043c u0438始终使用 u0443 u043f u043e u043c u始终固定第一锁定钩（62），第二锁定凸轮（64）和第三锁定钩（66）。 00a0 u043d u0443 u0442 u044b u0439第二个锁定凸轮（64） u0440 u0430 u0441 u043f u043e u043b u043e u0443 u043f u043e u043c u00a0 u043d u0443 u0442 u044b u044b u0441 u0442 u043e u043f u043e u0440 u043d u044b u043c u0438钩子（62、66）和 u0443 u043f u043f u043e u043e u043c u043c u00d0 u043d u0443 u0442 u043e u0435闭合环（20）包括一个计数器（24）和两个由环形物组成的突起（30），每个环的侧面都为 u0443 u043f u043e u043c u00a0 u043d u0443 u0442 u043e u0433 u043e狭缝（24）。 u043e u0442 u043b u0438 u0447 u0430 u044e u0449 u0435 u0435 u0441 u00a0以便 u0437 u0430 u043f u043e 上的突起（30） u0440 u043d u043e u043c环（20） u043e u043f u0440 u0435 u0434 u0435 u043b u00a0 u044e u0442以便在将锁紧环（20）安装在插槽（22）中后两个说（30）分别处于第一锁定钩（62）和第三锁定钩（66）的静止位置，以及一个狭缝（24） u043f u0435 u0440 u0435 u043a u0440 u044b u0432 u 0430 u043b u0441 u00a0第二个关闭钩（64）.; 2。在第1页上滚动设备 u0441 u0442 u043e u043f u043e u0440 u0435 u043d u0438 u00a0， u043e u0442 u043b u0438 u0447 u0430 u044e u0449 u0435 u0435 u0435 u0441 u00a0，第一（62）和第三（66）配有止动钩，每个 u0431 u043b u043e u043a u0438 u0440 u043e u0432 u043e u0447 u043d u0443 u044e行（ 144）相对的一侧，与 u043d u0430 u0445 u043e u0434 u00a0 u0449 u0435 u0439 u0441 u00a0 u0442 u043e u0440 u043e u0433 u043e 64），并设有止动环（20）的突起（30），每条接触线（32）都朝向狭缝（24）。和 u0431 u043b u043e u043a u0438 u0440 u043e u0432 u043e u0447 u043d u044b u0435边（144）与联系人 u0433 u0440 u0430 u043d u00a0 u043c u0438（32） u0434 u043b u00a0 u043f u0440 u0438 u0432 u0435 u0434 u0435 u043d u0438 u00a0突起（30）位于第一（62）和第三（66）带有止动钩的静止位置; 3。在ap.1和2中的任何一个上，设备 u0441 u0442 u043e u043f u043e u0440 u0435 u043d u0438 u00a0 u043e u0442 u043b u0438 u0447 u04447 u0430 u044e u0449 u0435 u0435 u0441 u00a0管状（22）具有两个侧面，即最靠近圆盘（10）的内壁，一个转子和一个距t圆盘（10）最远的外壁，一个转子和 u043a u0430 u0436 u0434 u0430 u00a0 u0431 u043b u043e u043a u0438 u0440 u043e u0432 u043e u0447 u043d u0430 u00a0行（144） u043d u0430 u04a u043e u0434 u0438 u0442 u0441 u00a0 u0441 u0442 u043e u043f u043e u0440 u043d u043e u043c挂钩（62、66）并在 u043e u0441 u0435 u0432 u043e中实现 u043c方向， u043d u0430 u0447 u0438 u043d u0430 u00a0从自由地面 u0443 u043f u043e u043c u00a0 u043d u0443 u0442 u043e u043e u0433 u043e锁定钩（62,66 ）到 u0443 u043f u043e u043c u00a0 u043d u0443 u0442 u043e u0433 u043e圆形凹槽（22）的内壁。; 4。 u043f u043f.2和3之一， u043e u0442 u043b u043b u0438 u0447 u0430 u044e 上的设备 u0441 u0442 u043e u043f u043e u0440 u0435 u043d u0438 u00a0 u0449 u0435 u0435 u0441 u00a0， u0431 u043b u043e u043a u0438 u0440 u043e u0432 u043e u0447 u043d u044b u0435边缘（144）指向转子盘的径向平面（ 10）.; 5。 u043f u043f.2和3之一， u043e u0442 u043b u043b u0438 u0447 u0430 u044e 上的设备 u0441 u0442 u043e u043f u043e u0440 u0435 u043d u0438 u00a0 u0449 u0435 u0435 u0441 u00a0， u0431 u043b u043e u043a u043a u0438 u0440 u043e u0432 u043e u0447 u043d u044b u0435边缘（144）设计成在径向上倾斜的平面转子（10）的旋转;; 6.节点驱动器 /环（10、20）燃气轮机 u0434 u0432 u0438 u0433 u0430 u0442 u0435 u043b u00a0包含封闭环（20）容纳部分（24）和装有钩子（6、62、64、66）的圆盘转子（10），统一在 u044b u043f u043e u043b u043d u0435 u043d u043d u044b u043c u0438的圆周上，并限制安装了套管（22） u0434 u043b u00a0安装 u0443 u043f u043e u043c u00a0 u043d u0443 u0442 u043e u0433 u043e锁紧环（20）， u043e u0442 u043b u0438 u0447 u0430 u044e u0449 u0438 u0439 u0441 u00a0这样磁盘（10）转子包含pic u043b u0435 u0434 u043e u0432 u0430 u0442 u0435 u043b u044c u043d u043e第一锁定钩（62），第二锁定钩（64）和第三锁定钩（如图66所示，带有一个闭合环（20），在切口的每一侧的一个边缘上具有两个突起（30）。（24）和 u0437 u0430 u043f u043e u0440 u043d u043e u043c环上的突起（30）（20） u043e u043f u0440 u0435 u0434 u0435 u043b u043b u00a0 u044e 因此，在将止动环（20）安装到管状（22）中之后，两个突起（30）分别位于第一锁定钩（62）和第三锁定钩（62）中的静止位置。 u043e u0440 u043d u044b u0439挂钩（66），一条狭缝（24） u043f u0435 u0440 u0435 u043a u0440 u044b u0432 u0430 u043b u0441 u00a0第二个关闭挂钩（64 ）;; 7。 p。 u043e u0442 u043b u0438 u0447 u0430 u044e u0449 u0438 u0439 u0441 u00a0 6的节点驱动器 /振铃（10、20），因此第一个（62）和第三个（66）带有止动钩，每对 1443 u0431 u043b u043e u043a u0438 u0440 u043e u0432 u043e u0447 u043d u0433 u044e线（144） u0430 u0445 u043e u0434 u00a0 u0449 u0435 u0439 u0441 u00a0例如 u043e u0442 u0438 u0432第二个锁定凸轮（64），设置了止动环（20）的突起（30），每个接触线（32）都指向狭缝（24）。 u043b u043e u043a u0438 u0440 u043e u0432 u043e u0447 u043d u044b u0435边缘（144）与联系人 u0433 u0440 u0430 u043d u00a0 u043c u0438（32） u0434 u043b u00a0 u043f u0440 u0438 u0432 u0435 u0434 u0435 u043d u0438 u00a0突起（30）在第一个（62）和第三个（66）中具有止动钩的位置。 ; 8。转子燃气轮机 u0434 u0432 u0438 u0433 u0430 u0442 u0435 u043b u00438 u0447 u0430 u044e u0449 u0438 u0438 u0439 u0441 u0040 u043f u043f.1-5中任何一个上的设备 u0441 u0442 u043e u043f u043e u0440 u0435 u043d u043438 u00a0和 /或节点驱动器 /环（10、20）之一 u043f u043f.6和7.; 9。涡轮轴， u043e u0442 u043b u0438 u0447 u0430 u044e u0449 u0438 u0439 u0441 u00a0包含设备 u0441 u0442 u043e u043f u043e u043e u0440 u0435 u043d u0438 u043f u043f.1-5和 /或节点驱动器 /环（10、20）上的 u043f u043f.6和7.中的任何一个u00a0 ;; 10。第9页上的涡轮轴， u043e u0442 u043b u0438 u0447 u0430 u044e u0449 u0438 u0439 u0441 u00a0， u00a0 u0432 u043b u00a0 u0435 u0442 u0441 u00a0

著录项

公开/公告号RU2006131299A

专利类型
公开/公告日2008-03-10

原文格式PDF
申请/专利权人 СНЕКМА (FR);
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申请/专利号RU20060131299
发明设计人 ДЕЗУШ ЛОРАН ЖИЛЬ (FR);
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申请日2006-08-30
分类号F02C1;
国家 RU
入库时间 2022-08-21 19:51:11

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