WO2019109197A1 - Turbine housing - Google Patents

Turbine housing Download PDF

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Publication number
WO2019109197A1
WO2019109197A1 PCT/CN2017/114359 CN2017114359W WO2019109197A1 WO 2019109197 A1 WO2019109197 A1 WO 2019109197A1 CN 2017114359 W CN2017114359 W CN 2017114359W WO 2019109197 A1 WO2019109197 A1 WO 2019109197A1
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WO
WIPO (PCT)
Prior art keywords
wheel cover
turbine
segments
adjacent
turbine wheel
Prior art date
Application number
PCT/CN2017/114359
Other languages
French (fr)
Chinese (zh)
Inventor
莫品亮
李志胜
Original Assignee
贵州智慧能源科技有限公司
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
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Application filed by 贵州智慧能源科技有限公司 filed Critical 贵州智慧能源科技有限公司
Priority to PCT/CN2017/114359 priority Critical patent/WO2019109197A1/en
Publication of WO2019109197A1 publication Critical patent/WO2019109197A1/en

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Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D25/00Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/24Casings; Casing parts, e.g. diaphragms, casing fastenings

Definitions

  • the present invention relates to the field of turbine covers, and more particularly to a segmented turbine wheel cover.
  • the turbine wheel cover in the gas turbine protects the turbine blades and seals, but the full-circle turbine wheel cover is subjected to thermal expansion after work and is subjected to stress extrusion. In the long-term, stress fatigue is easily caused to fail.
  • the present invention proposes a turbine wheel cover that can solve the above problems.
  • the present invention provides a turbine wheel cover for protecting a turbine, the wheel cover including a wheel cover body and a support member supporting the wheel cover body, the wheel cover body being divided into a plurality of wheel cover segments, and the A gap allowance is left between each adjacent two wheel cover segments.
  • each of the wheel cover segments is provided with a hook
  • the support member is provided with a first slot corresponding to the hook
  • each of the wheel covers is divided by A hook is fixed to the first slot.
  • the turbine wheel cover further includes a positioning pin; the hook is provided with a second slot; the support member is inserted into the second slot through the positioning pin to The wheel cover is fixed to the support member as shown.
  • the wheel cover body is formed by using a locking piece between each adjacent two wheel cover segments, and the locking piece is used to restrict the wheel cover block from moving in the radial direction. .
  • the wheel cover segments are provided with a notch for mounting the locking piece at both ends in the circumferential direction, and the locking piece is shared between each adjacent two wheel cover segments. In order to ensure the sealing effect of the wheel cover body.
  • the locking tab includes a first portion interposed with the notch and a second portion extending perpendicularly from the first portion.
  • the wheel cover body is divided into eight pieces of the wheel cover segments, and the eight wheel cover segments are all the same.
  • the margin remaining between each adjacent two wheel cover segments is equivalent.
  • the sum of the clearance margins remaining for each adjacent two wheel shroud segmented brackets is the upper limit of the radial expansion of the turbine wheel shroud at the operating temperature.
  • the sum of the gap allowance between each adjacent two wheel cover segments is 3.5 mm.
  • the present invention proposes a segmented turbine wheel cover, the wheel cover body is connected to the support member, and the wheel cover body is divided into a plurality of wheel cover segments, and each two wheel cover blocks are left between blocks.
  • the block of the present invention is compared with the full ring type turbine wheel cover.
  • the turbine wheel cover is easier to install and simple to machine.
  • a locking piece is used between each adjacent two wheel cover blocks to limit the integrity of the wheel cover body.
  • FIG. 1 is an assembled view of a turbine wheel cover in accordance with a consistent embodiment of the present invention.
  • Figure 2 is a perspective view of the turbine wheel cover of Figure 1.
  • Figure 3 is a schematic illustration of a wheel cover segmentation.
  • Figure 4 is a cross-sectional view of the wheel cover block of Figure 3.
  • Figure 5 is a schematic view showing the installation of the two wheel cover segments shown in Figure 3.
  • Figure 6 is a schematic view showing the structure of the lock piece.
  • a turbine wheel cover 99 as shown in FIG. 1 includes a wheel house body 10 and a support member 20 that supports the wheel house body 10.
  • the wheel house body 10 is divided into eight wheel cover segments 11, it being understood that this is only one embodiment of the present invention. In other embodiments, the wheel house body 10 can also be divided into The other number of wheel cover segments 11 does not limit the number of the wheel house main body 10 divided into the wheel cover segments 11.
  • each wheel cover block 11 is provided with hooks 13 and a second slot 15 is provided between each of the hooks 13.
  • the support member 20 is provided with a first notch 23 corresponding to the claw 13 and a positioning pin 25 corresponding to the second notch 15.
  • the hook 13 and the positioning pin 25 are respectively engageable in the first notch 23 and the second notch 15, so that the wheel cover segment 11 is fixed to the support member 20.
  • the wheel cover body 10 is formed by sequentially fixing each wheel cover block 11 to the support member 20.
  • the support of the wheel house main body 10 by the support member 20 ensures a good gap between the wheel house main body 10 and the turbine blades.
  • the block type turbine wheel cover 99 of the present embodiment is more convenient to install and simpler to process.
  • a gap allowance 16 is left between each two adjacent wheel cover segments 11, and the clearance margin 16 causes the wheel cover 10 to There is an expansion margin in the circumferential direction, and the clearance margin 16 is the upper limit of the expansion of the wheel house main body 10 at the operating temperature.
  • a gap allowance 16 is left between each two adjacent wheel cover segments 11, it being understood that this is only one embodiment of the present invention, in other embodiments, two adjacent wheels.
  • the gap allowance 16 is not limited between the cover segments 11 and is not limited by the present invention.
  • the sum of the gap margins 16 is 3.5 mm. It should be understood that this is only one embodiment of the present invention. In other embodiments, the gap margin 16 may be set according to different expansion upper limit values. The other values are determined, and the specific value of the gap margin 16 is not limited in the present invention.
  • the lock piece 18 is used between the two adjacent wheel cover segments to define the wheel cover body.
  • the locking tab 18 limits the radial movement of the wheel cover segments 11 and also ensures the integrity of the wheel house body 10, preventing the gas in the turbine wheel housing 99 from circulating with the outside air.
  • a notch 19 for mounting the locking piece 18 is provided at both ends of the wheel cover block 11 in the circumferential direction, and a locking piece 18 is shared between each adjacent two wheel cover segments 11.
  • the two notches 19 at the end of each adjacent two-wheel cover block 11 form a space for receiving the locking piece 18, the width of which is equivalent to the width of the locking piece 18, that is, the width of the notch 19 is two points of the width of the locking piece 18. one.
  • the locking tab 19 includes a first portion 181 that is inserted into the notch 18 and a second portion 182 that extends perpendicularly from the first portion 181, and has an overall L-shaped configuration. The sealing effect of the wheel house main body 10 is also ensured by inserting the locking piece 18 in the notch 19, that is, without affecting the thermal expansion in the circumferential direction when the wheel cover block 11 is in operation.
  • the present invention provides a segmented turbine wheel cover, the wheel cover body 10 is coupled to the support member 20, and the wheel cover body 10 is divided into a plurality of wheel cover segments 11, each of which is divided into two segments. Between the blocks, there is a gap 16 for the wheel cover body 10 to be thermally expanded during operation, which avoids the failure of the wheel house main body 10 to undergo stress extrusion due to thermal expansion under long-term operation, and is compared with the full-circular turbine wheel.
  • the cover, the segmented turbine wheel cover of the present invention is easier to install and simple to machine.
  • the locking piece 18 is used for limiting between each adjacent two wheel cover segments 11, thereby ensuring the integrity of the wheel cover body 10.

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Connection Of Plates (AREA)

Abstract

A turbine housing for protecting a turbine. The housing comprises a housing main body (10) and a supporting member (20) for supporting the housing main body (10). The housing main body (10) is divided into a plurality of housing segments (11). A gap allowance (16) is arranged between every two adjacent housing segments (11). The segmented turbine housing can be processed and installed easily.

Description

涡轮轮罩Turbine wheel cover 技术领域Technical field
本发明涉及涡轮罩领域,特别涉及一种分块式涡轮轮罩。The present invention relates to the field of turbine covers, and more particularly to a segmented turbine wheel cover.
背景技术Background technique
燃气轮机中的涡轮轮罩起保护涡轮叶片和密封作用,但是整环式的涡轮轮罩在工作时受热膨胀后产生应力挤压,长期以往,易产生应力疲劳而失效。The turbine wheel cover in the gas turbine protects the turbine blades and seals, but the full-circle turbine wheel cover is subjected to thermal expansion after work and is subjected to stress extrusion. In the long-term, stress fatigue is easily caused to fail.
技术问题technical problem
有鉴于此,本发明提出一种可以解决上述问题的涡轮轮罩。In view of this, the present invention proposes a turbine wheel cover that can solve the above problems.
技术解决方案Technical solution
本发明提出一种涡轮轮罩,用于保护涡轮,所述轮罩包括轮罩主体和支撑所述轮罩主体的支撑部件,所述轮罩主体分割成若干块轮罩分块,且所述每相邻两块轮罩分块之间留有间隙余量。The present invention provides a turbine wheel cover for protecting a turbine, the wheel cover including a wheel cover body and a support member supporting the wheel cover body, the wheel cover body being divided into a plurality of wheel cover segments, and the A gap allowance is left between each adjacent two wheel cover segments.
在一实施例中,所述每个轮罩分块上设有钩爪,所述支撑部件设有与所述钩爪对应的第一槽口,所述每个轮罩分块通过将所述钩爪固定在所述第一槽口上。In an embodiment, each of the wheel cover segments is provided with a hook, and the support member is provided with a first slot corresponding to the hook, and each of the wheel covers is divided by A hook is fixed to the first slot.
在一实施例中,所述涡轮轮罩还包括定位销;所述钩爪上设有第二槽口;所述支撑部件通过所述定位销穿卡合在所述第二槽口内将所述轮罩分块固定在所示支撑部件上。In an embodiment, the turbine wheel cover further includes a positioning pin; the hook is provided with a second slot; the support member is inserted into the second slot through the positioning pin to The wheel cover is fixed to the support member as shown.
在一实施例中,所述每相邻两个轮罩分块之间采用锁片进行限位构成所述轮罩主体,所述锁片用以限制所述轮罩分块在径向上串动。In an embodiment, the wheel cover body is formed by using a locking piece between each adjacent two wheel cover segments, and the locking piece is used to restrict the wheel cover block from moving in the radial direction. .
在一实施例中,所述轮罩分块沿周向上的两端都设有用于安装所述锁片的缺口,所述每相邻两个轮罩分块之间共用一所述锁片,以保证所述轮罩主体的密封作用。In an embodiment, the wheel cover segments are provided with a notch for mounting the locking piece at both ends in the circumferential direction, and the locking piece is shared between each adjacent two wheel cover segments. In order to ensure the sealing effect of the wheel cover body.
在一实施例中,所述锁片包括插设与所述缺口的第一部分和自第一部分垂直延伸的第二部分。In an embodiment, the locking tab includes a first portion interposed with the notch and a second portion extending perpendicularly from the first portion.
在一实施例中,所述轮罩主体分割成八块所述轮罩分块,所述八块轮罩分块均相同。In an embodiment, the wheel cover body is divided into eight pieces of the wheel cover segments, and the eight wheel cover segments are all the same.
在一实施例中,所述每相邻两轮罩分块之间留有的间隙余量相当。In an embodiment, the margin remaining between each adjacent two wheel cover segments is equivalent.
在一实施例中,所述每相邻两块轮罩分块支架留有的间隙余量总和为所述涡轮轮罩在工作温度下径向膨胀的上限值。In one embodiment, the sum of the clearance margins remaining for each adjacent two wheel shroud segmented brackets is the upper limit of the radial expansion of the turbine wheel shroud at the operating temperature.
在一实施例中,所述每相邻两块轮罩分块之间留有间隙余量的总和为3.5mm。In one embodiment, the sum of the gap allowance between each adjacent two wheel cover segments is 3.5 mm.
有益效果Beneficial effect
综上所述,本发明提出了一种分块式的涡轮轮罩,轮罩主体连接在支撑部件上,将轮罩主体分割成若干块轮罩分块,每两轮罩分块之间留有供轮罩主体在工作时受热膨胀的间隙余量,避免了轮罩主体在长期工作下因受热膨胀产生应力挤压而失效,而且相比较整环式的涡轮轮罩,本发明的分块式涡轮轮罩更易于安装,加工简单。另外,每相邻两个轮罩分块之间还采用锁片进行限位,保证了轮罩主体的整体性。In summary, the present invention proposes a segmented turbine wheel cover, the wheel cover body is connected to the support member, and the wheel cover body is divided into a plurality of wheel cover segments, and each two wheel cover blocks are left between blocks. There is a margin for the thermal expansion of the wheel cover body during operation, which avoids the failure of the wheel cover body to undergo stress extrusion due to thermal expansion under long-term operation, and the block of the present invention is compared with the full ring type turbine wheel cover. The turbine wheel cover is easier to install and simple to machine. In addition, a locking piece is used between each adjacent two wheel cover blocks to limit the integrity of the wheel cover body.
附图说明DRAWINGS
图1是本发明一致实施方式的涡轮轮罩的装配图。1 is an assembled view of a turbine wheel cover in accordance with a consistent embodiment of the present invention.
图2是图1所示涡轮轮罩的立体图。Figure 2 is a perspective view of the turbine wheel cover of Figure 1.
图3是轮罩分块的示意图。Figure 3 is a schematic illustration of a wheel cover segmentation.
图4是图3所示轮罩分块的剖面图。Figure 4 is a cross-sectional view of the wheel cover block of Figure 3.
图5是两个图3所示轮罩分块的安装示意图。Figure 5 is a schematic view showing the installation of the two wheel cover segments shown in Figure 3.
图6是锁片的结构示意图。Figure 6 is a schematic view showing the structure of the lock piece.
图中,99-涡轮轮罩,10-轮罩主体,11-轮罩分块,13-钩爪,15-第二槽口,16-间隙余量,18-锁片,181-锁片的第一部分,182-锁片的第二部分,19-缺口,20-支撑部件,23-第一槽口,25-定位销。In the figure, 99-turbine wheel cover, 10-wheel cover body, 11-wheel cover block, 13-hook claw, 15-second notch, 16-gap allowance, 18-lock piece, 181-lock piece The first part, 182-the second part of the locking piece, 19-notch, 20-supporting part, 23-first notch, 25-positioning pin.
本发明的实施方式Embodiments of the invention
在详细描述实施例之前,应该理解的是,本实用新型不限于本申请中下文或附图中所描述的详细结构或元件排布。本实用新型可为其它方式实现的实施例。而且,应当理解,本文所使用的措辞及术语仅仅用作描述用途,不应作限定性解释。本文所使用的“包括”、“包含”、“具有”等类似措辞意为包含其后所列出之事项、其等同物及其它附加事项。特别是,当描述“一个某元件”时,本实用新型并不限定该元件的数量为一个,也可以包括多个。Before the embodiments are described in detail, it is understood that the invention is not limited to The invention may be embodied in other ways. Also, it will be understood that the phraseology and terminology used herein are for the purpose of description The words "including", "comprising", "having", and <RTIgt; </ RTI> <RTIgt; </ RTI> used herein are meant to include the items listed thereafter, their equivalents, and other additional items. In particular, when describing "a certain element", the present invention does not limit the number of the elements to one, and may include a plurality.
如图1所示的涡轮轮罩99,其包括轮罩主体10和支撑轮罩主体10的支撑部件20。A turbine wheel cover 99 as shown in FIG. 1 includes a wheel house body 10 and a support member 20 that supports the wheel house body 10.
在本实施例中,轮罩主体10分割成八块轮罩分块11,应当理解的是,这仅作为本发明的一种实施方式,在其他实施例中,轮罩主体10也可分割成其他数量的轮罩分块11,本发明对轮罩主体10分割成轮罩分块11的数量不作限定。In the present embodiment, the wheel house body 10 is divided into eight wheel cover segments 11, it being understood that this is only one embodiment of the present invention. In other embodiments, the wheel house body 10 can also be divided into The other number of wheel cover segments 11 does not limit the number of the wheel house main body 10 divided into the wheel cover segments 11.
如图2至图4所示,每一轮罩分块11上设有钩爪13,每一钩爪13之间设有第二槽口15。支撑部件20在设有与钩爪13对应的第一槽口23和对应第二槽口15的定位销25。钩爪13和定位销25分别可卡合在第一槽口23和第二槽口15内,使轮罩分块11固定在支撑部件20上。将每一轮罩分块11依次固定在支撑部件20上即可组成轮罩主体10。由支撑部件20对轮罩主体10的支撑,保证了轮罩主体10与涡轮叶片间存在良好的间隙。相对于整环式的涡轮轮罩,本实施例的分块式涡轮轮罩99安装更方便,加工更简单。As shown in FIG. 2 to FIG. 4, each wheel cover block 11 is provided with hooks 13 and a second slot 15 is provided between each of the hooks 13. The support member 20 is provided with a first notch 23 corresponding to the claw 13 and a positioning pin 25 corresponding to the second notch 15. The hook 13 and the positioning pin 25 are respectively engageable in the first notch 23 and the second notch 15, so that the wheel cover segment 11 is fixed to the support member 20. The wheel cover body 10 is formed by sequentially fixing each wheel cover block 11 to the support member 20. The support of the wheel house main body 10 by the support member 20 ensures a good gap between the wheel house main body 10 and the turbine blades. Compared with the full ring type turbine wheel cover, the block type turbine wheel cover 99 of the present embodiment is more convenient to install and simpler to process.
更具体地,为了防止涡轮轮罩10在工作时受热膨胀而产生应力挤压,每两块相邻的轮罩分块11之间留有间隙余量16,间隙余量16使得轮罩10在周向上有膨胀余量,间隙余量16为轮罩主体10在工作温度下膨胀的上限值。每两块相邻的轮罩分块11之间留有间隙余量16相当,应当理解的是,这仅作为本发明的一中实施方式,在其他实施例中,每两块相邻的轮罩分块11之间留有间隙余量16也可以不相当,本发明对此不作限定。More specifically, in order to prevent stress extrusion of the turbine wheel cover 10 during thermal expansion during operation, a gap allowance 16 is left between each two adjacent wheel cover segments 11, and the clearance margin 16 causes the wheel cover 10 to There is an expansion margin in the circumferential direction, and the clearance margin 16 is the upper limit of the expansion of the wheel house main body 10 at the operating temperature. A gap allowance 16 is left between each two adjacent wheel cover segments 11, it being understood that this is only one embodiment of the present invention, in other embodiments, two adjacent wheels. The gap allowance 16 is not limited between the cover segments 11 and is not limited by the present invention.
在本实施例中,间隙余量16的总和为3.5mm,应当理解的是,这仅是本发明的一个实施例,在其他实施例中,间隙余量16可根据不同的膨胀上限值设定成其他值,本发明对间隙余量16的具体值不作限定。In the present embodiment, the sum of the gap margins 16 is 3.5 mm. It should be understood that this is only one embodiment of the present invention. In other embodiments, the gap margin 16 may be set according to different expansion upper limit values. The other values are determined, and the specific value of the gap margin 16 is not limited in the present invention.
如图5至图6所示,所述每相邻两个轮罩分块之间采用锁片18进行限位构成所述轮罩主体。锁片18限制轮罩分块11在径向上串动,也保证了轮罩主体10的完整性,防止涡轮轮罩99内的气体与外界空气流通。As shown in FIG. 5 to FIG. 6 , the lock piece 18 is used between the two adjacent wheel cover segments to define the wheel cover body. The locking tab 18 limits the radial movement of the wheel cover segments 11 and also ensures the integrity of the wheel house body 10, preventing the gas in the turbine wheel housing 99 from circulating with the outside air.
轮罩分块11沿周向上的两端都设有用于安装锁片18的缺口19,每相邻的两轮罩分块11之间共用一锁片18。每相邻的两轮罩分块11相靠近的一端的两缺口19构成容纳锁片18的空间,该空间的宽度与锁片18的宽度相当,即缺口19宽度为锁片18宽度的二分之一。锁片19包括插设在缺口18内的第一部分181和自第一部分181垂直延伸的第二部分182,整体呈L型结构。通过将锁片18插设在缺口19内,即不影响轮罩分块11工作时在周向上的受热膨胀,也保证了轮罩主体10的密封作用。A notch 19 for mounting the locking piece 18 is provided at both ends of the wheel cover block 11 in the circumferential direction, and a locking piece 18 is shared between each adjacent two wheel cover segments 11. The two notches 19 at the end of each adjacent two-wheel cover block 11 form a space for receiving the locking piece 18, the width of which is equivalent to the width of the locking piece 18, that is, the width of the notch 19 is two points of the width of the locking piece 18. one. The locking tab 19 includes a first portion 181 that is inserted into the notch 18 and a second portion 182 that extends perpendicularly from the first portion 181, and has an overall L-shaped configuration. The sealing effect of the wheel house main body 10 is also ensured by inserting the locking piece 18 in the notch 19, that is, without affecting the thermal expansion in the circumferential direction when the wheel cover block 11 is in operation.
综上所述,本发明提出了一种分块式的涡轮轮罩,轮罩主体10连接在支撑部件20上,将轮罩主体10分割成若干块轮罩分块11,每两轮罩分块之间留有供轮罩主体10在工作时受热膨胀的间隙余量16,避免了轮罩主体10在长期工作下因受热膨胀产生应力挤压而失效,而且相比较整环式的涡轮轮罩,本发明的分块式涡轮轮罩更易于安装,加工简单。另外,每相邻两个轮罩分块11之间还采用锁片18进行限位,保证了轮罩主体10的整体性。In summary, the present invention provides a segmented turbine wheel cover, the wheel cover body 10 is coupled to the support member 20, and the wheel cover body 10 is divided into a plurality of wheel cover segments 11, each of which is divided into two segments. Between the blocks, there is a gap 16 for the wheel cover body 10 to be thermally expanded during operation, which avoids the failure of the wheel house main body 10 to undergo stress extrusion due to thermal expansion under long-term operation, and is compared with the full-circular turbine wheel. The cover, the segmented turbine wheel cover of the present invention is easier to install and simple to machine. In addition, the locking piece 18 is used for limiting between each adjacent two wheel cover segments 11, thereby ensuring the integrity of the wheel cover body 10.
本文所描述的概念在不偏离其精神和特性的情况下可以实施成其它形式。所公开的具体实施例应被视为例示性而不是限制性的。因此,本实用新型的范围是由所附的权利要求,而不是根据之前的这些描述进行确定。在权利要求的字面意义及等同范围内的任何改变都应属于这些权利要求的范围。The concepts described herein may be embodied in other forms without departing from the spirit and scope. The specific embodiments disclosed are to be considered as illustrative and not restrictive. Therefore, the scope of the invention is to be determined by the appended claims Any changes which come within the meaning and range of the claims are intended to be within the scope of the claims.

Claims (10)

  1. 一种涡轮轮罩,用于保护涡轮,其特征在于:所述轮罩包括轮罩主体和支撑所述轮罩主体的支撑部件,所述轮罩主体分割成若干块轮罩分块,且所述每相邻两块轮罩分块之间留有间隙余量。A turbine wheel cover for protecting a turbine, the wheel cover comprising a wheel cover body and a support member supporting the wheel cover body, the wheel cover body being divided into a plurality of wheel cover segments, and There is a gap margin between each adjacent two wheel cover segments.
  2. 如权利要求1所述的涡轮轮罩,其特征在于:所述每个轮罩分块上设有钩爪,所述支撑部件设有与所述钩爪对应的第一槽口,所述每个轮罩分块通过将所述钩爪固定在所述第一槽口上。A turbine wheel cover according to claim 1, wherein each of said wheel cover segments is provided with a claw, and said support member is provided with a first notch corresponding to said claw, said each The wheel cover segments are secured to the first slot by securing the hooks.
  3. 如权利要求2所述的涡轮轮罩,其特征在于:所述涡轮轮罩还包括定位销;所述钩爪上设有第二槽口;所述支撑部件通过所述定位销穿卡合在所述第二槽口内将所述轮罩分块固定在所示支撑部件上。A turbine wheel cover according to claim 2, wherein said turbine wheel cover further comprises a positioning pin; said hook is provided with a second notch; said support member being engaged by said positioning pin The wheel cover is segmented and fixed to the support member shown in the second slot.
  4. 如权利要求1所述的涡轮轮罩,其特征在于:所述每相邻两个轮罩分块之间采用锁片进行限位构成所述轮罩主体,所述锁片用以限制所述轮罩分块在径向上串动。The turbine wheel cover of claim 1 wherein said each of said two adjacent wheel cover segments is restrained by a locking tab to form said wheel cover body, said locking tab for limiting said The wheel cover segments are strung in the radial direction.
  5. 如权利要求4所述的涡轮轮罩,其特征在于:所述轮罩分块沿周向上的两端都设有用于安装所述锁片的缺口,所述每相邻两个轮罩分块之间共用一所述锁片,以保证所述轮罩主体的密封作用。A turbine wheel cover according to claim 4, wherein both ends of the wheel cover block are provided with notches for mounting the locking piece at both ends in the circumferential direction, and each adjacent two wheel cover blocks are divided. A locking piece is shared between them to ensure the sealing effect of the wheel cover body.
  6. 如权利要求5所述的涡轮轮罩,其特征在于:所述锁片包括插设与所述缺口的第一部分和自第一部分垂直延伸的第二部分。The turbine wheel cover of claim 5 wherein said locking tab includes a first portion interposed with said indentation and a second portion extending perpendicularly from said first portion.
  7. 如权利要求1所述的涡轮轮罩,其特征在于:所述轮罩主体分割成八块所述轮罩分块,所述八块轮罩分块均相同。The turbine wheel cover of claim 1 wherein said wheel cover body is divided into eight said wheel cover segments, said eight wheel cover segments being identical.
  8. 如权利要求1所述的涡轮轮罩,其特征在于:所述每相邻两轮罩分块之间留有的间隙余量相当。The turbine wheel cover of claim 1 wherein said gap between said adjacent two wheel cover segments is equivalent.
  9. 如权利要求1所述的涡轮轮罩,其特征在于:所述每相邻两块轮罩分块支架留有的间隙余量总和为所述涡轮轮罩在工作温度下径向膨胀的上限值。A turbine wheel cover according to claim 1 wherein said sum of clearance margins remaining in each of said two adjacent wheel cover segmented brackets is an upper limit of said radial expansion of said turbine wheel cover at operating temperature value.
  10. 如权利要求9所述的涡轮轮罩,其特征在于:所述每相邻两块轮罩分块之间留有间隙余量的总和为3.5mm。The turbine wheel cover of claim 9 wherein said sum of gap allowance between each adjacent two wheel cover segments is 3.5 mm.
PCT/CN2017/114359 2017-12-04 2017-12-04 Turbine housing WO2019109197A1 (en)

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Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN1948718A (en) * 2005-10-14 2007-04-18 通用电气公司 Turbine shroud assembly and method for assembling a gas turbine engine
EP2851518A1 (en) * 2013-09-23 2015-03-25 MTU Aero Engines GmbH Component system of a turbo engine
CN105189934A (en) * 2013-03-14 2015-12-23 通用电气公司 Turbine shroud with spline seal
EP2993313A1 (en) * 2014-09-05 2016-03-09 United Technologies Corporation Offtakes for gas turbine engine secondary gas flows
EP3070278A2 (en) * 2015-03-18 2016-09-21 MTU Aero Engines GmbH Protection device for a turbo engine
CN107740711A (en) * 2017-12-04 2018-02-27 贵州智慧能源科技有限公司 Turbine wheel cover
CN207513639U (en) * 2017-12-04 2018-06-19 贵州智慧能源科技有限公司 Turbine wheel cover

Patent Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN1948718A (en) * 2005-10-14 2007-04-18 通用电气公司 Turbine shroud assembly and method for assembling a gas turbine engine
CN105189934A (en) * 2013-03-14 2015-12-23 通用电气公司 Turbine shroud with spline seal
EP2851518A1 (en) * 2013-09-23 2015-03-25 MTU Aero Engines GmbH Component system of a turbo engine
EP2993313A1 (en) * 2014-09-05 2016-03-09 United Technologies Corporation Offtakes for gas turbine engine secondary gas flows
EP3070278A2 (en) * 2015-03-18 2016-09-21 MTU Aero Engines GmbH Protection device for a turbo engine
CN107740711A (en) * 2017-12-04 2018-02-27 贵州智慧能源科技有限公司 Turbine wheel cover
CN207513639U (en) * 2017-12-04 2018-06-19 贵州智慧能源科技有限公司 Turbine wheel cover

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