CN209654862U - Heat-proof device for engine periphery pipeline - Google Patents

Heat-proof device for engine periphery pipeline Download PDF

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Publication number
CN209654862U
CN209654862U CN201821808942.2U CN201821808942U CN209654862U CN 209654862 U CN209654862 U CN 209654862U CN 201821808942 U CN201821808942 U CN 201821808942U CN 209654862 U CN209654862 U CN 209654862U
Authority
CN
China
Prior art keywords
covering
insulation layer
thermal insulation
pipeline
heat
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.)
Expired - Fee Related
Application number
CN201821808942.2U
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Chinese (zh)
Inventor
储德宝
邵彬彬
潘明汉
李锋
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.)
Xi'an Huiteng Aviation Technology Co Ltd
Original Assignee
Xi'an Huiteng Aviation Technology 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 Xi'an Huiteng Aviation Technology Co Ltd filed Critical Xi'an Huiteng Aviation Technology Co Ltd
Priority to CN201821808942.2U priority Critical patent/CN209654862U/en
Application granted granted Critical
Publication of CN209654862U publication Critical patent/CN209654862U/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

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Abstract

The utility model provides a kind of heat-proof device for engine periphery pipeline, belongs to heat-insulating technique field.Heat-proof device for engine periphery pipeline includes thermal insulation layer and covering, in which: the side of thermal insulation layer is coated on around the pipeline of engine periphery, and the other side of thermal insulation layer is connect with covering;The material of thermal insulation layer is ceramic matric composite or glass fibre;Covering uses density for 7.93 × 103kg/m3, with a thickness of the stainless steel of 0.05~0.08mm, and covering is arranged to the tread patterns modeling of 1.3~1.5mm thickness.The high-temperature gas that the composite construction being made of in the utility model thermal insulation layer and covering can prevent engine periphery pipeline from generating is diffused into exterior space, so as to reduce the factor for influencing the other components in engine periphery and working normally, high-temperature gas that engine high-temperature pipeline distributes can be reduced simultaneously to the destruction of environment and the harm of personnel, moreover it is possible to guarantee the full working life of engine peripheral equipment.

Description

Heat-proof device for engine periphery pipeline
Technical field
The utility model relates to heat-insulating technique field, in particular to a kind of heat-proof device for engine periphery pipeline.
Background technique
During the work time, internal stroke and fuel combustion can generate a large amount of high-temperature gases to engine.These High Temperature Gas Know from experience through engine itself and the peripheral tubes road direction external radiation being connect with engine.Meeting pair in high-temperature gas radiative process Environment, personnel and equipment cause irreversible damage.Environment is broken to reduce the high-temperature gas that engine working process generates Bad, personnel harm and the full working life for guaranteeing equipment, the utility model provide a kind of for engine periphery pipeline Heat-proof device.
Utility model content
To solve the above-mentioned problems, the utility model provides a kind of heat-proof device for engine periphery pipeline.
In order to solve the above technical problems, the technical solution adopted in the utility model is:
A kind of heat-proof device for engine periphery pipeline comprising thermal insulation layer and covering, in which: the thermal insulation layer Side is coated on around the pipeline of engine periphery, and the other side of the thermal insulation layer is connect with the covering;The thermal insulation layer Material is ceramic matric composite or glass fibre;The covering uses density for 7.93 × 103kg/m3, with a thickness of 0.05~ The stainless steel of 0.08mm, and the covering is arranged to the tread patterns modeling of 1.3~1.5mm thickness.
Optionally, the density of the ceramic matric composite is not higher than 160kg/m3
Optionally, the thermal insulation layer with a thickness of 3~30mm.
Optionally, the material of the covering is the 0Cr18Ni9 stainless steel of 0.05~0.08mm.
Optionally, the global density of the composite construction of the thermal insulation layer and covering composition is not higher than 300kg/m3
Optionally, the shape of the tread patterns modeling is fold shape, cross or concave-convex.
The technical solution that the embodiments of the present invention provide can include the following benefits:
The thermal insulation layer made of ceramic matric composite or glass fibre is coated by the way that the covering being made of stainless steel is arranged Engine periphery pipeline is thermally shielded, the heat that the high-temperature gas of engine periphery pipeline diverging generates can be sufficiently completely cut off, Achieve the effect that protect engine periphery component.The composite construction being made of in the utility model thermal insulation layer and covering can be to prevent The high-temperature gas that only engine periphery pipeline generates is diffused into exterior space, influences the other of engine periphery so as to reduce The factor that component works normally, while the destruction and people of high-temperature gas that engine high-temperature pipeline distributes to environment can be reduced The harm of member, moreover it is possible to guarantee the full working life of engine peripheral equipment.
Detailed description of the invention
The drawings herein are incorporated into the specification and forms part of this specification, and shows and meets the utility model Embodiment, and be used to explain the principles of the present invention together with specification.
Fig. 1 is the structural schematic diagram of the heat-proof device provided by the embodiment of the utility model for engine periphery pipeline.
Specific embodiment
With reference to the accompanying drawings and examples, specific embodiment of the present utility model is described in further detail.
It is practical new to this below in conjunction with attached drawing to keep the purpose of this utility model, technical solution and advantage clearer Type embodiment is described in further detail.
As shown in Figure 1, the heat-proof device provided by the embodiment of the utility model for engine periphery pipeline comprising every Thermosphere 1 and covering 2, in which: the side of thermal insulation layer 1 is coated on around the pipeline of engine periphery, the other side of thermal insulation layer 1 and illiteracy Skin 2 connects;The material of thermal insulation layer 1 is ceramic matric composite or glass fibre;Covering 2 uses density for 7.93 × 103kg/m3, With a thickness of the stainless steel of 0.05~0.08mm, and covering 2 is arranged to the tread patterns modeling of 1.3~1.5mm thickness.
Wherein, thermal insulation layer 1 plays the role of completely cutting off heat.The material of thermal insulation layer 1 is according to relevant criterion in the utility model It is calculated with calorifics, the thermal coefficient of 1 material of thermal insulation layer should meet condition shown in the following table 1.Ceramic matric composite or Glass fibre is all satisfied condition shown in table 1.
Table 1
Serial number Temperature (DEG C) Thermal coefficient (W/m K)
1 400 0.069
2 650 0.075
3 900 0.080
Further, the material of covering 2 is calculated according to relevant criterion and mechanical performance in the utility model, covering 2 Tensile strength should meet condition shown in the following table 2.Density is 7.93 × 103kg/m3, with a thickness of the stainless of 0.05~0.08mm Steel meets condition shown in table 2.
Table 2
Serial number Temperature (DEG C) Tensile strength
1 400 ≥720MPa
2 650 ≥650MPa
3 900 ≥520MPa
Preferably, the material of covering 2 is the 0Cr18Ni9 stainless steel of 0.05~0.08mm.
The application method of the utility model are as follows: firstly, calculating engine according to the hot ability to bear of engine periphery pipeline The permission of periphery pipeline is maximum using temperature and use temperature when best performance, and corresponding thermally conductive according to calculated result selection The material of the thermal insulation layer 1 of coefficient;Then, thermal insulation layer 1 is cut by respective shapes according to the shape of engine periphery pipeline and wrapped Overlay on the surface of engine periphery pipeline;Next, selecting the material of covering 2 and covering being prepared as to the flower of 1.3~1.5mm thickness After line moulding, covering 2 is coated on to the surface of thermal insulation layer 1, and by the gap firm welding on 2 both sides of covering;Finally, polishing welding Position is allowed to impulse- free robustness and notch.
The utility model can be increased to the maximum extent by setting covering 2 to the tread patterns modeling of 1.3~1.5mm thickness The tensile property of covering 2.
Wherein, the density of ceramic matric composite is not higher than 160kg/m3, the composite construction of thermal insulation layer 1 and the composition of covering 2 Global density be not higher than 300kg/m3, so that composite construction is integrally relatively lighter, to not cause to engine periphery pipeline More burdens.
Further, the thickness of thermal insulation layer 1 is by being calculated in detail to thermal coefficient, the thermal insulation layer calculated 1 with a thickness of 3~30mm.
Optionally, the shape of tread patterns modeling is fold shape, cross or concave-convex.
Wherein, the overall thermal conductivity for the composite construction that thermal insulation layer 1 and covering 2 form is lower than the thermal coefficient of thermal insulation layer 1, Sufficiently to completely cut off the heat of engine periphery high temperature conduit diverging, engine periphery component is protected.
Embodiment of above is merely to illustrate the utility model, and is not limitation of the utility model, related technology neck The those of ordinary skill in domain, in the case where not departing from the spirit and scope of the utility model, can also make a variety of changes and Modification, therefore all equivalent technical solutions also belong to the scope of the utility model, the scope of patent protection of the utility model is answered It is defined by the claims.

Claims (6)

1. a kind of heat-proof device for engine periphery pipeline, which is characterized in that including thermal insulation layer (1) and covering (2), In:
The side of the thermal insulation layer (1) is coated on around the pipeline of engine periphery, the other side of the thermal insulation layer (1) with it is described Covering (2) connection;The material of the thermal insulation layer (1) is ceramic matric composite or glass fibre;The covering (2) uses density It is 7.93 × 103kg/m3, with a thickness of the stainless steel of 0.05~0.08mm, and the covering (2) is arranged to 1.3~1.5mm thickness Tread patterns modeling.
2. the heat-proof device according to claim 1 for engine periphery pipeline, which is characterized in that the ceramic base is multiple The density of condensation material is not higher than 160kg/m3
3. the heat-proof device according to claim 1 for engine periphery pipeline, which is characterized in that the thermal insulation layer (1) with a thickness of 3~30mm.
4. the heat-proof device according to claim 1 for engine periphery pipeline, which is characterized in that the covering (2) Material be 0.05~0.08mm 0Cr18Ni9 stainless steel.
5. the heat-proof device according to claim 1 for engine periphery pipeline, which is characterized in that the thermal insulation layer (1) and the global density of the composite construction of covering (2) composition is not higher than 300kg/m3
6. according to claim 1 to the heat-proof device for being used for engine periphery pipeline described in any claim in 5, feature It is, the shape of the tread patterns modeling is fold shape, cross or concave-convex.
CN201821808942.2U 2018-10-22 2018-10-22 Heat-proof device for engine periphery pipeline Expired - Fee Related CN209654862U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201821808942.2U CN209654862U (en) 2018-10-22 2018-10-22 Heat-proof device for engine periphery pipeline

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201821808942.2U CN209654862U (en) 2018-10-22 2018-10-22 Heat-proof device for engine periphery pipeline

Publications (1)

Publication Number Publication Date
CN209654862U true CN209654862U (en) 2019-11-19

Family

ID=68506207

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201821808942.2U Expired - Fee Related CN209654862U (en) 2018-10-22 2018-10-22 Heat-proof device for engine periphery pipeline

Country Status (1)

Country Link
CN (1) CN209654862U (en)

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Granted publication date: 20191119