CN211924880U - Watertight structure of movable pipe shaft of airplane - Google Patents
Watertight structure of movable pipe shaft of airplane Download PDFInfo
- Publication number
- CN211924880U CN211924880U CN201921985701.XU CN201921985701U CN211924880U CN 211924880 U CN211924880 U CN 211924880U CN 201921985701 U CN201921985701 U CN 201921985701U CN 211924880 U CN211924880 U CN 211924880U
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- rain shield
- aircraft
- conical
- annular
- rudder
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Abstract
The utility model belongs to in aircraft seal structure field, specifically an aircraft activity hollow shaft watertight structure, this structure mainly comprises toper rain shield, annular rain shield, rudder pivot and fuselage covering etc. and each part adopts sealed riveting connection form. The utility model discloses can block the inside that the rainwater got into the aircraft from the rudder pivot, reduce aircraft structure and airborne equipment's corrosion, improve flight safety.
Description
Technical Field
The utility model belongs to aircraft seal structure field specifically is an aircraft rudder pivot watertight structure, can block that the rainwater gets into the inside structure of aircraft from the rudder pivot.
Background
The problem of water leakage of the rudder rotating shaft mainly has two ways, namely, a water receiving box is added at the bottom of the rotating shaft and then is led out of the machine body through a water pipe; and secondly, water leakage holes are additionally arranged at the bottom of the airplane for draining water. Neither of the above two solutions can solve the problem of passive drainage of rainwater into the interior of the aircraft. The utility model relates to a rudder pivot watertight structure can block that the rainwater gets into the inside structure of aircraft from the rudder pivot.
Disclosure of Invention
The utility model discloses the purpose is guaranteed the rudder pivot watertight, can block that the rainwater gets into the inside structure of aircraft from the rudder pivot.
Technical scheme
A watertight structure of an airplane movable pipe shaft comprises a conical rain shield and an annular rain shield, wherein the conical rain shield is arranged on a rudder rotating shaft at an opening of an airplane body, and the annular rain shield is arranged around an opening skin of the airplane body; the conical rain shield and the annular rain shield are in sealing riveting with the machine body and the rudder rotating shaft.
The conical rain shield and the annular rain shield are made of aluminum alloy.
The thickness of the conical rain shield and the annular rain shield is 2 mm.
The top end part of the conical rain shield is provided with a round hole, and the round hole is in gapless connection with the rudder rotating shaft.
And sealant is coated between the conical rain shield and the rudder.
The annular rain shield is cylindrical with a flange, and the flange is in sealing riveting with the machine body.
Technical effects
Compared with the prior art, the utility model has the advantages that: the utility model discloses can block the inside that the rainwater got into the aircraft from the rudder pivot, reduce the corrosion of aircraft structure, improve flight safety.
Drawings
FIG. 1 is a view of a conical rain screen
FIG. 2 is a view of an annular rain shield
FIG. 3 is an assembly drawing of the present invention
Detailed Description
The invention will be described in further detail with reference to the following detailed description and accompanying drawings:
1. the conical rain shield is made of a thin aluminum alloy plate, is in a sealing riveting connection with the rudder pipe shaft, is installed inside the rudder, and is prevented from being influenced by air flow during flying.
2. The annular rain shield is made of a thin aluminum alloy plate and is in sealing riveting connection with a fuselage skin.
3. After assembly, the conical rain shield rotates along with the rudder, and water flows to the fuselage skin along the rain shield.
A watertight structure of an airplane movable pipe shaft comprises a conical rain shield and an annular rain shield, wherein the conical rain shield is arranged on a rudder rotating shaft at an opening of an airplane body, and the annular rain shield is arranged around an opening skin of the airplane body; the conical rain shield and the annular rain shield are in sealing riveting with the machine body and the rudder rotating shaft.
The conical rain shield and the annular rain shield are made of aluminum alloy.
The thickness of the conical rain shield and the annular rain shield is 2 mm.
The top end part of the conical rain shield is provided with a round hole, and the round hole is in gapless connection with the rudder rotating shaft.
And sealant is coated between the conical rain shield and the rudder.
The annular rain shield is cylindrical with a flange, and the flange is in sealing riveting with the machine body.
Claims (6)
1. The utility model provides an aircraft activity hollow shaft watertight construction which characterized in that: the rain shield comprises a conical rain shield and an annular rain shield, wherein the conical rain shield is arranged on a rudder rotating shaft at an opening of a machine body, and the annular rain shield is arranged around a skin of the opening of the machine body; the conical rain shield and the annular rain shield are in sealing riveting with the machine body and the rudder rotating shaft.
2. An aircraft activity pipe shaft watertight construction according to claim 1 wherein: the conical rain shield and the annular rain shield are made of aluminum alloy.
3. An aircraft activity pipe shaft watertight construction according to claim 1 wherein: the thickness of the conical rain shield and the annular rain shield is 2 mm.
4. An aircraft activity pipe shaft watertight construction according to claim 1 wherein: the top end part of the conical rain shield is provided with a round hole, and the round hole is in gapless connection with the rudder rotating shaft.
5. An aircraft activity pipe shaft watertight construction according to claim 1 wherein: and sealant is coated between the conical rain shield and the rudder.
6. An aircraft activity pipe shaft watertight construction according to claim 1 wherein: the annular rain shield is cylindrical with a flange, and the flange is in sealing riveting with the machine body.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201921985701.XU CN211924880U (en) | 2019-11-15 | 2019-11-15 | Watertight structure of movable pipe shaft of airplane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201921985701.XU CN211924880U (en) | 2019-11-15 | 2019-11-15 | Watertight structure of movable pipe shaft of airplane |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN211924880U true CN211924880U (en) | 2020-11-13 |
Family
ID=73318715
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201921985701.XU Active CN211924880U (en) | 2019-11-15 | 2019-11-15 | Watertight structure of movable pipe shaft of airplane |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN211924880U (en) |
-
2019
- 2019-11-15 CN CN201921985701.XU patent/CN211924880U/en active Active
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CP03 | Change of name, title or address |
Address after: 723213 Liulin Town, Chenggu County, Hanzhong City, Shaanxi Province Patentee after: Shaanxi Aircraft Industry Co.,Ltd. Address before: 723213 box 34, Hanzhong City, Shaanxi Province Patentee before: Shaanxi Aircraft INDUSTRY(GROUP) Co.,Ltd. |
|
| CP03 | Change of name, title or address |