Detection device for aviation fuel
By designing a split aircraft fuel detection device, using the design of the hooking connection and placement plate, the problem of cleaning difficulties after the inspection is completed is solved, and the operation efficiency and detection accuracy are improved.
Patent Information
- Application Number
- CN202421014361.7
- Authority / Receiving Office
- CN · China
- Patent Type
- Utility models(China)
- Current Assignee / Owner
- Filing Date
- 2024-05-11
- Publication Date
- 2025-02-28
- Estimated Expiration
- 2034-05-11
AI Technical Summary
After the inspection is completed, it is difficult for the existing aviation fuel detection device to clean the detection bottles easily, which affects the accuracy of subsequent inspections and the operational efficiency of staff.
A split detection device is designed, including the upper bottle body and the lower bottle body, which is easy to disassemble and assemble by snap-in connection, and a placement plate is set on the lower bottle body for placing water test paper. At the same time, cleaning tools can be placed in the lower bottle body to facilitate cleaning of the upper bottle body.
It realizes convenient disassembly and assembly and cleaning of the detection device, improves the operating efficiency of staff, and ensures the accuracy of subsequent inspections.
Smart Images

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Abstract
Description
Technical Field
[0001] The utility model relates to the technical field of aviation fuel detection, in particular to a detection device for aviation fuel. Background Art
[0002] Aviation fuel refers to some fuel varieties specially designed for aircraft. It is of higher quality than the fuel used in heating systems and cars, and usually contains different additives to reduce the risk of icing and explosion due to high temperature. Aviation kerosene has appropriate density, high calorific value, good combustion performance, can burn quickly, stably, continuously and completely, and has a small combustion area, less carbon deposits, and is not easy to coke; it has good low-temperature fluidity and can meet the requirements of oil fluidity in cold and low-temperature areas and high-altitude flights; it has good thermal stability and antioxidant stability and can meet the needs of supersonic high-altitude flights; it has high cleanliness, no mechanical impurities and harmful substances such as moisture, and low sulfur content, especially mercaptan sulfur content, and little corrosion to mechanical parts.
[0003] When water is mixed into aviation kerosene, its freezing point will increase. If the aircraft flies in cold weather for a long time, the water in the fuel will easily freeze into ice, causing the engine to interrupt or completely stop fuel supply, endangering flight safety.
[0004] Therefore, in order to ensure flight safety, aviation fuel is generally extracted for testing. When testing aviation fuel, existing test bottles only consider how to extract aviation fuel, but do not consider how to facilitate the staff to clean the test bottles after the test is completed to ensure that subsequent staff can use the test bottles to conduct aviation fuel testing again without affecting the accuracy of the test. Utility Model Content
[0005] The utility model aims to provide an aviation fuel detection device, which adopts a split design of a detection bottle, so that it is divided into an upper bottle body and a lower bottle body, the upper bottle body and the lower bottle body are connected by snap-fitting, which is convenient for workers to install, and a placement plate for placing water test paper is arranged at the upper port of the lower bottle body, which not only makes it convenient for workers to put the water test paper into the detection bottle for aviation fuel detection, but also makes it convenient for workers to clean the upper bottle body.
[0006] In order to solve the above technical problems, the utility model adopts the following solutions:
[0007] A detection device for aviation fuel comprises a detection bottle, which is composed of an upper bottle body and a lower bottle body that are clamped together. A discharge port is arranged at one end of the top of the upper bottle body, and an oil inlet pipe is installed at the other end of the top of the upper bottle body. At least one clamping protrusion is embedded in the lower port of the upper bottle body, and an annular clamping piece that is mutually clamped with the clamping protrusion is embedded in the upper port of the lower bottle body. An annular clamping piece is provided on the outer side wall of the annular clamping piece corresponding to the clamping protrusion, and a clamping protrusion is embedded in the annular clamping groove. A placement plate is provided on the inner side wall of the annular clamping piece, and the placement plate is used to place a water test paper. A bottom cover is provided at the lower end of the lower bottle body, and a cleaning tool can be placed in the lower bottle body.
[0008] Furthermore, the placement plate is symmetrically provided with fixing blocks, the fixing blocks are provided with through holes, both ends of the through holes are respectively facing the inner side walls of the annular clamping member, and the through holes are used to limit the position of the water test paper.
[0009] Furthermore, the upper end of the annular clamp extends toward the upper bottle body, and the outer side wall of the lower end of the annular clamp is connected to the upper port of the lower bottle body. When the clamping protrusion is located in the annular clamping groove, the inner side wall of the upper bottle body is fitted and connected to the plane where the notch of the annular groove is located.
[0010] Furthermore, the annular groove is provided with an inlet end and an outlet end, the inlet end extends to the upper end of the annular clamping piece and is located below the corresponding clamping protrusion, the outlet end extends to the lower end of the annular clamping piece and is connected to the upper bottle body, a limiting protrusion is convexly provided in the annular groove, and the limiting protrusion is located at the outlet end of the annular groove, when the clamping protrusion is located in the annular groove and conflicts with the limiting protrusion, the lower port of the upper bottle body is fitly connected with the upper port of the lower bottle body.
[0011] Furthermore, the upper end surface of the limiting protrusion is lower than the plane where the notch of the annular groove is located.
[0012] Furthermore, a pressing assembly is provided in the oil inlet pipe, and the pressing assembly includes a mounting rod, a connecting rod is slidably inserted and connected to the top of the mounting rod, a baffle is installed at the bottom of the connecting rod, and a movable plate is installed at the top of the connecting rod.
[0013] Furthermore, the upper bottle body and the oil inlet pipe are both provided with interconnected through holes, the bottom of the connecting rod extends to the interior of the upper bottle body through the through hole, and the top of the baffle is in contact with the inner wall of the upper bottle body.
[0014] Furthermore, a spring is sleeved on the outer side of the connecting rod, the bottom of the spring is connected to the top of the mounting rod, and the top of the spring is connected to the bottom of the moving plate.
[0015] Beneficial effects of the utility model:
[0016] The utility model provides an aviation fuel detection device, which adopts a split design of a detection bottle, so that it is divided into an upper bottle body and a lower bottle body. The upper bottle body and the lower bottle body are connected by snapping, which is easy to operate and convenient for staff to disassemble and assemble.
[0017] In addition, a placement plate for placing water test paper is arranged at the upper port of the lower bottle body, which not only makes it convenient for the staff to put the water test paper into the test bottle for aviation fuel testing, but also makes it convenient for the staff to clean the upper bottle body. BRIEF DESCRIPTION OF THE DRAWINGS
[0018] Figure 1 This is a schematic cross-sectional view of the detection bottle in Example 1 of the utility model;
[0019] Figure 2 This is a front view structural diagram of the detection bottle in Example 1 of the utility model;
[0020] Figure 3 This is a schematic diagram of the structure of the placement plate in Example 1 of the utility model;
[0021] Figure 4 This is a cross-sectional structural diagram of a pressing assembly provided in the oil inlet pipe in Embodiment 2 of the utility model;
[0022] Explanation of the accompanying drawings: 1-upper bottle body, 11-bottom cover, 2-lower bottle body, 3-clamping protrusion, 4-annular clamping piece, 41-annular clamping groove, 42-limiting protrusion, 5-placing plate, 6-fixing block, 7-oil inlet pipe, 8-pressing assembly, 81-mounting rod, 82-connecting rod, 83-baffle, 84-movable plate, 85-spring, 9-discharge port, 10-filter layer. DETAILED DESCRIPTION
[0023] In order to enable those skilled in the art to better understand the technical solution of the present invention, the present invention is further described in detail below in conjunction with the accompanying drawings and specific implementation methods, but the implementation methods of the present invention are not limited thereto.
[0024] In the description of the present utility model, it should be noted that the terms "center", "up", "down", "left", "right", "vertical", "longitudinal", "lateral", "horizontal", "inside", "outside", "front", "back", "top", "bottom", etc. indicate directions or positional relationships based on the directions or positional relationships shown in the accompanying drawings, or are the directions or positional relationships in which the utility model product is usually placed when in use. They are only for the convenience of describing the present utility model and simplifying the description, and do not indicate or imply that the device or element referred to must have a specific direction, be constructed and operated in a specific direction, and therefore cannot be understood as a limitation on the present utility model.
[0025] In the description of the present invention, it is also necessary to explain that, unless otherwise clearly specified and limited, the terms "set", "open", "installed", "connected", and "connected" should be understood in a broad sense, for example, it can be a fixed connection, a detachable connection, or an integral connection; it can be a mechanical connection or an electrical connection; it can be a direct connection, or it can be indirectly connected through an intermediate medium, or it can be the internal communication of two components. For ordinary technicians in this field, the specific meanings of the above terms in the present invention can be understood according to specific circumstances.
[0026] The present invention is described in detail below with reference to the accompanying drawings and in combination with embodiments:
[0027] Example 1
[0028] At present, when testing aviation fuel, the existing test bottles only consider how to extract aviation fuel, but do not consider how to facilitate the staff to clean the test bottles after the test is completed to ensure that subsequent staff can use the test bottles to conduct aviation fuel testing again without affecting the accuracy of the test.
[0029] Therefore, the utility model provides an aviation fuel detection device, which adopts a split design of the detection bottle, so that it is divided into an upper bottle body 1 and a lower bottle body 2. The upper bottle body 1 and the lower bottle body 2 are connected by snap-fitting, which is convenient for workers to install. In addition, a placement plate 5 for placing a water test paper is arranged at the upper port of the lower bottle body 2, which not only makes it convenient for workers to put the water test paper into the detection bottle for aviation fuel detection, but also makes it convenient for workers to clean the upper bottle body 1.
[0030] Specifically, Figure 1 , Figure 2 , Figure 3As shown, a detection device for aviation fuel includes a detection bottle, which is composed of an upper bottle body 1 and a lower bottle body 2 that are clamped together. A discharge port 9 is provided at one end of the top of the upper bottle body 1, and an oil inlet pipe 7 is installed at the other end of the top of the upper bottle body 1. At least one clamping protrusion 3 is embedded in the lower port of the upper bottle body 1, and an annular clamping piece 4 that is mutually clamped with the clamping protrusion 3 is embedded in the upper port of the lower bottle body 2. The outer side wall of the annular clamping piece 4 is provided with an annular clamping groove 41 corresponding to the clamping protrusion 3, and the clamping protrusion 3 is embedded in the annular clamping groove 41. The inner side wall of the annular clamping piece 4 is provided with a placement plate 5, and the placement plate 5 is used to place a water test paper. The lower end of the lower bottle body 2 is provided with a bottom cover 11, and a cleaning tool can be placed in the lower bottle body 2. The purpose is that when the staff disassembles the test bottle into the upper bottle body 1 and the lower bottle body 2 by rotating, not only can the water test paper be fixed or taken out through the placement plate 5 set on the lower bottle body 2, but the bottom cover 11 of the lower bottle body 2 can also be opened, and a placement space is set in the lower bottle body 2 to accommodate cleaning tools, so that the staff can take out the cleaning tools to clean the inside of the upper bottle body 1, which is convenient for the next detection work.
[0031] Preferably, the placement plate 5 is symmetrically provided with a fixing block 6, the fixing block 6 is provided with a through hole, the two ends of the through hole are respectively facing the inner wall of the annular clamping member 4, and the through hole is used to limit the position of the water test paper. The purpose is to fix the position of the water test paper so that the water test paper is kept on the placement plate 5.
[0032] Preferably, the upper end of the annular clamping member 4 extends toward the upper bottle body 1, and the outer side wall of the lower end of the annular clamping member 4 is connected to the upper port of the lower bottle body 2. When the clamping protrusion 3 is located in the annular clamping groove 41, the inner side wall of the upper bottle body 1 is fitted and connected to the plane where the notch of the annular groove is located.
[0033] Preferably, the annular groove 41 is provided with an inlet end and an outlet end, the inlet end extends to the upper end of the annular clamping piece 4 and is located below the corresponding clamping protrusion 3, the outlet end extends to the lower end of the annular clamping piece 4 and is connected to the upper bottle body 1, a limiting protrusion 42 is convexly provided in the annular groove 41, and the limiting protrusion 42 is located at the outlet end of the annular groove 41, when the clamping protrusion 3 is located in the annular groove 41 and conflicts with the limiting protrusion 42, the lower port of the upper bottle body 1 is fitly connected with the upper port of the lower bottle body 2.
[0034] Preferably, the upper end surface of the limiting protrusion 42 is lower than the plane where the notch of the annular groove 41 is located.
[0035] Specifically, in this embodiment, the detection bottle is designed to be split into an upper bottle body 1 and a lower bottle body 2. The upper bottle body 1 and the lower bottle body 2 are connected by snapping, which is easy to operate and convenient for staff to disassemble and assemble. In addition, through disassembly and assembly, it is convenient for staff to place the water test paper into the detection bottle to perform fuel testing, and can also clean the upper bottle body 1.
[0036] Example 2
[0037] Based on the embodiment 1, in the embodiment 2, in order to prevent the fuel in the upper bottle body 1 from being contaminated, a sealing plug is provided at the top of the fuel inlet pipe 7, and a pressing assembly 8 is provided in the fuel inlet pipe 7. Figure 4 As shown, the pressing assembly 8 includes a mounting rod 81 , a connecting rod 82 is slidably inserted and connected to the top of the mounting rod 81 , a baffle 83 is installed at the bottom of the connecting rod 82 , and a moving plate 84 is installed at the top of the connecting rod 82 .
[0038] Preferably, the upper bottle body 1 and the oil inlet pipe 7 are both provided with interconnected through holes, the bottom of the connecting rod 82 extends to the interior of the upper bottle body 1 through the through hole, and the top of the baffle 83 fits with the inner wall of the upper bottle body 1 .
[0039] Preferably, a spring 85 is sleeved on the outer side of the connecting rod 82 , the bottom of the spring 85 is connected to the top of the mounting rod 81 , and the top of the spring 85 is connected to the bottom of the moving plate 84 .
[0040] The sealing plug can be used to seal the oil inlet pipe 7 when it is not in use. When the oil inlet pipe 7 is inserted into the aviation fuel extraction port, the movable plate 84 will drop due to external force obstruction. The movable plate 84 will drive the baffle 83 to drop through the connecting rod 82. The drop of the baffle 83 can open the through hole of the storage bottle and the oil inlet pipe 7, and the fuel can enter the storage bottle from the oil inlet pipe 7 through the through hole. When the fuel is not extracted, the rebound ability of the spring 85 itself can drive the baffle 83 to seal the through hole to prevent dust from entering the storage bottle from the oil inlet pipe 7.
[0041] It is understood that the above embodiments are merely exemplary embodiments used to illustrate the principles of the present invention, but the present invention is not limited thereto. For those skilled in the art, various modifications and improvements can be made without departing from the spirit and essence of the present invention, and these modifications and improvements are also considered to be within the scope of protection of the present invention.
Claims
1. A detection device for aviation fuel, characterized in that: The invention comprises a detection bottle, wherein the detection bottle is composed of an upper bottle body (1) and a lower bottle body (2) which are snap-fitted together; a discharge port (9) is arranged at one end of the top of the upper bottle body (1); an oil inlet pipe (7) is installed at the other end of the top of the upper bottle body (1); at least one snap-fitting protrusion (3) is embedded in the lower end of the upper bottle body (1); an annular snap-fitting piece (4) which is snap-fitted with the snap-fitting protrusion (3) is embedded in the upper end of the lower bottle body (2); an annular snap-fitting piece (4) is provided on the outer side wall of the annular snap-fitting piece (4) corresponding to the snap-fitting protrusion (3); the snap-fitting protrusion (3) is embedded in the annular snap-fitting piece (41); a placement plate (5) is arranged on the inner side wall of the annular snap-fitting piece (4); the placement plate (5) is used for placing a water test paper; a bottom cover (11) is arranged at the lower end of the lower bottle body (2); and a cleaning tool can be placed in the lower bottle body (2).
2. The aviation fuel detection device according to claim 1, characterized in that: The placement plate (5) is symmetrically provided with a fixing block (6), and the fixing block (6) is provided with a through hole, with both ends of the through hole facing the inner side wall of the annular clamping member (4) respectively, and the through hole is used to limit the position of the water test paper.
3. The aviation fuel detection device according to claim 1, characterized in that: The upper end of the annular engaging member (4) extends toward the upper bottle body (1), and the outer side wall of the lower end of the annular engaging member (4) is connected to the upper end of the lower bottle body (2). When the engaging protrusion (3) is located in the annular engaging groove (41), the inner side wall of the upper bottle body (1) is in close contact with the plane where the notch of the annular groove is located.
4. The aviation fuel detection device according to claim 2, characterized in that: The annular clamping groove (41) is provided with an inlet end and an outlet end. The inlet end extends to the upper end of the annular clamping piece (4) and is located below the corresponding clamping protrusion (3). The outlet end extends to the lower end of the annular clamping piece (4) and is connected to the upper bottle body (1). A limiting protrusion (42) is convexly provided in the annular clamping groove (41). The limiting protrusion (42) is located at the outlet end of the annular clamping groove (41). When the clamping protrusion (3) is located in the annular clamping groove (41) and conflicts with the limiting protrusion (42), the lower end of the upper bottle body (1) is closely connected with the upper end of the lower bottle body (2).
5. The aviation fuel detection device according to claim 4, characterized in that: The upper end surface of the limiting protrusion (42) is lower than the plane where the notch of the annular clamping groove (41) is located.
6. The aviation fuel detection device according to claim 1, characterized in that: A pressing assembly (8) is provided in the oil inlet pipe (7), and the pressing assembly (8) comprises a mounting rod (81), a connecting rod (82) is slidably inserted and connected to the top of the mounting rod (81), a baffle (83) is installed at the bottom of the connecting rod (82), and a movable plate (84) is installed at the top of the connecting rod (82).
7. The aviation fuel detection device according to claim 6, characterized in that: The upper bottle body (1) and the oil inlet pipe (7) are both provided with interconnected through holes, the bottom of the connecting rod (82) extends into the upper bottle body (1) through the through hole, and the top of the baffle (83) fits against the inner wall of the upper bottle body (1).
8. The aviation fuel detection device according to claim 7, characterized in that: A spring (85) is sleeved on the outer side of the connecting rod (82), the bottom of the spring (85) is connected to the top of the mounting rod (81), and the top of the spring (85) is connected to the bottom of the moving plate (84).