CN204297049U - A kind of lid rhone - Google Patents
A kind of lid rhone Download PDFInfo
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- CN204297049U CN204297049U CN201420684245.6U CN201420684245U CN204297049U CN 204297049 U CN204297049 U CN 204297049U CN 201420684245 U CN201420684245 U CN 201420684245U CN 204297049 U CN204297049 U CN 204297049U
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- rhone
- lid
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- osculum
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Abstract
The utility model discloses a kind of lid rhone, it is characterized in that, described lid rhone is closed hoop structure, in the least significant end of described rhone (5), osculum is set, described osculum connects discharge pipe line (6), a set of rhone is had under the rhone that the utility model designs makes each lid, be not related with other lids, effectively lid opposite joint can be leaked and after the leaking and catch of each nail, in time water is discharged body, reduce to leak and have water to the infringement of interior of aircraft system, and the intensity of original structure can not be reduced.
Description
Technical field
The utility model belongs to aeroplane structure design, relates to a kind of lid rhone.
Background technology
At present, it is paving sealing gasket that large-scale military, civilian airplane back lid waterproof measure uses more, and conventional rubber sealing gasket is easily aging or resilience is bad, and long-time use will lose waterproof effect.Draining aspect, the in-line rhone of many employings is connected directly between on the web of frame, beam, not easily locates during assembling.Ponding is flowed by the difference of height of rhone, if assemble improper, ponding can overflow from rhone.Because tandem rhone is not have a closed rhone under each lid, rhone is crossing frame or Liang Shixu structurally carries out perforate, reduces the intensity of structure to a certain extent.This rhone reserve construction space need to the securing member of docking by structure cross docking area, then cannot receive lid leaking near cross docking area.
Utility model content
The technical problems to be solved in the utility model is, provides a kind of lid rhone, easy construction and version is simple and reliable and can not reduce the intensity of original structure.
For the technical solutions of the utility model that solve the problem provide a kind of lid rhone, described lid rhone is closed hoop structure, arranges osculum in the least significant end of described rhone 5, and described osculum connects discharge pipe line 6.
Preferably, described rhone 5 is connected on mouthful frame 3 removably by connecting gusset plate 4.
Preferably, rhone 5 adopts segmented, and segmentation place uses grooved interfacing part 7 to dock, and does binding face sealing
A set of rhone is had under each lid, be not related with other lids, effectively lid opposite joint can be leaked and after the leaking and catch of each nail, in time water be discharged body, reduce to leak and have water to the infringement of interior of aircraft system, and the intensity of original structure can not be reduced.
Accompanying drawing explanation
Below in conjunction with accompanying drawing, the utility model is described in more detail, wherein:
Fig. 1 is a kind of lid rhone;
Fig. 2 is garland, connects gusset plate and discharge pipe line.
Detailed description of the invention
Below the utility model is described in further details:
The utility model provides a kind of lid rhone, is a kind of discharge structure be arranged on below lid.Lid corner is designed to fillet, facilitates shaping in corner of rhone.Sealing gasket 2 can use the silicone rubber seal gasket that resilience is higher.Rhone 5 be connected gusset plate 4 and adopt rivet interlacement, connecting gusset plate 4 uses plate nut to be connected with bolt with mouth frame 3, facilitate maintenance and the replacing of rhone, in order to reduce production cost, rhone 5 can adopt segmented, segmentation place uses grooved interfacing part 7 to dock, and does binding face sealing, and wet connection adopted by docking securing member.As shown in Figure 2, osculum is set in the minimum point of rhone 5, discharge pipe line 6 is welded with rhone 5, rhone internal water accumulation is discharged outside body by discharge pipe line 6.Need ensure during installing port cover lock that lockhole is within the scope of rhone, can be caught by rhone to ensure that lockhole leaks.
Claims (3)
1. a lid rhone, is characterized in that, described lid rhone is closed hoop structure, arranges osculum in the least significant end of described rhone (5), and described osculum connects discharge pipe line (6).
2. rhone according to claim 1, is characterized in that, described rhone (5) is connected on a mouthful frame (3) removably by connecting gusset plate (4).
3. rhone according to claim 1, is characterized in that, rhone (5) adopts segmented, and segmentation place uses grooved interfacing part (7) docking, and does binding face sealing.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201420684245.6U CN204297049U (en) | 2014-11-14 | 2014-11-14 | A kind of lid rhone |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
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CN201420684245.6U CN204297049U (en) | 2014-11-14 | 2014-11-14 | A kind of lid rhone |
Publications (1)
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CN204297049U true CN204297049U (en) | 2015-04-29 |
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Family Applications (1)
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CN201420684245.6U Active CN204297049U (en) | 2014-11-14 | 2014-11-14 | A kind of lid rhone |
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Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN109606613A (en) * | 2018-11-07 | 2019-04-12 | 中国航空工业集团公司西安飞机设计研究所 | A kind of side wall lid discharge structure |
CN110816808A (en) * | 2019-12-04 | 2020-02-21 | 中国直升机设计研究所 | Non-closed waterproof opening cover assembly |
-
2014
- 2014-11-14 CN CN201420684245.6U patent/CN204297049U/en active Active
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN109606613A (en) * | 2018-11-07 | 2019-04-12 | 中国航空工业集团公司西安飞机设计研究所 | A kind of side wall lid discharge structure |
CN110816808A (en) * | 2019-12-04 | 2020-02-21 | 中国直升机设计研究所 | Non-closed waterproof opening cover assembly |
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C14 | Grant of patent or utility model | ||
GR01 | Patent grant |