CN208516937U - A kind of adjustable hose lubricating oil oiling tooling of aircraft engine - Google Patents
A kind of adjustable hose lubricating oil oiling tooling of aircraft engine Download PDFInfo
- Publication number
- CN208516937U CN208516937U CN201820847219.9U CN201820847219U CN208516937U CN 208516937 U CN208516937 U CN 208516937U CN 201820847219 U CN201820847219 U CN 201820847219U CN 208516937 U CN208516937 U CN 208516937U
- Authority
- CN
- China
- Prior art keywords
- funnel
- hand
- lubricating oil
- held part
- aircraft 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.)
- Expired - Fee Related
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- Lubrication Details And Ventilation Of Internal Combustion Engines (AREA)
Abstract
The utility model discloses a kind of adjustable hose lubricating oil oiling toolings of aircraft engine, including funnel, hand-held part, metal hose and the "-" type spiral shell edge of a knife；The beneficial effects of the utility model are that the filling conduit under funnel is changed to adjustable metal hose, facilitate and operate under the confined space, are directed at engine oil filler, prevent oil spilling；In addition, bell mouth designs a word spiral shell blade type edge of a knife at, it is open for lubricating oil tank.Without individually borrowing a word spiral shell knife again, facilitates operation, improves efficiency, and can prevent tool from losing.
Description
Technical field
The utility model relates to mechanical frock field of tool more particularly to a kind of adjustable hose lubricating oil of aircraft engine to add
Oily tooling.
Background technique
Currently, the oil filling pipe of the funnel bottom of existing oiling tooling can not be adjusted, therefore in the limited situation in space not
Only staff is inconvenient, and is easy to appear the oil spilling situation of lubricating oil；Secondly, existing oil supplier needs before refueling
Lubricating oil tank additionally is opened using a word spiral shell knife therefore not only to need to carry excessive tool, but also be easy to cause a word spiral shell knife
Surface is stained with greasy dirt and influences its normal use.
Utility model content
The purpose of this utility model: providing a kind of aircraft engine adjustable hose lubricating oil oiling tooling, improves existing fly
Machine motor oil oiling tooling, facilitates operation, improves efficiency, and prevents oil spilling and tool from losing.
To achieve the goals above, the technical solution of the utility model is: a kind of adjustable hose lubricating oil of aircraft engine
Oiling tooling, including funnel, hand-held part, metal hose and the "-" type spiral shell edge of a knife；The funnel is metal funnel-shaped structure；Institute
The funnel top surface diameter stated is greater than the funnel basal diameter；The hand-held part is round hard tube；The hand-held part top
Face is connect with the funnel bottom surface, and the two is structure as a whole；The hand-held part axis and the funnel axis weight
It closes；The metal hose is that cross section is round, and the hand-held part bottom surface is arranged in the metal hose；It is described
The "-" type spiral shell edge of a knife be flat cuboid structure, and top surface is provided with chamfering；The "-" type spiral shell edge of a knife bottom surface with it is described
Funnel top surface edge connection, and the two by welding manner connection；The "-" type spiral shell edge of a knife plane of symmetry and described
Co-planar where funnel radius.
The adjustable hose lubricating oil oiling tooling of above-mentioned aircraft engine, wherein the hand-held part axis and described
Metal hose axis is tangent in the two junction.
The adjustable hose lubricating oil oiling tooling of above-mentioned aircraft engine, wherein the metal hose outer diameter with it is described
Hand-held part outer diameter it is identical.
The adjustable hose lubricating oil oiling tooling of above-mentioned aircraft engine, wherein the metal hose internal diameter with it is described
Hand-held part internal diameter it is identical.
The adjustable hose lubricating oil oiling tooling of above-mentioned aircraft engine, wherein the metal hose length is greater than institute
The hand-held part length stated.
The adjustable hose lubricating oil oiling tooling of above-mentioned aircraft engine, wherein the hand-held part length is less than described
Funnel length.
The adjustable hose lubricating oil oiling tooling of above-mentioned aircraft engine, wherein the "-" type spiral shell edge of a knife width is small
In the funnel top surface edge width.
In conclusion the beneficial effects of the utility model are, the filling conduit under funnel is changed to adjustable metal hose, side
Just it is operated under the confined space, is directed at engine oil filler, prevents oil spilling；In addition, bell mouth designs a word spiral shell blade type edge of a knife at,
It is open for lubricating oil tank.Without individually borrowing a word spiral shell knife again, facilitates operation, improves efficiency, and can prevent tool from losing.
Detailed description of the invention
Fig. 1 is a kind of structural schematic diagram of the aircraft engine of the utility model with adjustable hose lubricating oil oiling tooling.
Fig. 2 is a kind of front view of the aircraft engine of the utility model with adjustable hose lubricating oil oiling tooling.
Fig. 3 is a kind of side view of the aircraft engine of the utility model with adjustable hose lubricating oil oiling tooling.
Specific embodiment
The embodiments of the present invention that the following is further explained with reference to the attached drawings.
It refers to shown in attached drawing 1 to attached drawing 3, a kind of aircraft engine adjustable hose lubricating oil oiling tooling, including funnel
1, hand-held part 2, metal hose 3 and the "-" type spiral shell edge of a knife 4；The funnel 1 is metal funnel-shaped structure；The funnel 1 pushes up
Face diameter is greater than 1 basal diameter of funnel；The hand-held part 2 is round hard tube；2 top surface of hand-held part with it is described
Funnel bottom surface 1 connect, and the two is structure as a whole；2 axis of hand-held part is overlapped with 1 axis of funnel；Institute
The metal hose 3 stated is that cross section is round, and 2 bottom surface of hand-held part is arranged in the metal hose 3；Described
The "-" type spiral shell edge of a knife 4 is flat cuboid structure, and top surface is provided with chamfering；4 bottom surface of the "-" type spiral shell edge of a knife with it is described
1 top surface edge of funnel connection, and the two by welding manner connection；4 plane of symmetry of the "-" type spiral shell edge of a knife with it is described
Funnel 1 radius where co-planar.
2 axis of hand-held part and 3 axis of metal hose are tangent in the two junction, so that total is more
Have integrality and continuity.
3 outer diameter of metal hose is identical as 2 outer diameter of hand-held part, reduces the on-way resistance drawn game of lubricating oil flowing
Portion's resistance.
3 internal diameter of metal hose is identical as 2 internal diameter of hand-held part, reduces the on-way resistance drawn game of lubricating oil flowing
Portion's resistance.
3 length of metal hose is greater than 2 length of hand-held part, and the needs of metal hose 3, which protrude into, to be started
Machine oil tank, therefore length is longer.
2 length of hand-held part is less than 1 length of funnel, and the hand-held part 2 is only used for the hand of staff
Work is held, therefore length is without too long.
4 width of the "-" type spiral shell edge of a knife is less than the 1 top surface edge width of funnel, so that the "-" type spiral shell
The edge of a knife 4 is fully mounted at the 1 top surface edge of funnel, prevents stress concentration.
In use, the "-" type spiral shell edge of a knife 4 of the user by the 1 top surface edge of funnel, it may be convenient to open
Open aircraft lubricating oil tank；Then, user one holds the hand-held part 2, and lubricating oil is poured into the funnel with lubricating oil tank on the other hand
1, and in advance according to operating space, the metal hose 3 is regulated into position alignment motor oil case, prevents oil spilling.
In conclusion the beneficial effects of the utility model are, person can be used to read and divide by mobile phone for the utility model
Turnning circle is enjoyed, is given full play to using enthusiasm；Turnning circle can also be judged by light simultaneously, facilitate match or carry out it
He interacts.
The above is only the preferred embodiment of the present invention, and therefore it does not limit the scope of the patent of the utility model,
Any equivalent structural transformation made using the contents of the description of this utility model is directly or indirectly related with other are attached to
The technical field of product, is also included in the patent protection scope of the utility model.
Claims (7)
1. a kind of adjustable hose lubricating oil oiling tooling of aircraft engine, it is characterised in that: soft including funnel, hand-held part, metal
Pipe and the "-" type spiral shell edge of a knife；The funnel is metal funnel-shaped structure；The funnel top surface diameter is greater than the funnel
Basal diameter；The hand-held part is round hard tube；The hand-held part top surface is connect with the funnel bottom surface, and the two
It is structure as a whole；The hand-held part axis is overlapped with the funnel axis；The metal hose is that cross section is circle,
And the hand-held part bottom surface is arranged in the metal hose；The "-" type spiral shell edge of a knife is flat cuboid structure, and
And top surface is provided with chamfering；The "-" type spiral shell edge of a knife bottom surface is connect with the funnel top surface edge, and the two passes through
Welding manner connection；Co-planar where the "-" type spiral shell edge of a knife plane of symmetry and the funnel radius.
2. a kind of adjustable hose lubricating oil oiling tooling of aircraft engine according to claim 1, it is characterised in that: described
Hand-held part axis and the metal hose axis it is tangent in the two junction.
3. a kind of adjustable hose lubricating oil oiling tooling of aircraft engine according to claim 1, it is characterised in that: described
Metal hose outer diameter it is identical as the hand-held part outer diameter.
4. a kind of adjustable hose lubricating oil oiling tooling of aircraft engine according to claim 1, it is characterised in that: described
Metal hose internal diameter it is identical as the hand-held part internal diameter.
5. a kind of adjustable hose lubricating oil oiling tooling of aircraft engine according to claim 1, it is characterised in that: described
Metal hose length be greater than the hand-held part length.
6. a kind of adjustable hose lubricating oil oiling tooling of aircraft engine according to claim 1, it is characterised in that: described
Hand-held part length be less than the funnel length.
7. a kind of adjustable hose lubricating oil oiling tooling of aircraft engine according to claim 1, it is characterised in that: described
"-" type spiral shell edge of a knife width be less than the funnel top surface edge width.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820847219.9U CN208516937U (en) | 2018-06-03 | 2018-06-03 | A kind of adjustable hose lubricating oil oiling tooling of aircraft engine |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820847219.9U CN208516937U (en) | 2018-06-03 | 2018-06-03 | A kind of adjustable hose lubricating oil oiling tooling of aircraft engine |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN208516937U true CN208516937U (en) | 2019-02-19 |
Family
ID=65339963
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201820847219.9U Expired - Fee Related CN208516937U (en) | 2018-06-03 | 2018-06-03 | A kind of adjustable hose lubricating oil oiling tooling of aircraft engine |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN208516937U (en) |
-
2018
- 2018-06-03 CN CN201820847219.9U patent/CN208516937U/en not_active Expired - Fee Related
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20190219 Termination date: 20190603 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |