CN216070575U - Aircraft fuel oil drain device - Google Patents
Aircraft fuel oil drain device Download PDFInfo
- Publication number
- CN216070575U CN216070575U CN202122955955.0U CN202122955955U CN216070575U CN 216070575 U CN216070575 U CN 216070575U CN 202122955955 U CN202122955955 U CN 202122955955U CN 216070575 U CN216070575 U CN 216070575U
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- funnel
- fuel oil
- aircraft fuel
- connecting rod
- oil drain
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Abstract
The utility model discloses an aircraft fuel oil discharging device, which comprises a storage box and a bracket base, wherein the storage box is arranged on the bracket base, a connecting rod is vertically arranged on the bracket base, a telescopic rod is arranged in the connecting rod, the connecting rod is connected with the telescopic rod through a bolt, a threaded hole matched with the bolt is formed in the telescopic rod, a funnel is arranged at one end of the telescopic rod, a rubber sleeve is arranged on the funnel, and an oil discharging hose is arranged at a conduit at the lower end of the funnel. The risk of fuel leakage and deflagration that personnel lead to has been avoided, realizes convenient fuel release work.
Description
Technical Field
The utility model relates to the technical field of oil drainage devices, in particular to an aircraft fuel oil drainage device.
Background
According to the maintenance technical requirements, fuel oil release work needs to be carried out after the performance of the aircraft entering a factory is checked, so that the disassembly and inspection work can be carried out safely at a later stage. The traditional oil drainage mode is as follows: an oil discharge gun is adopted, the funnel opening is aligned to the oil discharge nozzle, the lower end of the oil gun is aligned to the oil drum, and the oil gun is held by hands until fuel oil is completely discharged. This oil drain mode is owing to adopt the handheld oil drain of manpower at the oil drain in-process, and the personnel of having had of a specified duration control the difficulty, the condition that the fuel leaked often can appear, simultaneously, the oil gun often uses the iron sheet to make, and aircraft coating also can be damaged to sharp-pointed edges and corners, owing to lack electrostatic protection during the oil drain, human static also probably arouses deflagration when the fuel releases, brings serious aviation incident.
SUMMERY OF THE UTILITY MODEL
The utility model aims to overcome one or more defects in the prior art and provide an aircraft fuel oil discharging device.
The purpose of the utility model is realized by the following technical scheme: the utility model provides an aircraft fuel oil drain device, includes containing box and support base, the containing box sets up on the support base, the vertical connecting rod that is provided with on the support base, be provided with the telescopic link in the connecting rod, through bolted connection between connecting rod and the telescopic link, be provided with a plurality of screw holes that match with the bolt on the telescopic link, the telescopic link upper end is provided with the funnel, be provided with the rubber sleeve on the funnel, the pipe department of funnel lower extreme is provided with the oil drain hose.
According to the utility model, the storage box is provided with the handrail, and the arrangement of the corresponding handrail can make the fuel oil discharging device more convenient to move.
According to the utility model, the lower end of the containing box is provided with a plurality of rollers, and the fuel oil discharging device can be conveniently moved by arranging the plurality of rollers.
Optionally, the bracket base is detachably provided with the static releaser, and the static releaser is used for eliminating static electricity and preventing fuel oil from deflagration.
Optionally, the roller is a universal wheel with a brake, and the roller can stop rolling at an ideal position by arranging the universal wheel with the brake, so that the stability of the fuel oil discharging device is guaranteed.
The utility model has the beneficial effects that:
1. the utility model reduces the working intensity of personnel, improves the maintenance working efficiency, improves the safety and the convenience of fuel oil release, avoids the fuel oil leakage and deflagration risks caused by personnel, is suitable for all upper single-wing navigation airplanes, and realizes the convenient fuel oil release work
2. The utility model is provided with the static releaser which is used for eliminating the static electricity of the human body and avoiding the combustion of fuel oil caused by the static electricity.
Drawings
FIG. 1 is a schematic view of the structure of the present invention.
In the figure: 1. a storage box; 2. a connecting rod; 3. a telescopic rod; 4. a funnel; 5. a rubber sleeve; 6. an oil drain hose; 7. a handrail; 8. a roller; 9. an electrostatic discharger; 10. a bracket base.
Detailed Description
The technical solutions of the present invention will be described clearly and completely with reference to the following embodiments, and it should be understood that the described embodiments are only a part of the embodiments of the present invention, and not all of the embodiments. All other embodiments, which can be obtained by a person skilled in the art without inventive effort based on the embodiments of the present invention, are within the scope of the present invention.
Referring to fig. 1, the embodiment provides an aircraft fuel oil discharging device, which comprises a storage box 1 and a support base 10, wherein the storage box 1 is arranged on the support base 10, a connecting rod 2 is vertically arranged on the support base 10, a telescopic rod 3 is arranged in the connecting rod 2, the telescopic rod 3 is slidably mounted in the connecting rod 2, the connecting rod 2 and the telescopic rod 3 are connected through a bolt, a plurality of threaded holes matched with the bolt are formed in the telescopic rod 3, a funnel 4 is arranged at the upper end of the telescopic rod 3, a rubber sleeve 5 is arranged on the funnel 4, the funnel 4 can be tightly attached to an oil discharging opening of an aircraft oil storage box through the rubber sleeve 5, the fuel oil is prevented from leaking outwards, an oil discharging hose 6 is arranged at a conduit opening at the lower end of the funnel 4, the other end of the oil discharging hose 6 is communicated with the oil discharging box, and the oil discharging device is moved to the oil discharging opening below a wing when in use, not hard up the lock nut of telescopic link 3, adjust telescopic link 3 and make funnel 4 adjust well the fuel oil discharge opening, put into the oil drum with oil drain hose 6 simultaneously, after loosening wing discharge opening end cap, hug closely the discharge opening with the cover like funnel 4 of gum cover 5, the personnel can leave behind the locking telescopic link 3, treat the fuel oil and put in place after, resume to right in place telescopic link 3 etc. remove the oil drain device, set up the static electricity releaser 9 on support base 10 and can effectively eliminate human static.
Be provided with handrail 7 on the containing box 1, be provided with gyro wheel 8 on the support base 10, set up corresponding handrail 7 and gyro wheel 8 and make removal oil drain device convenient and fast.
The connecting rod 2 is connected with the telescopic rod 3 through a bolt, the structure is simple, and the lifting is convenient.
The gyro wheel 8 is the universal wheel of area brake, through setting up the universal wheel reinforcing oil drain device's of area brake stability.
The foregoing is illustrative of the preferred embodiments of this invention, and it is to be understood that the utility model is not limited to the precise form disclosed herein and that various other combinations, modifications, and environments may be resorted to, falling within the scope of the concept as disclosed herein, either as described above or as apparent to those skilled in the relevant art. And that modifications and variations may be effected by those skilled in the art without departing from the spirit and scope of the utility model as defined by the appended claims.
Claims (5)
1. The utility model provides an aircraft fuel oil jettison gear, includes containing box (1) and support base (10), its characterized in that, containing box (1) sets up on support base (10), vertically on support base (10) be provided with connecting rod (2), slidable mounting has telescopic link (3) in connecting rod (2), through bolted connection between connecting rod (2) and telescopic link (3), be provided with a plurality of screw holes that match with the bolt on telescopic link (3), telescopic link (3) upper end is provided with funnel (4), funnel (4) port demountable installation has rubber sleeve (5), the pipe department of funnel (4) lower extreme is provided with oil drain hose (6).
2. An aircraft fuel drain as claimed in claim 1, characterized in that the container (1) is provided with a handrail (7).
3. An aircraft fuel drain as claimed in claim 1, characterized in that the lower end of the container (1) is provided with a plurality of rollers (8).
4. An aircraft fuel oil drain device according to claim 1, characterized in that the bracket base (10) is detachably provided with the electrostatic discharger (9).
5. An aircraft fuel oil drain device according to claim 3, characterized in that the rollers (8) are provided with braked universal wheels.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN202122955955.0U CN216070575U (en) | 2021-11-29 | 2021-11-29 | Aircraft fuel oil drain device |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN202122955955.0U CN216070575U (en) | 2021-11-29 | 2021-11-29 | Aircraft fuel oil drain device |
Publications (1)
Publication Number | Publication Date |
---|---|
CN216070575U true CN216070575U (en) | 2022-03-18 |
Family
ID=80662312
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN202122955955.0U Active CN216070575U (en) | 2021-11-29 | 2021-11-29 | Aircraft fuel oil drain device |
Country Status (1)
Country | Link |
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CN (1) | CN216070575U (en) |
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2021
- 2021-11-29 CN CN202122955955.0U patent/CN216070575U/en active Active
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