CN204783323U - Spray tube adjustment sheet heat screen coupling mechanism - Google Patents
Spray tube adjustment sheet heat screen coupling mechanism Download PDFInfo
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- CN204783323U CN204783323U CN201520489835.8U CN201520489835U CN204783323U CN 204783323 U CN204783323 U CN 204783323U CN 201520489835 U CN201520489835 U CN 201520489835U CN 204783323 U CN204783323 U CN 204783323U
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- heat screen
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Abstract
The utility model provides a spray tube adjustment sheet heat screen coupling mechanism, relates to the aeroengine structural design field for the pneumatic flow path of adjustment aeroengine axial symmetry contracting nozzle, the support sets up between combined material heat screen and adjustment sheet, and the structure of support for being provided with the cavity support on the support base is provided with the bar hole on parallel of cavity support and the support base, and the nut card of bolt is in in the cavity support, the screw rod of bolt stretches out the bar hole and the cover has the bush. On the adjustment sheet is fixed in the bolt through the nut, between bush and the nut. The utility model provides a spray tube adjustment sheet heat screen coupling mechanism be convenient for assembly and dismantlement, high, the safe and reliable of device stability are through setting up between heat screen and adjustment sheet the utility model provides a spray tube adjustment sheet heat screen coupling mechanism makes the heat screen match with high expansion -pressure ratio metal material heat under high temperature environment.
Description
Technical field
The utility model belongs to aeroengine field of structural design, in particular to a kind of flap heat screen bindiny mechanism.
Background technique
Aeroengine axisymmetric contracting nozzle is provided with adjustment sheet for adjusting pneumatic stream, and adjustment sheet wall is easily subject to the ablation of high-temperature fuel gas, needs to increase metallic material heat screen mechanism at adjustment sheet wall and blocks high-temperature fuel gas.Compared to traditional metallic material, composite material, due to advantages such as temperature tolerance are strong, proportion is low, fire-resistant gas scouring capability is strong, is applicable to heat screen.But composite material has following restrictive condition: be difficult to heat under hot environment with high expansion ratio metal material materials and parts and mate, on composite material element, hole arranged and influential point of tendons reduces fiber continuity thus reduction mechanical property, and composite material heat screen cost height need possess interchangeability.The problem needing now solution badly how to design a kind of bindiny mechanism can overcome above-mentioned shortcoming.
Model utility content
The purpose of this utility model is to solve above-mentioned deficiency of the prior art, provide a kind of simple and reasonable, make the hot flap heat screen bindiny mechanism of mating of composite material heat screen and high expansion ratio metal material materials and parts.
The purpose of this utility model is achieved through the following technical solutions: a kind of flap heat screen bindiny mechanism, comprise support, bolt, lining, wherein, support is structure bracket base being provided with hollow seats, hollow seats and bracket base parallel surface are provided with bar hole, the nut of bolt is stuck in described hollow seats, and the screw rod of bolt stretches out bar hole and cover has lining.
In such scheme preferably, Bracket setting is between composite material heat screen and adjustment sheet, and bracket base is fixedly connected with composite material heat screen by rivet by described support, and adjustment sheet is fixed on bolt, between lining and nut by nut.
In above-mentioned either a program preferably, the outer annular diameter of lining is greater than the width of the bar hole on support.
In above-mentioned either a program preferably, nut is connected with bolt thread, and the diameter of the nut of bolt is greater than the strip hole on described support.
In above-mentioned either a program preferably, the quantity of the described support be connected with adjusting vane is at least two.
The beneficial effect of flap heat screen bindiny mechanism provided by the utility model is, be convenient to assembling and dismounting, device stability is high, safe and reliable, be easy to realize, the flap heat screen bindiny mechanism provided by arranging the utility model between heat screen with adjustment sheet makes heat screen mate with high expansion ratio metallic material heat in high temperature environments.
Accompanying drawing explanation
Fig. 1 is the structural representation of the preferred embodiment according to flap heat screen bindiny mechanism of the present utility model;
Fig. 2 is the structure sectional view embodiment illustrated in fig. 1 according to flap heat screen bindiny mechanism of the present utility model;
Fig. 3 is embodiment illustrated in fig. 1 and composite material heat screen, adjustment sheet package assembly sectional view according to flap heat screen bindiny mechanism of the present utility model.
Reference character:
1-support, 2-bolt, 3-lining, 4-nut, A-adjustment sheet, B-composite material heat screen.
Embodiment
In order to understand the flap heat screen bindiny mechanism according to the utility model scheme better, be further elaborated explanation below in conjunction with the preferred embodiment of accompanying drawing to flap heat screen bindiny mechanism of the present utility model.
As shown in Figure 1-Figure 3, a kind of flap heat screen bindiny mechanism that the utility model provides, comprise support 1, bolt 2, lining 3, wherein, support 1 is structure bracket base being provided with hollow seats, hollow seats and bracket base parallel surface are provided with bar hole, and the nut of bolt 2 is stuck in described hollow seats, and the screw rod of bolt 2 stretches out bar hole and cover has lining 3.
Support 1 is arranged between composite material heat screen B and adjustment sheet A, and bracket base is fixedly connected with composite material heat screen B by rivet by support 1, and adjustment sheet A is fixed on bolt 2, between lining 3 and nut 4 by nut 4.The outer annular diameter of lining 3 is greater than the width of the bar hole on support 1.Nut 4 is threaded with bolt 2, and the diameter of the nut of bolt 2 is greater than the strip hole on support 1.The quantity of the support 1 be connected with adjusting vane A is at least two.
Bolt 2, lining 3 and one direction can be moved in the chute of support 1 as a whole by the adjustment sheet A that nut 4 is fixing, and then realize single-degree-of-freedom between adjustment sheet A and composite material heat screen B and connect, improve the heat coupling between adjustment sheet A and composite material heat screen B under hot environment.
Originally a kind of flap heat screen bindiny mechanism provided, use the two-dimensional flat plate structure ensureing the optimum mechanical property of composite material, realize low bulk to mate than the good heat between composite material with high expansion ratio metallic material parts, hot matching capacity is good, composite fiber continuity is high, be easy to dismounting, structure is simple.
More than be described in detail in conjunction with flap heat screen bindiny mechanism of the present utility model specific embodiment, but be not to restriction of the present utility model, everyly according to technical spirit of the present utility model, technical scope of the present utility model is all belonged to any simple modification made for any of the above embodiments, also it should be noted that, comprise the combination in any between each part mentioned above according to the category of flap heat screen bindiny mechanism of the present utility model technological scheme.
Claims (5)
1. a flap heat screen bindiny mechanism, it is characterized in that, comprise support (1), bolt (2), lining (3), wherein, support (1) is for bracket base being provided with the structure of hollow seats, hollow seats and bracket base parallel surface are provided with bar hole, and the nut of bolt (2) is stuck in described hollow seats, and the screw rod of bolt (2) stretches out bar hole and cover has lining (3).
2. flap heat screen bindiny mechanism as claimed in claim 1, it is characterized in that: described support (1) is arranged between composite material heat screen (B) and adjustment sheet (A), bracket base is fixedly connected with composite material heat screen (B) by rivet by described support (1), and adjustment sheet (A) is fixed on bolt (2), between lining (3) and nut (4) by nut (4).
3. flap heat screen bindiny mechanism as claimed in claim 2, is characterized in that: the outer annular diameter of described lining (3) is greater than the width of the bar hole on described support (1).
4. flap heat screen bindiny mechanism as claimed in claim 2, it is characterized in that: nut (4) is threaded with described bolt (2), the diameter of the nut of described bolt (2) is greater than the strip hole on described support (1).
5. the flap heat screen bindiny mechanism as described in above-mentioned arbitrary claim, is characterized in that: the quantity of the described support (1) be connected with adjusting vane (A) is at least two.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
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CN201520489835.8U CN204783323U (en) | 2015-07-09 | 2015-07-09 | Spray tube adjustment sheet heat screen coupling mechanism |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
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CN201520489835.8U CN204783323U (en) | 2015-07-09 | 2015-07-09 | Spray tube adjustment sheet heat screen coupling mechanism |
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CN204783323U true CN204783323U (en) | 2015-11-18 |
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CN201520489835.8U Active CN204783323U (en) | 2015-07-09 | 2015-07-09 | Spray tube adjustment sheet heat screen coupling mechanism |
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Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN108678871A (en) * | 2017-12-26 | 2018-10-19 | 中国航发四川燃气涡轮研究院 | A kind of jet pipe heat insulation structural for thrust deflexion jet engine |
CN113217224A (en) * | 2021-06-21 | 2021-08-06 | 中国航发沈阳发动机研究所 | Spray tube adjusting sheet and heat shield integrated structure |
CN113623084A (en) * | 2021-10-13 | 2021-11-09 | 中国航发四川燃气涡轮研究院 | Efficient combined cooling structure suitable for exhaust system of binary vector spray pipe |
CN114013669A (en) * | 2021-11-23 | 2022-02-08 | 中国航发沈阳发动机研究所 | Aeroengine capable of realizing short-time strong infrared stealth |
CN114151227A (en) * | 2021-10-20 | 2022-03-08 | 中国航发四川燃气涡轮研究院 | Heat shield structure for binary vector spray pipe |
-
2015
- 2015-07-09 CN CN201520489835.8U patent/CN204783323U/en active Active
Cited By (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN108678871A (en) * | 2017-12-26 | 2018-10-19 | 中国航发四川燃气涡轮研究院 | A kind of jet pipe heat insulation structural for thrust deflexion jet engine |
CN108678871B (en) * | 2017-12-26 | 2020-12-29 | 中国航发四川燃气涡轮研究院 | Jet pipe heat insulation structure for thrust steering jet engine |
CN113217224A (en) * | 2021-06-21 | 2021-08-06 | 中国航发沈阳发动机研究所 | Spray tube adjusting sheet and heat shield integrated structure |
CN113623084A (en) * | 2021-10-13 | 2021-11-09 | 中国航发四川燃气涡轮研究院 | Efficient combined cooling structure suitable for exhaust system of binary vector spray pipe |
CN114151227A (en) * | 2021-10-20 | 2022-03-08 | 中国航发四川燃气涡轮研究院 | Heat shield structure for binary vector spray pipe |
CN114013669A (en) * | 2021-11-23 | 2022-02-08 | 中国航发沈阳发动机研究所 | Aeroengine capable of realizing short-time strong infrared stealth |
CN114013669B (en) * | 2021-11-23 | 2023-08-04 | 中国航发沈阳发动机研究所 | Aeroengine capable of realizing short-time strong infrared stealth |
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