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CN112539419B - Heat shield - Google Patents

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Publication number
CN112539419B
CN112539419B CN202011503408.2A CN202011503408A CN112539419B CN 112539419 B CN112539419 B CN 112539419B CN 202011503408 A CN202011503408 A CN 202011503408A CN 112539419 B CN112539419 B CN 112539419B
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CN
China
Prior art keywords
shielding
heat shield
groove
main
piece
Prior art date
Legal status (The legal status 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 status listed.)
Active
Application number
CN202011503408.2A
Other languages
Chinese (zh)
Other versions
CN112539419A (en
Inventor
张山子
沈逸文
何磊
崔耀欣
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Shanghai Electric Gas Turbine Co ltd
Original Assignee
Shanghai Electric Gas Turbine Co ltd
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.)
Filing date
Publication date
Application filed by Shanghai Electric Gas Turbine Co ltd filed Critical Shanghai Electric Gas Turbine Co ltd
Priority to CN202011503408.2A priority Critical patent/CN112539419B/en
Publication of CN112539419A publication Critical patent/CN112539419A/en
Application granted granted Critical
Publication of CN112539419B publication Critical patent/CN112539419B/en
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Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23RGENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/002Wall structures
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23RGENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/42Continuous combustion chambers using liquid or gaseous fuel characterised by the arrangement or form of the flame tubes or combustion chambers
    • F23R3/60Support structures; Attaching or mounting means
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23RGENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R2900/00Special features of, or arrangements for continuous combustion chambers; Combustion processes therefor
    • F23R2900/00012Details of sealing devices
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23RGENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R2900/00Special features of, or arrangements for continuous combustion chambers; Combustion processes therefor
    • F23R2900/03043Convection cooled combustion chamber walls with means for guiding the cooling air flow

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  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)

Abstract

The invention provides a heat shield which comprises a supporting piece (1), a plurality of main shielding pieces (2) and a plurality of auxiliary shielding pieces (3), wherein all the main shielding pieces (2) are fixedly connected with the supporting piece (1) through fixing pieces (14), one sides of all the main shielding pieces (2) facing the combustion chamber of the gas turbine are sequentially connected to form shielding parts, an open slot is formed in one side, facing the supporting piece (1), of each adjacent main shielding piece (2), an auxiliary shielding piece (3) is arranged in the open slot, one end of each fixing piece (14) is fixed in the open slot, and the other end of each fixing piece (14) is fixed on the supporting piece (1). The heat shield is used for solving the problem that a heat shield of a combustion chamber of a gas turbine cannot effectively insulate heat in the prior art.

Description

Heat shield
Technical Field
The present invention relates to heat shields for gas turbines, and more particularly to a heat shield for a gas turbine combustor.
Background
The combustion process in a gas turbine takes place in the combustion chamber housing, which, because of its operation in a high temperature environment, requires the addition of refractory materials inside the housing for insulation. The refractory insulating layer (hereinafter referred to as a heat shield) is typically formed of a plurality of sheet-like tiles circumferentially arranged about the axis of the rotor, completely covering the inner surface of the housing. The heat shield is secured to the housing by a metal support member that contacts the sides of the heat shield. In the actual use process, in order to ensure thermal expansion, gaps exist between adjacent heat shields, so that hot gas can invade to directly reach the end parts of the supporting members, and the local areas of the supporting members are ablated in an over-temperature manner, so that the supporting members are disabled. Particularly, the supporting members are positioned at the middle and lower parts of the gaps between the heat shields, and high-temperature fuel gas enters the gaps and then directly contacts with the end parts of the supporting members, so that the end parts of the supporting members are exposed to high temperature conditions, are extremely easy to oxidize and can have fracture failure. In addition, the existence of the gap also enables the end part of the supporting member to receive heat radiation of high-temperature fuel gas, and the phenomena of thermal viscosity creep and relaxation of the supporting member material can be caused after long-time action, so that the fixing state can be invalid.
Patent publication CN1818527a proposes a heat shield on a support structure, the fixture in which is designed with a cooling system, the clamp section of which can be supplied with cooling fluid directly. However, this structure still does not avoid contact of the clamping section of the fastener with the high-temperature fuel gas and heat radiation exchange.
Patent publication CN103518100a proposes a heat shield with a heat shield that is provided with a beveled shoulder leading edge and a concave trailing edge on each side of the adjoining side wall that can overlap. But this structure is not effective in preventing intrusion of high temperature fuel gas in the case where the heat shield gap is increased.
Therefore, a new structure is required to solve the above-mentioned problems.
Disclosure of Invention
In view of the above-mentioned drawbacks of the prior art, an object of the present invention is to provide a heat shield for solving the problem that the heat shield of the combustion chamber of a gas turbine cannot effectively insulate heat in the prior art.
In order to achieve the above and other related objects, the present invention provides a heat shield comprising a support, a plurality of main shields and a plurality of auxiliary shields, wherein all the main shields are fixedly connected with the support through fixing members, all the main shields are sequentially connected to form a shielding part on one side of the main shields facing a combustion chamber of a gas turbine, an open slot is arranged between adjacent main shields on one side facing the support, the auxiliary shields are arranged in the open slot, one end of each fixing member is fixed in the open slot, and the other end of each fixing member is fixed on the support.
Preferably, the support has cooling channels provided therethrough, the secondary shield has cooling holes provided therein, the cooling channels communicate with all of the cooling holes, and the hole ends of the cooling holes face the primary shield.
Preferably, a sealing structure is arranged between the auxiliary shielding piece and the shielding part, and a through hole corresponding to the cooling hole is arranged on the sealing structure.
The sealing structure and the auxiliary shielding piece are of an integrated structure, and the sealing surface of the sealing structure is in a wave-breaking shape.
The sealing structure and the auxiliary shielding piece are of an embedded structure.
Preferably, the opening groove is further provided with a limiting clamping groove limiting one end part of the fixing piece.
Preferably, the supporting piece is provided with a positioning groove for limiting the other end part of the fixing piece.
Preferably, the main shielding member is rectangular, each of four corners of the rectangle is provided with a groove, and two corresponding grooves on two adjacent main shielding members are connected to form the open slot.
Preferably, the secondary shield is a superalloy or a refractory material.
As described above, the heat shield of the invention has the following beneficial effects:
The auxiliary shielding piece is arranged between the adjacent main shielding pieces, the auxiliary shielding piece can seal the gap between the two adjacent main shielding pieces, hot gas in the gas chamber is prevented from leaking from the gap, meanwhile, the problem that the fixing piece is opposite to the gap to cause the hot gas to leak is avoided, and the gap between the two main shielding pieces is also shortened due to the fact that the fixing piece is opposite to the gap to cause the hot gas to leak.
Drawings
Fig. 1 is a schematic view showing a mounting structure of a heat shield in the present embodiment.
Fig. 2 is a schematic view of a portion of a heat shield of fig. 1.
Fig. 3 is a schematic view showing a first sectional structure along the line A-A in fig. 1.
Fig. 4 is a schematic view showing a second sectional structure along the line A-A in fig. 1.
Description of element reference numerals
1. Support member
2. Main shield
3. Auxiliary shielding piece
4. Positioning groove
5. Cooling channel
6. Cold air side
7. Hot gas side
8. Sealing structure
9A through hole
9B hollow part
10. Second protrusion
11. Gap of
12. Groove
13. First protrusion
14. Fixing piece
15. Locking end
Detailed Description
Further advantages and effects of the present invention will become apparent to those skilled in the art from the disclosure of the present invention, which is described by the following specific examples.
As shown in fig. 1 to 4, the invention provides a heat shield, which comprises a supporting member 1, a plurality of main shielding members 2 and a plurality of auxiliary shielding members 3, wherein all the main shielding members 2 are fixedly connected with the supporting member 1 through fixing members 14, one sides of all the main shielding members 2 facing to a combustion chamber of a gas turbine are sequentially connected to form a shielding part, an open slot is formed between the adjacent main shielding members 2 at one side facing to the supporting member 1, the auxiliary shielding members 3 are arranged in the open slot, one end of the fixing members 14 are fixed in the open slot, and the other end of the fixing members 14 are fixed on the supporting member 1.
The auxiliary shielding pieces 3 are arranged between the adjacent main shielding pieces 2, the auxiliary shielding pieces 3 can seal gaps between the two adjacent main shielding pieces 2, hot gas in the gas chamber is prevented from leaking from the gaps, meanwhile, the problem that the fixing pieces 14 are dead against the gaps to cause hot gas leakage is avoided, the problem that the gaps between the two main shielding pieces 2 fail under the action of high-temperature air flow is also shortened, and the leakage of the hot gas is further reduced.
Specifically, in the present embodiment, the primary shielding member 2 and the secondary shielding member 3 are arranged in a positional relationship shown in fig. 1, one secondary shielding member 3 is arranged between each two primary shielding members 2, the shielding members are arranged on the supporting member 1 in a positional relationship shown in fig. 2, the shielding members are arranged on the side of the supporting member 1 having the positioning grooves 4, and the shielding portions are formed on the side of the supporting member. Specifically, as shown in fig. 2, in this embodiment, the main shielding member 2 is rectangular, four corners of the rectangle are respectively provided with a groove 12, in order to facilitate connection and fixation, the structure surrounding the groove 12 is two protrusions, namely a first protrusion 13 and a second protrusion 10, the second protrusion 10 protrudes from the first protrusion 13, a groove 12 is formed between the first protrusion 13 and the second protrusion 10, the first protrusion 13 is used for connecting the main shielding member 2 and the supporting member 1, the second protrusion 10 is used for heat insulation, two corresponding grooves 12 on two adjacent main shielding members 2 are connected to form an open slot, the auxiliary shielding member 3 is arranged in the open slot, a gap between two adjacent main shielding members 2 is sealed and shielded, so as to prevent the leakage of hot gas in the gas chamber, and meanwhile, if the auxiliary shielding member 3 is dislocated with the main shielding member 2 in the gas flow direction, the main shielding member 2 can be limited to move in the axial direction, and in order to ensure that the auxiliary shielding member 3 works normally, so as to realize the effect of shielding the hot gas and the auxiliary shielding member 3 is a refractory material.
Further, in order to facilitate the air on the cold air side 6 to enter the interior of the heat shield structure for cooling, the support member 1 is provided with a cooling channel 5 penetrating the support member 1, the auxiliary shield member 3 is provided with cooling holes, the cooling channel 5 is communicated with all the cooling holes, and the hole ends of the cooling holes face the main shield member 2.
The air of the cold air side 6 enters through the cooling channel 5 on the supporting piece 1 and then enters the positioning hole, the end part of the fixing piece 14 positioned in the positioning hole is cooled, the end part of the positioning piece is prevented from being heated and losing the function of fixing and locking, so that leakage of hot fuel gas and heat radiation is caused, meanwhile, the air also enters into the open slot through the cooling hole, the other end part of the fixing piece 14 fixed in the open slot is cooled, and the end part of the fixing piece 14 is prevented from being heated and losing the function of fixing and locking, so that leakage of the hot fuel gas and the heat radiation is caused.
In order to further prevent leakage of hot gas and heat radiation in the combustion chamber, a sealing structure 8 is arranged between the auxiliary shielding piece 3 and the shielding part, a through hole corresponding to the cooling hole is arranged on the sealing structure 8, the through hole can ensure circulation of cold air and play a role of indirect sealing, meanwhile, the sealing structure 8 can prevent the hot gas on the hot gas side 7 from leaking into the open slot and avoid heat failure of a fixing piece 14 fixed in the open slot, and meanwhile, in order to increase sealing performance, a sealing structure 8 is arranged on a contact surface of the auxiliary shielding piece 3 and the second protrusion 10, wherein the sealing structure 8 and the auxiliary shielding piece 3 can be in an integrated structure, and the sealing surface of the sealing structure 8 is in a wavy shape.
In order to facilitate installation and positioning, the opening groove is also provided with a limiting clamping groove at one end of the limiting fixing piece 14, the supporting piece 1 is provided with a positioning groove 4 at the other end of the limiting fixing piece 14, the limiting clamping groove and the positioning groove 4 are respectively fixed at two ends of the main fixing piece 14 to realize the fixing and locking functions of the fixing piece 14, and meanwhile, the fixing groove can also be used as a circulation channel of cool air to cool the fixing piece 14 fixed in the fixing groove.
The auxiliary shielding member 3 may be in a structure shown in fig. 3, the auxiliary shielding member 3 is provided with a plurality of through holes 9a (i.e. the above cooling holes), one end of the auxiliary shielding member 3, which is in contact with the second protrusion 10, is provided with a sealing structure 8, the sealing structure 8 is provided with a through hole corresponding to the through holes 9a, and the through hole is communicated with the mounting groove 4 and the groove 12, so that air on the cold air side 6 enters from the cooling channel 5, and then enters into the groove 12 through the through hole, thereby realizing cooling of the most end part of the locking end 15, and avoiding fixing failure caused by thermal deformation of the locking end 15.
The secondary shielding member 3 may have a structure as shown in fig. 4, the secondary shielding member has a hollow portion 9b communicating with the outside, one end of the secondary shielding member 3 contacting with the second protrusion 10 on the primary shielding member 2 has a sealing structure 8, the sealing surface of the sealing structure 8 is in a wave shape, the sealing structure 8 has a plurality of communication holes (i.e. the above cooling holes), and the plurality of communication holes (i.e. the above cooling holes) are communicated with the hollow portion 9b, the air on the cold air side 6 enters from the cooling channel 5, enters into the hollow portion 9b through the communication holes, finally enters into the groove 12 and the gap between the two primary shielding members 2, thereby realizing cooling of the locking end 15 and preventing heat radiation leakage inside the heat shield.
The whole structure of the invention can realize triple protection, namely, the cooling air directly led to the gap 11 between the main shielding pieces 2 is first re-protected to prevent hot gas invasion, the sealing piece on the auxiliary shielding piece 3 is second re-protected, even if hot gas invades through the gap 11, the cooling air led to the end part of the fixing piece 14 is third re-protected to ensure that the temperature of the end part of the fixing piece 14 meets the requirement.
In summary, the heat shield of the invention can effectively reduce the harmful effects of heat gas leakage and heat radiation caused by the heat shield gap 11, can greatly avoid the contact between the end of the fixing piece 14 and the heat gas, ensures the normal temperature of the end of the fixing piece 14, and reduces the failure risk.
Therefore, the invention effectively overcomes various defects in the prior art and has high industrial utilization value.
The above embodiments are merely illustrative of the principles of the present invention and its effectiveness, and are not intended to limit the invention. Modifications and variations may be made to the above-described embodiments by those skilled in the art without departing from the spirit and scope of the invention. Accordingly, it is intended that all equivalent modifications and variations of the invention be covered by the claims, which are within the ordinary skill of the art, be within the spirit and scope of the present disclosure.

Claims (6)

1.一种用于燃气轮机燃烧室的热屏,其特征在于,包括:支承件(1)、多个主屏蔽件(2)和多个副屏蔽件(3),所有所述主屏蔽件(2)均通过固定件(14)与所述支承件(1)固定相连,所有所述主屏蔽件(2)朝向燃气轮机燃烧室的一侧依次衔接形成屏蔽部,相邻所述主屏蔽件(2)间在朝向支承件(1)的一侧设有开口槽,所述开口槽中设有所述副屏蔽件(3),且固定件(14)的一端固定在所述开口槽中,固定件(14)的另一端固定在所述支承件(1)上;所述支承件(1)上具有贯穿所述支承件(1)设置的冷却通道(5),所述副屏蔽件(3)上设有冷却孔,所述冷却通道(5)与所有所述冷却孔连通,且所述冷却孔的孔端朝向主屏蔽件(2);所述副屏蔽件(3)与所述屏蔽部间设有密封结构(8),所述密封结构(8)上设置有与所述冷却孔对应的通孔;所述主屏蔽件(2)为矩形,在矩形的四个角处均设有一个凹槽(12),相邻两个所述主屏蔽件(2)上,对应的两个所述凹槽(12)衔接形成所述开口槽。1. A heat shield for a gas turbine combustion chamber, characterized in that it comprises: a support member (1), a plurality of main shielding members (2) and a plurality of secondary shielding members (3), wherein all the main shielding members (2) are fixedly connected to the support member (1) via a fixing member (14), and all the main shielding members (2) are connected in sequence on a side facing the gas turbine combustion chamber to form a shielding portion, and an open groove is provided between adjacent main shielding members (2) on a side facing the support member (1), and the secondary shielding member (3) is provided in the open groove, and one end of the fixing member (14) is fixed in the open groove, and the other end of the fixing member (14) is fixed to the support member (1). ); the support member (1) is provided with a cooling channel (5) penetrating the support member (1); the secondary shielding member (3) is provided with cooling holes, the cooling channel (5) is connected with all the cooling holes, and the hole ends of the cooling holes face the main shielding member (2); a sealing structure (8) is provided between the secondary shielding member (3) and the shielding portion, and the sealing structure (8) is provided with through holes corresponding to the cooling holes; the main shielding member (2) is rectangular, and a groove (12) is provided at each of the four corners of the rectangle, and the corresponding two grooves (12) on two adjacent main shielding members (2) are connected to form the open groove. 2.根据权利要求1所述的热屏,其特征在于:所述密封结构(8)与所述副屏蔽件(3)为一体式结构,所述密封结构(8)的密封面呈波浪状。2. The heat shield according to claim 1, characterized in that the sealing structure (8) and the auxiliary shielding component (3) are an integrated structure, and the sealing surface of the sealing structure (8) is wavy. 3.根据权利要求1所述的热屏,其特征在于:所述密封结构(8)与所述副屏蔽件(3)为镶嵌式结构。3. The heat shield according to claim 1, characterized in that the sealing structure (8) and the auxiliary shielding component (3) are inlaid structures. 4.根据权利要求1所述的热屏,其特征在于:所述开口槽内还具有限位所述固定件(14)的一端端部的限位卡槽。4. The heat shield according to claim 1, characterized in that: the opening groove also has a limiting groove for limiting one end of the fixing member (14). 5.根据权利要求3所述的热屏,其特征在于:所述支承件(1)上设有限位所述固定件(14)的另一端端部的定位槽(4)。5. The heat shield according to claim 3, characterized in that: the support member (1) is provided with a positioning groove (4) for limiting the other end of the fixing member (14). 6.根据权利要求1所述的热屏,其特征在于:所述副屏蔽件(3)为耐高温合金或者耐火材料。6. The heat shield according to claim 1, characterized in that the secondary shielding component (3) is made of a high temperature resistant alloy or a refractory material.
CN202011503408.2A 2020-12-18 2020-12-18 Heat shield Active CN112539419B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN202011503408.2A CN112539419B (en) 2020-12-18 2020-12-18 Heat shield

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN202011503408.2A CN112539419B (en) 2020-12-18 2020-12-18 Heat shield

Publications (2)

Publication Number Publication Date
CN112539419A CN112539419A (en) 2021-03-23
CN112539419B true CN112539419B (en) 2024-12-17

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Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN214064984U (en) * 2020-12-18 2021-08-27 上海电气燃气轮机有限公司 Heat shield for gas turbine combustion chamber

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP1284390A1 (en) * 2001-06-27 2003-02-19 Siemens Aktiengesellschaft Thermal shield for a component carrying hot gases, especially for structural components of gas turbines
EP2522907A1 (en) * 2011-05-12 2012-11-14 Siemens Aktiengesellschaft Heat shield assembly
CN108884743B (en) * 2016-03-24 2021-03-12 佛吉亚排放控制技术美国有限公司 Thermal shield for vehicle exhaust system
US10378772B2 (en) * 2017-01-19 2019-08-13 General Electric Company Combustor heat shield sealing

Patent Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN214064984U (en) * 2020-12-18 2021-08-27 上海电气燃气轮机有限公司 Heat shield for gas turbine combustion chamber

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