CN2900358Y - Novel aviation oil discharging rod - Google Patents
Novel aviation oil discharging rod Download PDFInfo
- Publication number
- CN2900358Y CN2900358Y CNU200620034313XU CN200620034313U CN2900358Y CN 2900358 Y CN2900358 Y CN 2900358Y CN U200620034313X U CNU200620034313X U CN U200620034313XU CN 200620034313 U CN200620034313 U CN 200620034313U CN 2900358 Y CN2900358 Y CN 2900358Y
- Authority
- CN
- China
- Prior art keywords
- oil
- valve
- draining
- bar
- elasticity
- 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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- Loading And Unloading Of Fuel Tanks Or Ships (AREA)
Abstract
The utility model discloses a new aviation jettison bar, which comprises a click, a rubber cup, and a jettison pipe. The product is characterized in that: the click can be arranged on a click base connected with a jettison pipe; the upper part of the click is provided with a card hanger; the utility model adopts the click made of soft metal to avoid damages to the jettison groove; it is easy for workers to operate and replace the click. The click shape can be changed into a crossbeam, a cross, a heterotypic, and a hexagon according to the shape of the jettison groove mouth; the utility model can also exempt sinking oil and people or materials from pollution, thus realizing the double environmental protection; with simple structure, the product can be carried around easily, and adjust the length of the jettison bar with the telescopic mechanism according to the height of planes; when the rest oil is drained from the bottom, the utility model can hang the card hanger on the jettison groove mouth to drain oil for long time, relieving people of holding the jettison bar.
Description
Technical field
The utility model relates to the aviation machine field, particularly a kind of novel aviation of the pattern of draining the oil that breaks traditions bar of draining the oil.
Background technology
The existing aviation bar of draining the oil is the bar of draining the oil that a kind of type must corresponding a kind of specific model, and traditional top of draining the oil is hard metallic material, and is non-exchange and damage the wing notch of draining the oil easily.When the staff drains the oil in the course of the work the aircraft of each different model, the bar of draining the oil of different model must be changed and just oil-out work can be finished, the drain oil unit that all needs to carry in the lump a variety of models when therefore the staff uses at every turn at work, increase the difficulty and the loaded down with trivial details property of work like this to the staff, brought very big inconvenience.And in the process of draining the oil, the staff must head on the bar of draining the oil, and can not throw off the bar of draining the oil and prepare other work, and the leakproofness of the process of therefore draining the oil is entirely by manual control, and the entire work process imprecision pollutes easily and splashes.
Summary of the invention
Goal of the invention of the present utility model is to provide a kind of novel aviation bar of draining the oil, and can be used for the work of draining the oil of any type, and can overlap to hang on the notch of draining the oil and work closely voluntarily, can not pollute and splash.
The technical solution of the utility model is as follows:
A kind of novel aviation bar of draining the oil comprises top, rubber cup and oil drain tube, it is characterized in that: described top is detachable be installed in oil drain tube bonded assembly top headstock on; The top of described top is provided with the card lacing film.
The diameter that the width of described card lacing film equals to come directly towards, the length of card lacing film is greater than the diameter of top.
The lower end of described leather cup is provided with the elastic valve of band oil leaking hole; Described elastic valve comprises on the elasticity valve under the valve and elasticity, and leather cup is fixedly connected on the upper end of valve on the elasticity, and valve is actively socketed under the elasticity on the valve on the elasticity, and the inside of valve is provided with the spring that contacts with valve on the elasticity under the elasticity; Valve is captiveed joint with oil drain tube under the described elasticity.
Described top and top headstock adopt thread connecting mode, perhaps adopt card to insert connection mode.
Adopt screw thread to captive joint between described top headstock and the oil drain tube, perhaps adopt card to insert connection mode.
Described oil drain tube is provided with the telescoping mechanism of regulating duct length, the length that can regulate oil drain tube as required.
Top of the present utility model adopts soft metal (copper or aluminium) to make, when the staff uses the utility model, only need turn 90 degrees coming directly towards the notch of draining the oil of jacking gently, revolving then, at this moment block lacing film and just can overlap and hang on the notch of draining the oil, other work are prepared in staff's operation of can letting go simultaneously; Because the utility model is provided with elastic valve, when on the elasticity during the downward compression spring of valve, the top can easily be put the notch of draining the oil into; When card lacing film cover hangs on the notch of draining the oil, spring upwards pushes valve and rubber cup on the elasticity, therefore rubber cup can with the aircraft surfaces closed contact, can be soft and press close to notch in the top, precipitated oil also is not easy contaminated in the process of draining the oil and splashes, can not pollute simultaneously other object or staff because of splashing yet, just realize tight automatically function of locking the notch surface of draining the oil yet.Simultaneously, when a plurality of types are drained the oil, only need to change the top and just can easily realize.
Advantage of the present utility model is as follows:
The top that the utility model adopts soft metal to make is difficult for the notch of draining the oil is caused damage; Simple to operation when the staff uses, change the top also flexibly and fast, the top can be according to drain the oil notch shape and changing arbitrarily as a word, cross, abnormal shape, hexagon etc. of aircraft; The utility model can also be realized precipitated oil and all not contaminated double environmental protection of other people or thing; Outward appearance is simple and easy to carry, and simultaneously can regulate length so that terrain clearance that should type is drained the oil to the bar of draining the oil according to the height utilization telescoping mechanism of different aircrafts; Emit the bottom in the troubleshooting during excess oil, the required time of draining the oil is longer, can utilize the card lacing film that the utility model card is hung over aircraft and drain the oil on the notch, need not manually lifting the bar of draining the oil, and can carry out the long period and drain the oil.
Description of drawings
Fig. 1 is a main TV structure scheme drawing of the present utility model
Fig. 2 is a cross-sectional view of the present utility model
Fig. 3 is a plan structure scheme drawing of the present utility model
The specific embodiment
Embodiment 1
A kind of novel aviation bar of draining the oil comprises top 1, rubber cup 2 and oil drain tube 3, it is characterized in that: described top 1 is detachable be installed in oil drain tube 3 bonded assembly top headstocks 4 on; The top of described top 1 is provided with card lacing film 5.
The width of described card lacing film 5 equals to come directly towards 1 diameter, and the length of card lacing film 5 is greater than the diameter of top 1.
The lower end of described leather cup 2 is provided with the elastic valve of band oil leaking hole 6; Described elastic valve comprises on the elasticity valve 8 under the valve 7 and elasticity, and leather cup 2 is fixedly connected on the upper end of valve 7 on the elasticity, and valve 7 is actively socketed under the elasticity on the valve 8 on the elasticity, and the inside of valve 8 is provided with the spring 9 that contacts with valve 7 on the elasticity under the elasticity; Valve 8 is captiveed joint with oil drain tube 3 under the described elasticity.
Thread connecting mode is adopted with top headstock 4 in described top 1.
Adopt card to insert connection mode between described top headstock 4 and the oil drain tube 3.
Described oil drain tube 3 is provided with the telescoping mechanism of regulating duct length, the length that can regulate oil drain tube as required.
Top 1 of the present utility model adopts soft metal to make, as: copper, aluminium, very convenient replacing, and be not easy to damage the notch of draining the oil.When the airport employe uses the utility model, only need be with the top 1 jacking notch of draining the oil gently, revolve then and turn 90 degrees, card lacing film 5 just can overlap and hang on the notch of draining the oil, and the staff can let go and operate other work of preparing simultaneously; Because flexible valve, can make the surperficial closed contact of rubber cup 2 and aircraft, can realize the drain the oil function of notch surface of tight automatically lock, and the oil of precipitation can be not contaminated and splash yet, and can not pollute other object or staff simultaneously because of splashing yet.When a plurality of types are drained the oil, only need to change top 1 and just can easily realize; Described rubber cup 2 can be changed its size according to actual needs.
Embodiment 2
A kind of novel aviation bar of draining the oil, described top 1 adopts card to insert connection mode with top headstock 4.
Adopt screw thread to captive joint between described top headstock 4 and the oil drain tube 3.
Embodiment 3
A kind of novel aviation bar of draining the oil, thread connecting modes are adopted with top headstock 4 in described top 1.
Adopt screw thread to captive joint between described top headstock 4 and the oil drain tube 3.
Embodiment 4
A kind of novel aviation bar of draining the oil, described top 1 adopts card to insert connection mode with top headstock 4.
Adopt card to insert connection mode between described top headstock 4 and the oil drain tube 3.
Embodiment 5
The shape that described card lacing film 5 is rectangular, perhaps set as required.
Claims (6)
1, a kind of novel aviation bar of draining the oil, comprise top (1), rubber cup (2) and oil drain tube (3), it is characterized in that: described top (1) detachable be installed in oil drain tube (3) bonded assembly top headstock (4) on: the top of described top (1) is provided with card lacing film (5).
2, a kind of novel aviation according to claim 1 bar of draining the oil is characterized in that: the width of described card lacing film (5) equals the diameter of top (1), and the length of card lacing film (5) is greater than the diameter of top (1).
3, a kind of novel aviation according to claim 1 bar of draining the oil is characterized in that: the lower end of described leather cup (2) is provided with the elastic valve of band oil leaking hole (6); Described elastic valve comprises valve (8) under valve on the elasticity (7) and the elasticity, leather cup (2) is fixedly connected on the upper end of valve on the elasticity (7), valve on the elasticity (7) is actively socketed on the valve under the elasticity (8), and the inside of valve under the elasticity (8) is provided with the spring (9) that contacts with valve (7) on the elasticity; Valve under the described elasticity (8) is captiveed joint with oil drain tube (3).
4, a kind of novel aviation according to claim 1 bar of draining the oil is characterized in that: described top (1) adopts thread connecting mode with top headstock (4), perhaps adopts card to insert connection mode.
5, a kind of novel aviation according to claim 1 bar of draining the oil is characterized in that: adopt screw thread to captive joint between described top headstock (4) and the oil drain tube (3), perhaps adopt card to insert connection mode.
6, a kind of novel aviation according to claim 1 bar of draining the oil is characterized in that: described oil drain tube (3) is provided with the telescoping mechanism of regulating duct length.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CNU200620034313XU CN2900358Y (en) | 2006-05-25 | 2006-05-25 | Novel aviation oil discharging rod |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CNU200620034313XU CN2900358Y (en) | 2006-05-25 | 2006-05-25 | Novel aviation oil discharging rod |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN2900358Y true CN2900358Y (en) | 2007-05-16 |
Family
ID=38084521
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CNU200620034313XU Expired - Fee Related CN2900358Y (en) | 2006-05-25 | 2006-05-25 | Novel aviation oil discharging rod |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN2900358Y (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2013056625A1 (en) * | 2011-10-18 | 2013-04-25 | 中国商用飞机有限责任公司 | Telescopic tool for fuel oil precipitate discharge |
| CN111951382A (en) * | 2020-08-11 | 2020-11-17 | 哈尔滨理工大学 | Three-dimensional reconstruction information processing equipment based on deep learning |
| CN112112706A (en) * | 2020-09-29 | 2020-12-22 | 中国航发动力股份有限公司 | Oil drainage device and method for sealing valve |
-
2006
- 2006-05-25 CN CNU200620034313XU patent/CN2900358Y/en not_active Expired - Fee Related
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2013056625A1 (en) * | 2011-10-18 | 2013-04-25 | 中国商用飞机有限责任公司 | Telescopic tool for fuel oil precipitate discharge |
| CN111951382A (en) * | 2020-08-11 | 2020-11-17 | 哈尔滨理工大学 | Three-dimensional reconstruction information processing equipment based on deep learning |
| CN112112706A (en) * | 2020-09-29 | 2020-12-22 | 中国航发动力股份有限公司 | Oil drainage device and method for sealing valve |
| CN112112706B (en) * | 2020-09-29 | 2021-08-17 | 中国航发动力股份有限公司 | Oil drainage device and method for sealing valve |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| C41 | Transfer of patent application or patent right or utility model | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20100115 Address after: 17, No. two, South Ring Road, two, Sichuan, Chengdu Province, China: 610041 Patentee after: No.2 Inst, China Civil Aviation General Bureau Address before: 17, No. two, South Ring Road, two, Sichuan, Chengdu Province, China: 610041 Co-patentee before: Chen Yaoguang Patentee before: Second Research Institute of the Civil Aviation Administration of China |
|
| EE01 | Entry into force of recordation of patent licensing contract |
Assignee: Chengdu Newave Aerochemical Co., Ltd. Assignor: No.2 Inst, China Civil Aviation General Bureau|Chen Yaoguang Contract fulfillment period: 2009.10.20 to 2016.5.25 Contract record no.: 2009510000157 Denomination of utility model: Novel aviation oil discharging rod Granted publication date: 20070516 License type: Exclusive license Record date: 20091116 |
|
| LIC | Patent licence contract for exploitation submitted for record |
Free format text: EXCLUSIVE LICENSE; TIME LIMIT OF IMPLEMENTING CONTACT: 2009.10.20 TO 2016.5.25; CHANGE OF CONTRACT Name of requester: CHENGDU CIVIL AVIATON LIUWEI HANGHUA CO., LTD Effective date: 20091116 |
|
| C17 | Cessation of patent right | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20070516 Termination date: 20110525 |