Oil supply component and gas turbine engine having the same

Abstract

The present invention belongs to the technical field of engines, and specifically discloses an oil supply part and a gas turbine engine having the same. By connecting the two ends of a first connecting channel with a cleaning medium inlet and a cleaning medium outlet respectively, the gas entering from the cleaning medium inlet can flow to the cleaning medium outlet through the first connecting channel and flow out from the cleaning medium outlet; the cleaning medium outlet is arranged on the outer wall of the annular wall, the cleaning medium outlet is arranged between any two adjacent grate teeth, and the cleaning medium outlet is arranged on the outer side of the grate tooth structure, so that the gas flowing out of the cleaning medium outlet can disperse the fuel accumulated between and near the grate teeth, reduce the risk of fuel coking between or outside the grate teeth after sealing, reduce the failure rate of the rotor stuck on the stator, and reduce the cost incurred when returning to the factory for maintenance due to engine failure, that is, extend the service life of the engine and the overhaul interval, thereby improving the reliability of the engine.

Description

Technical Field

[0001] The present invention relates to the technical field of engines, and in particular to an oil supply component and a gas turbine engine having the same. Background Art

[0002] A gas turbine engine is a device that converts the chemical energy of fuel into mechanical work. The fuel is supplied to the fuel atomizer through the fuel supply component, and the fuel atomizer atomizes the fuel and supplies the oil mist to the combustion chamber for combustion, generating high-temperature combustion gas to drive the turbine to output mechanical work.

[0003] The fuel atomization component of the existing combustion chamber is an oil-slinging plate connected to the main shaft of the engine, and the oil supply component that supplies oil to the oil-slinging plate is generally fixedly installed on the back of the diffuser. In this case, the oil supply component is the stator component, and the oil-slinging plate is the rotor component. There will be a sealing gap between the two after installation, and the gap needs to be sealed to avoid oil and gas crossflow. Since the grate seal can be applied to high-speed rotating equipment, the grate seal is widely used in gas turbine engines. That is, during implementation, the gas turbine engine uses a grate seal structure to seal the gap between the rotor and the stator. At this time, the grate seal structure gap between the rotor and the stator is about (0.3-0.8) mm.

[0004] However, during the engine starting phase, due to the low speed of the oil slinger, the fuel atomization effect is not ideal, and there is a part of un-atomized liquid fuel. This part of the fuel will flow into the grate seal structure between the oil slinger and the oil supply part as it rotates, and even further overflow. The main manifestation is that some fuel accumulates between the grate teeth on the stator and around the grate teeth. If this part of the fuel is not removed in time, when the ambient temperature reaches a certain value, this part of the fuel will have the risk of coking. Coking will cause the grate seal gap to be blocked by coking materials, which will greatly increase the rotation resistance. In severe cases, it will cause the rotor to stagnate, and then the engine cannot be started, resulting in insufficient practicality of the oil supply part. Summary of the invention

[0005] Therefore, the technical problem to be solved by the present invention is that in the prior art, during the engine startup phase, unatomized fuel will enter the spaces between the grate teeth on the stator and be accumulated around the grate teeth. When the temperature reaches a certain value, this part of the fuel will have the risk of coking, resulting in insufficient practicality of the fuel supply component.

[0006] To this end, the present invention provides an oil supply component, comprising:

[0007] a first body having an annular wall;

[0008] A comb tooth structure, the comb tooth structure comprising a plurality of comb teeth, the plurality of comb teeth being arranged on the outer wall of the annular wall, and the plurality of comb teeth being arranged at intervals along the axial direction of the annular wall;

[0009] A gas transmission structure, the gas transmission structure includes a cleaning medium inlet, a cleaning medium outlet and a first connecting channel, the cleaning medium inlet is arranged on the outer wall of the annular wall, and the cleaning medium inlet and the comb tooth structure are arranged axially with each other along the annular wall, the cleaning medium outlet is arranged on the outer wall of the annular wall, the cleaning medium outlet and the cleaning medium inlet are arranged axially with each other along the annular wall, the cleaning medium outlet is arranged between any two adjacent comb teeth, and the cleaning medium outlet is arranged on the outside of the comb tooth structure, the first connecting channel is arranged inside the annular wall, and both ends of the first connecting channel are respectively connected to the cleaning medium inlet and the cleaning medium outlet.

[0010] Optionally, the above-mentioned oil supply part,

[0011] The first connecting passage includes a first connecting section and a second connecting section, the first connecting section extends along the circumferential direction of the annular wall, the second connecting section extends along the axial direction of the annular wall, the cleaning medium inlet is connected to the first connecting section, and both ends of the second connecting section are respectively connected to the first connecting section and the cleaning medium outlet.

[0012] Optionally, the above-mentioned oil supply part,

[0013] There are multiple cleaning medium outlets, and the multiple cleaning medium outlets are arranged at intervals along the axial direction of the annular wall. The multiple cleaning medium outlets are all connected to the second connecting section.

[0014] Optionally, the above-mentioned oil supply part,

[0015] There are a plurality of second communication sections, and the plurality of second communication sections are arranged at intervals along the circumference of the annular wall;

[0016] The cleaning medium outlets are provided in a plurality of groups, and the plurality of groups of cleaning medium outlets are arranged at intervals along the circumference of the annular wall, and any group is provided with a plurality of cleaning medium outlets correspondingly connected to any of the second connecting sections.

[0017] Optionally, the above-mentioned oil supply part,

[0018] The first communication section passes through the end of the annular wall and forms a first opening;

[0019] The oil supply member further comprises a first cover body, and the first cover body is arranged on the end of the annular wall to close the first opening.

[0020] Optionally, the above-mentioned oil supply part,

[0021] A gas injection convex portion is provided on the outer wall of the annular wall;

[0022] The cleaning medium inlet is formed on the gas injection convex portion;

[0023] The first communication channel further includes a third communication section, which is disposed inside the gas injection convex portion, and two ends of the third communication section are respectively communicated with the cleaning medium inlet and the first communication section.

[0024] Optionally, the above-mentioned oil supply component further includes:

[0025] A liquid transmission structure, the liquid transmission structure includes a fuel inlet, a second connecting channel and a fuel outlet, the fuel inlet and the cleaning medium inlet are arranged at radial intervals along the annular wall, and the fuel inlet and the comb tooth structure are arranged at axial intervals along the annular wall, the second connecting channel is arranged inside the annular wall, the fuel outlet is opened inside the second connecting channel, and the fuel outlet is connected to the fuel inlet through the second connecting channel.

[0026] Optionally, the above-mentioned oil supply part,

[0027] The second communication passage comprises a fourth communication section, a fifth communication section and a sixth communication section which are connected to each other, the fourth communication section extends along the circumferential direction of the annular wall, the fifth communication section extends along the axial direction of the annular wall, and the sixth communication section extends along the radial direction of the annular wall;

[0028] The fuel inlet is communicated with the sixth communicating section.

[0029] Optionally, the above-mentioned oil supply part,

[0030] A liquid injection convex portion is provided on the outer wall of the annular wall, and the liquid injection convex portion and the gas injection convex portion are arranged at intervals along the radial direction of the annular wall;

[0031] The fuel inlet is formed in the injection convex portion.

[0032] Optionally, the above-mentioned oil supply part,

[0033] The fourth connecting section passes through the other end of the annular wall and forms a second opening;

[0034] The oil supply member further comprises a second cover body, and the second cover body is arranged to cover the second opening.

[0035] A gas turbine engine comprising:

[0036] The oil supply part is the above-mentioned oil supply part;

[0037] An oil-slinging plate, the oil-slinging plate comprising a second body and an annular groove formed on the second body, the annular groove being used to accommodate the annular wall;

[0038] An air inlet pipe, one end of which is connected to a discharge port of a first storage element storing a cleaning medium, and the other end of which is connected to a cleaning medium inlet;

[0039] An oil inlet pipe, one end of which is connected to the discharge port of the second storage element storing the fuel, and the other end of which is connected to the fuel inlet;

[0040] The flame tube is movably sleeved on the outer wall of the annular groove.

[0041] The technical solution provided by the present invention has the following advantages:

[0042] The oil supply part provided by the present invention includes a first body, a grate structure and a gas transmission structure. The first body has an annular wall; the grate structure includes a plurality of grate teeth, the plurality of grate teeth are arranged on the outer wall of the annular wall, and the plurality of grate teeth are arranged at intervals along the axial direction of the annular wall; the gas transmission structure includes a cleaning medium inlet, a plurality of cleaning medium outlets and a first connecting channel, the cleaning medium inlet is arranged on the outer wall of the annular wall, and the cleaning medium inlet and the grate structure are arranged at intervals along the axial direction of the annular wall, the cleaning medium outlet is arranged on the outer wall of the annular wall, the cleaning medium outlet and the cleaning medium inlet are arranged at intervals along the axial direction of the annular wall, the cleaning medium outlet is arranged between any two adjacent grate teeth, and the cleaning medium outlet is arranged on the outside of the grate structure, the first connecting channel is arranged inside the annular wall, and the two ends of the first connecting channel are respectively connected to the cleaning medium inlet and the cleaning medium outlet.

[0043] The oil supply component of this structure is connected with the cleaning medium inlet and the cleaning medium outlet respectively by using the two ends of the first connecting channel, so that the gas entering from the cleaning medium inlet can flow to the cleaning medium outlet through the first connecting channel and finally flow out from the cleaning medium outlet; the cleaning medium outlet is arranged on the outer wall of the annular wall, and the cleaning medium outlet is arranged between any two adjacent grate teeth, and the cleaning medium outlet is arranged on the outside of the grate tooth structure, so that the gas flowing out from the cleaning medium outlet can disperse the fuel accumulated between and near the grate teeth, reduce the risk of fuel coking between or outside the grate teeth after sealing, reduce the failure rate of the rotor getting stuck on the stator, improve the practicality of the oil supply component, and reduce the cost incurred when returning to the factory for maintenance due to engine failure, that is, extend the engine service life and overhaul interval time, thereby improving the reliability of the engine. BRIEF DESCRIPTION OF THE DRAWINGS

[0044] In order to more clearly illustrate the specific implementation methods of the present invention or the technical solutions in the prior art, the drawings required for use in the specific implementation methods or the description of the prior art will be briefly introduced below. Obviously, the drawings described below are some implementation methods of the present invention. For ordinary technicians in this field, other drawings can be obtained based on these drawings without paying creative work.

[0045] Figure 1 A cross-sectional view of a gas turbine engine provided for an embodiment of the present invention;

[0046] Figure 2 A schematic diagram of the structure of an oil supply component in a gas turbine engine provided by an embodiment of the present invention;

[0047] Figure 3 for Figure 2 Sectional view of section AA;

[0048] Figure 4 for Figure 3 Cross-sectional view of the middle BB section;

[0049] Figure 5 for Figure 3 Schematic diagram of the structure in the K direction;

[0050] Figure 6 for Figure 5 Sectional view of the CC section;

[0051] Figure 7 An axonometric view of an oil supply component in a gas turbine engine provided for an embodiment of the present invention;

[0052] Figure 8 A schematic diagram of the structure of the internal circulation channel of the oil supply member provided in an embodiment of the present invention;

[0053] Fig. 9 An axonometric view of the internal flow channel of the oil supply member provided in an embodiment of the present invention;

[0054] Description of reference numerals:

[0055] 11-first body; 111-annular wall; 12-comb structure; 121-comb; 13-gas transmission structure; 131-cleaning medium inlet; 132-cleaning medium outlet; 133-first communication channel; 1331-first communication section; 1332-second communication section; 1333-third communication section; 1334-first opening; 134-gas injection convex portion; 14-first cover; 15-liquid transmission structure; 151-fuel inlet; 152-second communication channel; 1521-fourth communication section; 1522-fifth communication section; 1523-sixth communication section; 1524-second opening; 153-fuel outlet; 154-liquid injection convex portion; 16-second cover;

[0056] 2- oil-slinging plate; 21- second body; 211- annular groove;

[0057] 3- Intake pipe;

[0058] 4-Oil inlet pipe;

[0059] 5-Flame tube. DETAILED DESCRIPTION

[0060] The technical solution of the present invention will be described clearly and completely below in conjunction with the accompanying drawings. Obviously, the described embodiments are only part of the embodiments of the present invention, not all of the embodiments. Based on the embodiments of the present invention, all other embodiments obtained by ordinary technicians in this field without creative work are within the scope of protection of the present invention.

[0061] In the description of the present invention, it should be noted that the terms "center", "upper", "lower", "left", "right", "vertical", "horizontal", "inner", "outer", etc., indicating the orientation or positional relationship, are based on the orientation or positional relationship shown in the drawings, and are only for the convenience of describing the present invention and simplifying the description, rather than indicating or implying that the device or element referred to must have a specific orientation, be constructed and operated in a specific orientation, and therefore cannot be understood as limiting the present invention. In addition, the terms "first", "second", and "third" are used for descriptive purposes only, and cannot be understood as indicating or implying relative importance.

[0062] In the description of the present invention, it should be noted that, unless otherwise clearly specified and limited, the terms "installed", "connected", and "connected" should be understood in a broad sense, for example, it can be a fixed connection, a detachable connection, or an integral connection; it can be a mechanical connection or an electrical connection; it can be a direct connection, or it can be indirectly connected through an intermediate medium, or it can be the internal communication of two components. For ordinary technicians in this field, the specific meanings of the above terms in the present invention can be understood according to specific circumstances.

[0063] In addition, the technical features involved in the different embodiments of the present invention described below can be combined with each other as long as they do not conflict with each other.

[0064] Example 1

[0065] In this embodiment, an oil supply member is provided, such as Figures 1 to 9 As shown, the gas transmission structure 13 includes a first body 11, a comb structure 12 and a gas transmission structure 13. The first body 11 has an annular wall 111; the comb structure 12 includes a plurality of comb teeth 121, which are arranged on the outer wall of the annular wall 111, and the plurality of comb teeth 121 are arranged at intervals along the axial direction of the annular wall 111; the gas transmission structure 13 includes a cleaning medium inlet 131, a cleaning medium outlet 132 and a first connecting channel 133, the cleaning medium inlet 131 is arranged on the outer wall of the annular wall 111, and the cleaning medium inlet 131 and the comb structure 12 are arranged along the axial direction of the annular wall 111. The cleaning medium outlet 132 is arranged at intervals, and is arranged on the outer wall of the annular wall 111. The cleaning medium outlet 132 and the cleaning medium inlet 131 are arranged at intervals along the axial direction of the annular wall 111. The cleaning medium outlet 132 is arranged between any two adjacent comb teeth 121, and the cleaning medium outlet 132 is arranged on the outside of the comb tooth structure 12. The first connecting channel 133 is arranged inside the annular wall 111, and the two ends of the first connecting channel 133 are respectively connected to the cleaning medium inlet 131 and the cleaning medium outlet 132.

[0066] The oil supply component provided in this embodiment uses the two ends of the first connecting channel 133 to be connected to the cleaning medium inlet 131 and the cleaning medium outlet 132 respectively, so that the gas entering from the cleaning medium inlet 131 can flow to the cleaning medium outlet 132 through the first connecting channel 133, and finally flow out from the cleaning medium outlet 132; the cleaning medium outlet 132 is arranged on the outer wall of the annular wall 111, and the cleaning medium outlet 132 is arranged between any two adjacent comb teeth 121, and the cleaning medium outlet 132 is arranged on the outer side of the comb tooth structure 12, so that the gas flowing out from the cleaning medium outlet 132 can disperse the fuel accumulated between the comb teeth 121 and near the comb teeth 121, reduce the risk of fuel coking between the comb teeth 121 or outside the comb teeth 121 after sealing, reduce the failure rate of the rotor stuck on the stator, improve the practicality of the oil supply component, reduce the cost incurred when returning to the factory for maintenance due to engine failure, that is, extend the engine service life and overhaul interval time, and thus improve the reliability of the engine.

[0067] It can be explained that, if the oil supply component provided in this embodiment needs to be cleaned, the oil supply component is in a shutdown state.

[0068] It can be explained that, in the oil supply member provided in this embodiment, the medium entering from the cleaning medium inlet 131 can be gas such as high-pressure air, or can be liquid such as cleaning agent.

[0069] like Figures 1 to 9 As shown, the oil supply part provided in this embodiment, the first connecting channel 133 includes a first connecting section 1331 and a second connecting section 1332, the first connecting section 1331 extends along the circumference of the annular wall 111, and the second connecting section 1332 extends along the axial direction of the annular wall 111, the cleaning medium inlet 131 is connected to the first connecting section 1331, and the two ends of the second connecting section 1332 are respectively connected to the first connecting section 1331 and the cleaning medium outlet 132.

[0070] The oil supply member provided in this embodiment does not limit the structure of the first connecting section 1331. It can be a non-connecting U-shape or a connecting O-shape.

[0071] The oil supply part provided in this embodiment does not limit the number of cleaning medium outlets 132, and can be in the form of one group of multiple, or in the form of multiple groups of multiple. It is only necessary to provide multiple cleaning medium outlets 132, and the multiple cleaning medium outlets 132 are arranged at axial intervals along the annular wall 111, and the multiple cleaning medium outlets 132 are all connected to the second connecting section 1332.

[0072] As one of the embodiments, the cleaning medium outlet 132 is in the form of multiple groups. Figures 1 to 9 As shown, the oil supply part provided in this embodiment is provided with a plurality of second connecting sections 1332, and the plurality of second connecting sections 1332 are arranged at circumferential intervals along the annular wall 111; a plurality of cleaning medium outlets 132 are provided, and the plurality of groups of cleaning medium outlets 132 are arranged at circumferential intervals along the annular wall 111, and any group is provided with a plurality of cleaning medium outlets 132 corresponding to and connected with any second connecting section 1332.

[0073] like Figures 1 to 9 As shown, the oil supply member provided in this embodiment has a first connecting section 1331 that penetrates the end of the annular wall 111 and forms a first opening 1334 ; the oil supply member also includes a first cover body 14 , which is covered on the end of the annular wall 111 to close the first opening 1334 .

[0074] like Figures 1 to 9 As shown, in the oil supply part provided in this embodiment, an air injection protrusion 134 is provided on the outer wall of the annular wall 111; a cleaning medium inlet 131 is formed on the air injection protrusion 134; the first connecting channel 133 also includes a third connecting section 1333, the third connecting section 1333 is arranged inside the air injection protrusion 134, and the two ends of the third connecting section 1333 are respectively connected to the cleaning medium inlet 131 and the first connecting section 1331.

[0075] like Figures 1 to 9 As shown, the oil supply member provided in this embodiment further includes a liquid transmission structure 15. At this time, the liquid transmission structure 15 includes a fuel inlet 151, a second communication channel 152 and a fuel outlet 153. The fuel inlet 151 and the cleaning medium inlet 131 are arranged at intervals along the radial direction of the annular wall 111, and the fuel inlet 151 and the comb tooth structure 12 are arranged at intervals along the axial direction of the annular wall 111. The second communication channel 152 is arranged inside the annular wall 111, and the fuel outlet 153 is opened inside the second communication channel 152, and the fuel outlet 153 is connected to the fuel inlet 151 through the second communication channel 152.

[0076] like Figures 1 to 9 As shown, the oil supply component provided in this embodiment, the second connecting channel 152 includes a fourth connecting section 1521, a fifth connecting section 1522 and a sixth connecting section 1523 that are connected to each other, the fourth connecting section 1521 extends along the circumferential direction of the annular wall 111, the fifth connecting section 1522 extends along the axial direction of the annular wall 111, and the sixth connecting section 1523 extends along the radial direction of the annular wall 111; the fuel inlet 151 is connected to the sixth connecting section 1523.

[0077] It can be explained that, in the oil supply component provided in this embodiment, the fuel outlet 153 is opened in the fourth connecting section 1521 .

[0078] Furthermore, the fuel supply member provided in this embodiment does not limit the number of the fuel outlets 153 , which may be two or more. In this case, the fuel outlets 153 are evenly distributed in the fourth connecting section 1521 along the circumferential direction of the annular wall 111 .

[0079] The fuel supply member provided in this embodiment does not limit the structure of the fourth connecting section 1521. It can be a non-connected U-shaped or a connected O-shaped. When it is a U-shaped, the uniformity of the fuel sprayed from each fuel outlet 153 can be better, and when it is an O-shaped, the processing cost of the fourth connecting section 1521 can be reduced.

[0080] like Figures 1 to 9 As shown, in the oil supply part provided in this embodiment, a liquid injection protrusion 154 is provided on the outer wall of the annular wall 111 , and the liquid injection protrusion 154 and the gas injection protrusion 134 are arranged at intervals along the radial direction of the annular wall 111 ; the fuel inlet 151 is formed in the liquid injection protrusion 154 .

[0081] like Figures 1 to 9 As shown, in the oil supply member provided in this embodiment, the fourth connecting section 1521 penetrates the other end of the annular wall 111 and forms a second opening 1524 ; the oil supply member further includes a second cover body 16 , which is disposed at the second opening 1524 .

[0082] It can be explained that the oil supply member provided in this embodiment does not limit the structure of the cleaning medium outlet 132. In order to increase the range of high-pressure air or cleaning agent flushing the fuel accumulated between the grate teeth 121 and near the grate teeth 121, the structure of the cleaning medium outlet 132 can be set to a tapered hole, so that the high-pressure air or cleaning agent can be dispersed after flowing out of the cleaning medium outlet 132. In addition, in order to increase the force of high-pressure air or cleaning agent to disperse the fuel accumulated between the grate teeth 121 and near the grate teeth 121, the structure of the cleaning medium outlet 132 can be set to a cylindrical hole.

[0083] It can be explained that, in the fuel supply member provided in this embodiment, the axial direction of the fuel outlet 153 is arranged crosswise or parallel to the axial direction of the cleaning medium outlet 132. As one embodiment, the axial direction of the fuel outlet 153 is arranged parallel to the axial direction of the cleaning medium outlet 132.

[0084] Example 2

[0085] This embodiment provides a gas turbine engine, and the oil supply part provided in the above embodiment. Figures 1 to 9 As shown, the gas turbine engine provided in this embodiment further includes an oil slinger 2, an air intake pipe 3, an oil intake pipe 4 and a flame tube 5. The oil slinger 2 includes a second body 21 and an annular groove 211 provided on the second body 21, and the annular groove 211 is used to accommodate the annular wall 111; one end of the air intake pipe 3 is connected to the discharge port of the first storage member storing the cleaning medium, and the other end of the air intake pipe 3 is connected to the cleaning medium inlet 131; one end of the oil intake pipe 4 is connected to the discharge port of the second storage member storing the fuel, and the other end of the oil intake pipe 4 is connected to the fuel inlet 151; the flame tube 5 is movably sleeved on the outer wall of the annular groove 211.

[0086] It can be explained that, in the gas turbine engine provided in this embodiment, the annular wall 111 and the annular groove 211 are arranged coaxially with the engine rotor.

[0087] It can be explained that, in the gas turbine engine provided in this embodiment, the flame tube 5 is located in the combustion chamber of the gas turbine engine.

[0088] It can be explained that if Figure 1As shown, a certain gap is formed between the comb tooth structure 12 and the annular groove 211, and a third connecting channel for fuel oil to flow is formed at the sleeve joint of the flame tube 5 and the annular groove 211. At this time, the third connecting channel is connected to the inner cavity of the flame tube 5, so that the fuel oil dispersed from the cleaning medium outlet 132 can flow from the gap here to the third connecting channel and flow to the inner cavity of the flame tube 5. That is, the gas turbine engine provided in this embodiment, by accommodating the annular wall 111 in the annular groove 211 of the oil-slinging plate 2, and movably sleeved the flame tube 5 on the outer wall of the annular groove 211, so that the fuel oil flows out of the annular wall 111 and enters the oil-slinging plate 2, and the fuel oil can be thrown into the combustion chamber where the flame tube 5 is located with the rotation of the oil-slinging plate 2, so that the fuel oil collides with the air in the flame tube 5, and then the fuel oil is broken into oil mist, and then burned and released heat in the flame tube 5, so that the fuel oil burns more fully.

[0089] It should be noted that, since there is a certain gap between the grate structure 12 and the annular groove 211, if the fuel oil adheres to this gap, coking will occur, which is intuitively manifested as the gap being blocked. Through the setting of the cleaning medium outlet 132, high-pressure air will be sprayed to this gap, and then the fuel oil in the gap will be flushed, thereby achieving the purpose of cleaning the fuel oil and reducing the risk of coking and stagnation. At the same time, if the medium entering from the cleaning medium inlet 131 is a cleaning agent, after the cleaning agent disperses the fuel oil accumulated between the grate teeth 121 and near the grate teeth 121, this part of the cleaning agent will be like the fuel oil. With the action of its own gravity and the action of the thrust generated by the adjacent cleaning agent, it is intuitively manifested that the cleaning agent will be displaced along the radial and axial directions of the annular wall 111, enter the combustion chamber where the flame tube 5 is located through the third connecting channel, and finally be discharged to the outside of the gas turbine engine through the oil leakage valve set on the casing of the combustion chamber. At the same time, if there is still a small amount of cleaning agent in the gas turbine engine after cleaning, high-pressure air is blown into the cleaning medium inlet 131 for air washing.

[0090] Furthermore, if the gas turbine engine is in working condition, the oil inlet pipe 4 supplies fuel to the fuel inlet 151, the fuel will enter the oil throwing plate 2 through the fuel outlet 153, and enter the inner cavity of the flame tube 5 through the third connecting channel for combustion. During this process, the air intake pipe 3 stops supplying cleaning agent or high-pressure air to the cleaning medium inlet 131; if the gas turbine engine is in a shutdown state, the oil inlet pipe 4 stops supplying fuel to the fuel inlet 151, the air intake pipe 3 is opened, and high-pressure air or cleaning agent is supplied to the cleaning medium inlet 131. After the cleaning is completed, the air intake pipe 3 stops supplying cleaning agent or high-pressure air to the cleaning medium inlet 131.

[0091] Obviously, the above embodiments are merely examples for the purpose of clear explanation, and are not intended to limit the implementation methods. For those skilled in the art, other different forms of changes or modifications can be made based on the above description. It is not necessary and impossible to list all the implementation methods here. The obvious changes or modifications derived therefrom are still within the scope of protection of the invention.

Claims

1. An oil supply component, characterized in that: include: A first body (11), the first body (11) having an annular wall (111); A comb tooth structure (12), the comb tooth structure (12) comprising a plurality of comb teeth (121), the plurality of comb teeth (121) being arranged on the outer wall of the annular wall (111), and the plurality of comb teeth (121) being arranged at intervals along the axial direction of the annular wall (111); A gas transmission structure (13), the gas transmission structure (13) comprising a cleaning medium inlet (131), a cleaning medium outlet (132) and a first connecting channel (133), the cleaning medium inlet (131) being arranged on the outer wall of the annular wall (111), and the cleaning medium inlet (131) and the comb tooth structure (12) being arranged at intervals along the axial direction of the annular wall (111), the cleaning medium outlet (132) being arranged on the outer wall of the annular wall (111), and the cleaning medium outlet (132) being arranged on the outer wall of the annular wall (111), and the cleaning medium outlet (132) being arranged on the outer wall of the annular wall (111). The cleaning medium inlet (131) and the cleaning medium outlet (132) are arranged axially spaced apart from each other along the annular wall (111), the cleaning medium outlet (132) is arranged between any two adjacent comb teeth (121), and the cleaning medium outlet (132) is arranged on the outside of the comb tooth structure (12), the first connecting channel (133) is arranged inside the annular wall (111), and two ends of the first connecting channel (133) are respectively connected to the cleaning medium inlet (131) and the cleaning medium outlet (132).

2. The oil supply member according to claim 1, characterized in that: The first connecting passage (133) comprises a first connecting section (1331) and a second connecting section (1332); the first connecting section (1331) extends along the circumferential direction of the annular wall (111); the second connecting section extends along the axial direction of the annular wall (111); the cleaning medium inlet (131) is connected to the first connecting section (1331); and two ends of the second connecting section (1332) are respectively connected to the first connecting section (1331) and the cleaning medium outlet (132).

3. The oil supply member according to claim 2, characterized in that: A plurality of cleaning medium outlets (132) are provided, and the plurality of cleaning medium outlets (132) are arranged at intervals along the axial direction of the annular wall (111), and the plurality of cleaning medium outlets (132) are all connected to the second connecting section (1332).

4. The oil supply member according to claim 2, characterized in that: A plurality of the second communicating sections (1332) are provided, and the plurality of the second communicating sections (1332) are arranged at intervals along the circumference of the annular wall (111); The cleaning medium outlets (132) are provided in a plurality of groups, and the plurality of groups of cleaning medium outlets (132) are arranged at intervals along the circumference of the annular wall (111), and any group is provided with a plurality of cleaning medium outlets (132) correspondingly connected to any of the second connecting sections (1332).

5. The oil supply member according to claim 2, characterized in that: The first connecting section (1331) passes through the end of the annular wall (111) and forms a first opening (1334); The oil supply member further comprises a first cover body (14), wherein the first cover body (14) is arranged on the end of the annular wall (111) to close the first opening (1334).

6. The oil supply member according to claim 2, characterized in that: A gas injection convex portion (134) is provided on the outer wall of the annular wall (111); The cleaning medium inlet (131) is formed on the gas injection convex portion (134); The first connecting channel (133) further comprises a third connecting section (1333), wherein the third connecting section (1333) is arranged inside the gas injection protrusion (134), and two ends of the third connecting section (1333) are respectively connected to the cleaning medium inlet (131) and the first connecting section (1331).

7. The oil supply member according to any one of claims 1 to 5, characterized in that: Also includes: A liquid transmission structure (15), the liquid transmission structure (15) comprising a fuel inlet (151), a second communication channel (152) and a fuel outlet (153), the fuel inlet (151) and the cleaning medium inlet (131) being arranged radially spaced apart from each other along the annular wall (111), and the fuel inlet (151) and the comb tooth structure (12) being arranged axially spaced apart from each other along the annular wall (111), the second communication channel (152) being arranged inside the annular wall (111), the fuel outlet (153) being opened inside the second communication channel (152), and the fuel outlet (153) being communicated with the fuel inlet (151) through the second communication channel (152).

8. The oil supply member according to claim 7, characterized in that: The second communicating passage (152) comprises a fourth communicating section (1521), a fifth communicating section (1522) and a sixth communicating section (1523) which are connected to each other, the fourth communicating section (1521) extending along the circumferential direction of the annular wall (111), the fifth communicating section (1522) extending along the axial direction of the annular wall (111), and the sixth communicating section (1523) extending along the radial direction of the annular wall (111); The fuel inlet (151) is in communication with the sixth communication section (1523).

9. The oil supply member according to claim 8, characterized in that: A liquid injection convex portion (154) is provided on the outer wall of the annular wall (111), and the liquid injection convex portion (154) and the gas injection convex portion (134) are arranged at intervals along the radial direction of the annular wall (111); The fuel inlet (151) is formed in the liquid injection protrusion (154).

10. The oil supply member according to claim 8, characterized in that: The fourth connecting section (1521) passes through the other end of the annular wall (111) and forms a second opening (1524); The oil supply member further comprises a second cover body (16), wherein the second cover body (16) is arranged to cover the second opening (1524).

11. A gas turbine engine, characterized in that: include: The oil supply component is the oil supply component according to any one of claims 1 to 10; An oil-slinging plate (2), the oil-slinging plate (2) comprising a second body (21) and an annular groove (211) provided on the second body (21), the annular groove (211) being used to accommodate the annular wall (111); An air inlet pipe (3), one end of which is in communication with a discharge port of a first storage element storing a cleaning medium, and the other end of which is in communication with a cleaning medium inlet (131); An oil inlet pipe (4), one end of which is in communication with an outlet of a second storage element for storing fuel, and the other end of which is in communication with a fuel inlet (151); A flame tube (5), wherein the flame tube (5) is movably sleeved on the outer wall of the annular groove (211).

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