Tool for discharging airplane fuel oil sediment

Abstract

The utility model relates to the technical field of aircraft fuel oil discharge, in particular to a tool for discharging aircraft fuel oil sediment, which comprises a vertical pipe and a collecting bottle, the inner wall of the bottom of the vertical pipe is connected with an adjusting pipe in a sliding mode, the outer wall of one side of the bottom of the vertical pipe is provided with a limiting hole, and the inner wall of the limiting hole is connected with a locking knob through threads. The outer wall of the top end of the vertical pipe is sleeved with a sleeve, the outer wall of the top end of the sleeve is fixedly connected with a conical pipe, and the outer wall of the top end of the conical pipe is fixedly connected with a collecting pipe. Fuel oil sediments can be conveniently collected through the conical collecting pipe, the supporting protrusions can be conveniently aligned with a drainage or door through the transparent silica gel material, the vertical pipe and the adjusting pipe are both hollow and matched with the collecting pipe so that the fuel oil sediments can be conveniently collected, and the collecting bottle is directly connected to the bottom of the adjusting pipe through threads, so that the fuel oil sediments can be conveniently collected. Collected fuel oil sediments directly enter the collecting bottle and are prevented from splashing and dripping on the ground, and the discharging efficiency of the fuel oil sediments of the airplane is improved.

Description

Technical Field

[0001] The utility model relates to the technical field of aircraft fuel discharge, in particular to a tool for discharging aircraft fuel sediment. Background Art

[0002] Fuel sediment will be produced in the fuel tank of the aircraft. The main component of fuel sediment is water. Water enters the fuel tank through impurities in the fuel and condensation of moist air. Water is deposited in the fuel tank, causing microorganisms to grow, which will cause microbial corrosion in the fuel tank and damage the fuel tank structure. Because the density of water is greater than that of fuel, water will be deposited at the lowest point of the fuel tank, so the fuel tank drain valve is installed on the lower surface of the wing, corresponding to the lowest point of each fuel tank.

[0003] A Chinese patent with publication number CN207809811U was searched and disclosed, which is a tool for discharging aircraft fuel sediment. The length of the extension tube can be flexibly adjusted according to the height of the aircraft fuel tank; a support frame is used to fix the bottom of the extension tube to the ground, so that one operator can complete the work of discharging aircraft fuel sediment, which greatly facilitates the operation; a rain shield is provided at the bottom end of the extension tube, which can protect the oil bottle mouth that receives the fuel sediment to prevent rainwater from entering and affecting the next step of analyzing the fuel sediment.

[0004] Based on the above search and combined with the prior art, it is found that the above patent has certain defects. The drain valve is opened by the top of the top head, and the fuel sediment is collected in conjunction with the adsorption section. However, the line of sight is easily blocked by the adsorption section during the alignment of the top head and the drain valve, which makes it difficult to align with the drain valve, and the structural connectivity is poor. The shape of the adsorption section is not convenient for collecting fuel sediment, which reduces the discharge efficiency of aircraft fuel sediment. Utility Model Content

[0005] The utility model aims to provide a tool for discharging aircraft fuel sediments to solve the problems raised in the above-mentioned background technology.

[0006] The technical solution of the utility model is: a tool for discharging aircraft fuel sediment, comprising a stand pipe and a collecting bottle, the bottom inner wall of the stand pipe is slidably connected with an adjusting tube, one side outer wall of the bottom of the stand pipe is provided with a limiting hole, the inner wall of the limiting hole is threadedly connected with a locking knob, a sleeve is sleeved on the top outer wall of the stand pipe, a conical tube is fixedly connected to the top outer wall of the sleeve, a collecting tube is fixedly connected to the top outer wall of the conical tube, a fixing rod is fixedly connected to the inner wall of the conical tube, a supporting rod is fixedly connected to the outer wall of the fixing rod, a supporting protrusion is arranged on the top outer wall of the supporting rod, a threaded connecting pipe is fixedly connected to the bottom outer wall of the adjusting tube, a connecting pipe is fixedly connected to the top outer wall of the collecting bottle, a threaded groove is arranged on the inner wall of the connecting pipe, and the threaded groove is matched with the size of the threaded connecting pipe.

[0007] Preferably, the collecting tube is arranged in a conical shape, the collecting tube is made of silica gel, and the size of the collecting tube is adapted to the size of the supporting protrusion.

[0008] Preferably, the outer wall of the top end of the support rod is provided with an inclined surface, the inclined surface is adapted to the size of the support protrusion, and the inner wall of the sleeve is provided with a sealing gasket.

[0009] Preferably, the outer wall of the adjusting tube is provided with scale marks, the adjusting tube is adapted to the size of the vertical tube, and the supporting rod is located directly above the sleeve.

[0010] Preferably, an anti-slip sleeve is fixedly connected to the outer wall of the adjusting tube, and a plurality of anti-slip protrusions are arranged on the outer wall of the anti-slip sleeve, and the anti-slip protrusions are distributed in a ring array.

[0011] The utility model provides a tool for discharging aircraft fuel sediment through improvement, which has the following improvements and advantages compared with the prior art:

[0012] First, the utility model is provided with a collecting pipe, a fixing rod, a vertical pipe, a supporting rod, an adjusting pipe and a collecting bottle. The vertical pipe is pushed upward, and the collecting pipe at the top of the conical pipe wraps the drainage valve. The supporting rod on the fixing rod cooperates with the supporting protrusion to insert into the drainage valve of the aircraft. After the drainage valve is lifted up, the fuel sediment falls into the conical pipe and the collecting pipe, and enters the collecting bottle along the vertical pipe and the adjusting pipe to be directly collected. The collecting pipe arranged in a conical shape is convenient for collecting the fuel sediment, and the transparent silicone material is also convenient for aligning the supporting protrusion with the drainage or door. The vertical pipe and the adjusting pipe are both hollow, and the collecting pipe is convenient for collecting the fuel sediment, and the collecting bottle is directly connected to the bottom of the adjusting pipe by a thread, and the collected fuel sediment directly enters the collecting bottle to prevent splashing and dripping on the ground, thereby improving the discharge efficiency of the aircraft fuel sediment;

[0013] Second, the utility model is provided with a stand pipe, an adjusting pipe and a locking knob, so that the length can be adjusted according to the height of different staff or aircraft drainage valves. The adjusting pipe slides inside the stand pipe and is fixed by the locking knob. The application range is wider, and the practicality of the fuel sediment discharge tool is improved.

[0014] Thirdly, the utility model is provided with threaded connecting pipes, sleeves, connecting pipes, risers and adjusting pipes, and the structures are assembled by means of knotting or threaded connection, which can also be conveniently disassembled into separate parts, thus reducing the maintenance and replacement costs. Moreover, after disassembly, it is more convenient to carry and transport, thus improving the convenience of the fuel sediment discharge tool. BRIEF DESCRIPTION OF THE DRAWINGS

[0015] The utility model is further explained below in conjunction with the accompanying drawings and embodiments:

[0016] Figure 1 It is a schematic diagram of the overall structure of the utility model;

[0017] Figure 2 It is an exploded schematic diagram of the casing connection structure of the utility model;

[0018] Figure 3 It is an exploded schematic diagram of the riser connection structure of the utility model;

[0019] Figure 4 It is an exploded schematic diagram of the regulating pipe connection structure of the utility model.

[0020] Description of reference numerals:

[0021] 1. Vertical pipe; 2. Conical pipe; 3. Collecting pipe; 4. Support protrusion; 5. Locking knob; 6. Adjusting pipe; 7. Collecting bottle; 8. Support rod; 9. Fixing rod; 10. Sleeve; 11. Anti-slip sleeve; 12. Anti-slip protrusion; 13. Threaded pipe; 14. Inclined surface; 15. Connecting pipe. DETAILED DESCRIPTION

[0022] The utility model is described in detail below, and the technical solutions in the embodiments of the utility model are clearly and completely described. Obviously, the described embodiments are only part of the embodiments of the utility model, not all of the embodiments. Based on the embodiments of the utility model, all other embodiments obtained by ordinary technicians in this field without creative work are within the scope of protection of the utility model.

[0023] The utility model provides a tool for discharging aircraft fuel sediment through improvement. The technical solution of the utility model is:

[0024] like Figure 1-Figure 4As shown, a tool for discharging aircraft fuel sediment comprises a stand pipe 1 and a collecting bottle 7, wherein an adjusting tube 6 is slidably connected to the inner wall of the bottom of the stand pipe 1, a limiting hole is provided on the outer wall of one side of the bottom of the stand pipe 1, a locking knob 5 is threadedly connected to the inner wall of the limiting hole, a sleeve 10 is sleeved on the outer wall of the top end of the stand pipe 1, a conical tube 2 is fixedly connected to the outer wall of the top end of the sleeve 10, a collecting tube 3 is fixedly connected to the outer wall of the top end of the conical tube 2, a fixing rod 9 is fixedly connected to the inner wall of the conical tube 2, a supporting rod 8 is fixedly connected to the outer wall of the fixing rod 9, a supporting protrusion 4 is provided on the outer wall of the top end of the supporting rod 8, a threaded connecting tube 13 is fixedly connected to the outer wall of the bottom end of the adjusting tube 6, a connecting tube 15 is fixedly connected to the outer wall of the top end of the collecting bottle 7, a threaded groove is provided on the inner wall of the connecting tube 15, and the threaded groove is matched with the size of the threaded connecting tube 13.

[0025] Furthermore, the collecting tube 3 is arranged in a conical shape and is made of silicone. The collecting tube 3 is adapted to the size of the supporting protrusion 4. The top outer wall of the support rod 8 is provided with a slope 14, and the slope 14 is adapted to the size of the supporting protrusion 4. The inner wall of the sleeve 10 is provided with a sealing gasket. The collecting tube 3 made of transparent silicone material is convenient for observation and alignment.

[0026] Furthermore, the outer wall of the adjusting tube 6 is provided with scale marks, the adjusting tube 6 is adapted to the size of the vertical tube 1, the support rod 8 is located directly above the sleeve 10, the outer wall of the adjusting tube 6 is fixedly connected with an anti-slip sleeve 11, and the outer wall of the anti-slip sleeve 11 is provided with a plurality of anti-slip protrusions 12, which are distributed in a circular array to increase the friction of the palm and prevent falling off.

[0027] Working principle: When collecting the discharge of aircraft fuel sediment, push the standpipe 1 upwards, the collection tube 3 at the top of the conical tube 2 wraps the drainage valve, and the support rod 8 on the fixed rod 9 cooperates with the support protrusion 4 to insert it into the aircraft's drainage valve. The collection tube 3 made of transparent silicone material is convenient for observation and alignment. After the drainage valve is lifted, the fuel sediment falls into the conical tube 2 and the collection tube 3, and enters the collection bottle 7 along the standpipe 1 and the adjustment tube 6 to be directly collected. When the length needs to be adjusted according to different usage scenarios or user needs, pull the adjustment tube to adjust the length. The joint tube 6 slides in the standpipe 1 to adjust the overall length, and then the structure is limited by the locking knob 5. The collecting tube 3 is set in a cone shape to facilitate the collection of fuel sediment. An anti-slip sleeve 11 and an anti-slip protrusion 12 are set on the outer wall of the adjusting tube 6 to increase the friction with the palm to prevent it from falling off. The conical tube 2 is connected to the standpipe 1 through the sleeve 10. The standpipe 1 and the adjusting tube 6 are detachable. The collecting bottle 7 is connected to the threaded pipe 13 at the bottom of the adjusting tube 6 through the connecting tube 15, which is also convenient for disassembly. The maintenance cost is lower and it is convenient to disassemble and assemble, and it is easy to carry and move.

[0028] The technical means disclosed in the utility model are not limited to the technical means disclosed in the above technical means, but also include technical solutions composed of equivalent replacement of the above technical features. Matters not covered in the utility model belong to the common knowledge of those skilled in the art.

Claims

1. A tool for discharging aircraft fuel sediment, comprising a standpipe (1) and a collecting bottle (7), characterized in that: The bottom inner wall of the stand pipe (1) is slidably connected with an adjusting tube (6); a limiting hole is provided on one side outer wall of the bottom of the stand pipe (1); a locking knob (5) is threadedly connected to the inner wall of the limiting hole; a sleeve (10) is sleeved on the top outer wall of the stand pipe (1); a conical tube (2) is fixedly connected to the top outer wall of the sleeve (10); a collecting tube (3) is fixedly connected to the top outer wall of the conical tube (2); a fixing rod (9) is fixedly connected to the inner wall of the conical tube (2); a supporting rod (8) is fixedly connected to the outer wall of the fixing rod (9); a supporting protrusion (4) is provided on the top outer wall of the supporting rod (8); a threaded connecting tube (13) is fixedly connected to the bottom outer wall of the adjusting tube (6); a connecting tube (15) is fixedly connected to the top outer wall of the collecting bottle (7); a threaded groove is provided on the inner wall of the connecting tube (15); and the threaded groove is matched with the size of the threaded connecting tube (13).

2. A tool for discharging aircraft fuel sediment according to claim 1, characterized in that: The collecting tube (3) is arranged in a conical shape, the collecting tube (3) is made of silica gel, and the size of the collecting tube (3) is adapted to that of the supporting protrusion (4).

3. A tool for discharging aircraft fuel sediment according to claim 1, characterized in that: The outer wall of the top end of the support rod (8) is provided with an inclined surface (14), the inclined surface (14) is adapted to the size of the support protrusion (4), and the inner wall of the sleeve (10) is provided with a sealing gasket.

4. A tool for discharging aircraft fuel sediment according to claim 1, characterized in that: The outer wall of the adjusting tube (6) is provided with scale marks, the adjusting tube (6) is adapted to the size of the standpipe (1), and the supporting rod (8) is located directly above the sleeve (10).

5. A tool for discharging aircraft fuel sediment according to claim 1, characterized in that: The outer wall of the regulating tube (6) is fixedly connected with an anti-slip sleeve (11), and the outer wall of the anti-slip sleeve (11) is provided with a plurality of anti-slip protrusions (12), and the anti-slip protrusions (12) are distributed in a ring array.

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