CN217841769U - Be used for aviation piston engine lubricating oil adapter - Google Patents
Be used for aviation piston engine lubricating oil adapter Download PDFInfo
- Publication number
- CN217841769U CN217841769U CN202221788467.3U CN202221788467U CN217841769U CN 217841769 U CN217841769 U CN 217841769U CN 202221788467 U CN202221788467 U CN 202221788467U CN 217841769 U CN217841769 U CN 217841769U
- Authority
- CN
- China
- Prior art keywords
- adapter
- lubricating oil
- relief valve
- main part
- piston engine
- 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.)
- Active
Links
Images
Landscapes
- Lubrication Of Internal Combustion Engines (AREA)
Abstract
The utility model provides a be used for aviation piston engine lubricating oil adapter, including the lubricating oil adapter main part, the lateral part of lubricating oil adapter main part is provided with the relief valve of adapter, the relief valve of adapter include adapter safety valve core be provided with adapter relief valve spring on the adapter safety valve core, adapter relief valve spring one end is provided with the steel ball, the relief valve of adapter inserts inside it from the lateral part of lubricating oil adapter main part to seal through seal ring, lubricating oil adapter main part upper portion still is provided with two conversion pipeline elbow joints, the utility model discloses engine lubricating oil adapter is connected with aviation piston engine main part and lubricating oil radiator lubricating oil, provides the relief valve structure of adapter, prevents that lubricating oil cooling device from being damaged, and control lubricating oil pressure has protected lubricating oil cooling device to fix hose connection position, prevented that hookup location's hose from damaging.
Description
Technical Field
The utility model relates to an aeroengine spare part structural design technical field especially relates to a be used for aeropiston engine lubricating oil adapter.
Background
The main part of aviation piston engine is at the during operation, usually with lubricating oil radiator lug connection, long-term operation can lead to lubricating oil pressure unstable, easily produces the damage to lubricating oil cooling device, and the unable fixed and hose connection department of coupling hose direction harms easily.
SUMMERY OF THE UTILITY MODEL
The utility model aims at providing a be used for aviation piston engine lubricating oil adapter, with the main part cooperation work of engine, can control lubricating oil pressure to fixed hose connection position, prevented that connection position's hose from damaging.
To achieve the purpose, the utility model adopts the following technical proposal: the utility model provides a be used for aviation piston engine lubricating oil adapter, includes the lubricating oil adapter main part, the lubricating oil adapter main part is hollow structure, the lateral part of lubricating oil adapter main part is provided with the relief valve of adapter, the relief valve of adapter include adapter safety valve core be provided with adapter relief valve spring on the adapter safety valve core, adapter relief valve spring one end is provided with the steel ball, the relief valve of adapter inserts it inside from the lateral part of lubricating oil adapter main part to seal through seal ring, lubricating oil adapter main part upper portion still is provided with two switching pipeline elbow joints.
Further, the bottom end face of the lubricating oil adapter main body is also provided with a sealing gasket.
The utility model discloses engine lubricating oil adapter is connected with aviation piston engine main part and lubricating oil radiator lubricating oil, provides the relief valve structure of adapter, prevents that lubricating oil cooling device from being damaged, and control lubricating oil pressure has protected lubricating oil cooling device to fix hose connection position, prevented that hookup location's hose from damaging.
Drawings
FIG. 1 is a front view of an oil adapter structure for an aviation piston engine according to the present invention;
FIG. 2 is a side view of the structure of the lubricating oil adapter for an aviation piston engine according to the present invention;
in the figure: the method comprises the following steps of 1-lubricating oil adapter main body, 2-switching pipeline elbow joint, 3-adapter safety valve core, 4-adapter safety valve spring, 5-sealing washer, 6-sealing washer, 7-steel ball and 8-plug.
Detailed Description
In order to facilitate understanding of the present invention, the present invention will be described more fully hereinafter with reference to the accompanying drawings. Preferred embodiments of the present invention are shown in the drawings. The invention may, however, be embodied in many different forms and should not be construed as limited to the embodiments set forth herein. Rather, these embodiments are provided so that this disclosure will be thorough and complete.
As shown in fig. 1-2, a lubricating oil adapter for an aviation piston engine comprises a lubricating oil adapter main body 1, wherein the lubricating oil adapter main body is of a hollow structure, a safety valve 2 of the adapter is arranged on the side portion of the lubricating oil adapter main body, the safety valve of the adapter comprises an adapter safety valve core 3, an adapter safety valve spring 4 is arranged on the adapter safety valve core, a steel ball 7 is arranged at one end of the adapter safety valve spring, the safety valve of the adapter is inserted into the adapter main body from the side portion of the lubricating oil adapter main body and is sealed through a sealing washer 5, two conversion pipeline bent joints 2 are further arranged on the upper portion of the lubricating oil adapter main body, a sealing gasket 6 is further arranged on the bottom end face of the lubricating oil adapter main body, and a plug 8 is further arranged on the upper pipeline of the lubricating oil adapter main body.
The utility model discloses the flexible pipe of advancing, going out that lubricating oil cooling device is connected respectively to adapter conversion pipeline elbow joint, and the terminal surface and the machine casket of lubricating oil adapter are connected, provide power through the hydraulic pump, make the lubricating oil pass through the relief valve of adapter, controlled to go to after the lubricating oil pressure again among the lubricating oil cooling device, protected lubricating oil cooling device, pass through the lubricating oil adapter again after the lubricating oil cooling, be connected to the oil circuit, provide low temperature lubricating oil for the engine.
The utility model discloses engine lubricating oil adapter is connected with aviation piston engine main part and lubricating oil radiator lubricating oil, provides the relief valve structure of adapter, prevents that lubricating oil cooling device from being damaged, and control lubricating oil pressure has protected lubricating oil cooling device to fix hose connection position, prevented that hookup location's hose from damaging.
Claims (2)
1. The utility model provides a be used for aviation piston engine lubricating oil adapter, includes the lubricating oil adapter main part, the lubricating oil adapter main part is hollow structure, its characterized in that, the lateral part of lubricating oil adapter main part is provided with the relief valve of adapter, the relief valve of adapter include adapter safety valve core be provided with adapter relief valve spring on the adapter safety valve core, adapter relief valve spring one end is provided with the steel ball, the relief valve of adapter inserts its inside from the lateral part of lubricating oil adapter main part to seal through seal ring, lubricating oil adapter main part upper portion still is provided with two conversion pipeline knee joints.
2. The adapter of claim 1, wherein the bottom end face of the body of the adapter is further provided with a gasket.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202221788467.3U CN217841769U (en) | 2022-07-12 | 2022-07-12 | Be used for aviation piston engine lubricating oil adapter |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202221788467.3U CN217841769U (en) | 2022-07-12 | 2022-07-12 | Be used for aviation piston engine lubricating oil adapter |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN217841769U true CN217841769U (en) | 2022-11-18 |
Family
ID=84038106
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202221788467.3U Active CN217841769U (en) | 2022-07-12 | 2022-07-12 | Be used for aviation piston engine lubricating oil adapter |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN217841769U (en) |
-
2022
- 2022-07-12 CN CN202221788467.3U patent/CN217841769U/en active Active
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN217841769U (en) | Be used for aviation piston engine lubricating oil adapter | |
| CN212428697U (en) | Coiled tubing well head blowout preventer | |
| CN217328941U (en) | Quick joint for pipeline | |
| CN206036472U (en) | Two -way sealing quick -operation joint | |
| CN212616928U (en) | Hydraulic hose connector with good sealing performance | |
| CN212616963U (en) | Three-way hose connector with low occupied area | |
| CN212617036U (en) | Novel flexible hose joint is restoreed in non-excavation of oil field pipeline | |
| CN211306145U (en) | Improved hydraulic wrench | |
| CN210890473U (en) | Double-layer protection type high-pressure oil pipe with replaceable lantern ring assembly | |
| CN212313671U (en) | Improved oil inlet pipeline of steering gear | |
| CN203463832U (en) | Insulation connector | |
| CN219493441U (en) | Two-way flange for hydraulic pipeline end of hydraulic press | |
| CN214998531U (en) | Safety control valve for hydraulic pneumatic control system | |
| CN214888853U (en) | Sealing element of piston type energy accumulator | |
| CN209819027U (en) | Buckling type hydraulic rubber pipe joint | |
| CN211344310U (en) | Double-layer protection type high-pressure oil pipe with two ends incapable of being high | |
| CN218439869U (en) | Sealing structure of middle tap pipe of water feeding pump | |
| CN217602772U (en) | Forced pressure relief device of cooling system of mining dump truck | |
| CN221221852U (en) | Quick-inserting mechanism for gas-liquid communication of automatic equipment | |
| CN215928294U (en) | Power assembly and engineering machinery | |
| CN220705609U (en) | Rotary guide double-cylinder hydraulic section module for petroleum drilling and production | |
| CN213598783U (en) | Flange type hydraulic connecting joint | |
| CN218762075U (en) | High-pressure movable elbow | |
| CN212671705U (en) | Environment-friendly underground oil drainage tool | |
| CN217899221U (en) | Pipeline connecting structure |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant |