Aircraft preservative spraying auxiliary tool
By designing auxiliary tooling for corrosion inhibitor spraying, the problems of low efficiency, unevenness, and insufficient environmental performance of traditional aircraft corrosion inhibitor spraying have been solved, achieving uniform spraying, rapid drying, and air purification, thus improving operational safety.
Patent Information
- Authority / Receiving Office
- CN · China
- Patent Type
- Utility models(China)
- Current Assignee / Owner
- SHANDONG TAIKOO AIRCRAFT ENG
- Filing Date
- 2025-03-17
- Publication Date
- 2026-05-12
AI Technical Summary
Traditional aircraft corrosion inhibitor spraying suffers from problems such as low efficiency, uneven spraying, complex operation, and insufficient environmental performance.
An auxiliary tooling for aircraft corrosion protection spraying was designed, comprising a corrosion protection storage tank, a spray nozzle, a corrosion protection delivery mechanism, a heating box, a purification mechanism, and an altitude adjustment mechanism. Through the combination of a delivery pump, a spray nozzle, a heating mechanism, and a purification filter, uniform spraying, accelerated drying, and air purification are achieved.
It achieves uniform coating of aircraft wheel wells, reduces the diffusion of corrosion inhibitors, improves coating efficiency and environmental performance, and protects the health of operators.
Smart Images

Figure CN224221693U_ABST
Abstract
Description
Technical Field
[0001] This utility model relates to the field of aircraft maintenance technology, and in particular to an auxiliary tooling for spraying aircraft corrosion inhibitors. Background Technology
[0002] Aircraft are susceptible to corrosion due to prolonged exposure to harsh environments. Regularly applying anti-corrosion coatings to the wheel wells is a crucial measure for maintaining the structural integrity of aircraft. Traditional manual spraying methods suffer from low efficiency, uneven application, and high health risks to operators. While some auxiliary tools exist in current technologies, they still have limitations such as complex operation, insufficient spraying precision, and room for improvement in environmental performance. Utility Model Content
[0003] The purpose of this invention is to provide an auxiliary tooling for spraying aircraft corrosion inhibitors to solve the problems mentioned in the background art.
[0004] To achieve the above objectives, this utility model provides the following technical solution: an auxiliary tooling for aircraft corrosion inhibitor spraying, comprising a support plate, a horizontally arranged lifting plate above the support plate, a corrosion inhibitor storage tank, a baffle, and a heating box fixedly installed on the lifting plate, the baffle being vertically arranged on the lifting plate, a nozzle being provided on the corrosion inhibitor storage tank, a corrosion inhibitor delivery mechanism being provided on the corrosion inhibitor storage tank, the nozzle being connected to the corrosion inhibitor delivery mechanism via a gripping hose, a heating mechanism for heat drying the corrosion inhibitor being provided inside the heating box, a purification mechanism for air extraction and purification being provided on the lifting plate, and a height adjustment mechanism for adjusting the device height being provided on the support plate and the lifting plate.
[0005] Preferably, the preservative delivery mechanism includes a delivery pump fixedly installed on the top of the preservative storage tank, a pumping pipe fixedly installed at the inlet end of the delivery pump, the pumping pipe being located inside the preservative storage tank, a delivery pipe fixedly installed at the outlet end of the delivery pump, and the other end of the delivery pipe being connected to a nozzle via a gripping hose.
[0006] Preferably, the heating mechanism includes a heat pipe fixedly installed at the lower end of the heating box and a support plate horizontally installed at the upper end of the heating box. A fan is fixedly installed on the support plate, and the direction of the fan is vertically upward.
[0007] Preferably, the purification mechanism includes a purification filter element fixedly installed at the bottom of the lifting plate, the air inlet end of the purification filter element is connected to the air outlet of the exhaust fan, the exhaust pipe is fixedly fixed to the baffle in the vertical direction, the air inlet of the exhaust fan is connected to the lower end of the exhaust pipe, and the air outlet end of the purification filter element is fixedly installed with an air outlet pipe.
[0008] Preferably, the height adjustment mechanism includes a nut fixedly installed on the lifting plate, a height adjustment screw rotatably installed on the support plate in the vertical direction, an adjustment motor fixedly installed at the bottom of the support plate, the height adjustment screw being coaxially connected to the output end of the adjustment motor, and the nut being threadedly connected to the height adjustment screw.
[0009] Preferably, a guide rod is fixedly installed on the support plate in the vertical direction, and the lifting plate is slidably installed on the guide rod.
[0010] Preferably, a push handle is fixedly installed on the support plate, a caster wheel is provided at the bottom of the support plate, and an addition pipe is connected to the upper end of the preservative storage tank.
[0011] The beneficial effects of this utility model are:
[0012] In this invention, through the arrangement of a preservative storage tank, a spray nozzle, and a preservative delivery mechanism, a delivery pump draws the preservative from the storage tank into a delivery pipe, which then enters the spray nozzle. During spraying, the operator can hold the flexible hose 14 to spray the aircraft wheel wells and adjust the spraying position. The position of the adjustment device can be adjusted to regulate the spraying area, resulting in a more uniform spraying of the aircraft wheel wells. The heat pipe heats the air, and the fan blows hot air towards the spraying position, allowing for post-spray drying of the sprayed area and accelerating the drying of the preservative.
[0013] In this invention, the height adjustment mechanism, baffle, and purification mechanism are designed to allow the height adjustment screw to rotate when the motor rotates. This rotation of the screw then moves the nut on the screw, allowing the device to be adjusted to a suitable spraying height for easier spraying. The baffle blocks the spread of the preservative from the operator's side, slowing down the spread of the preservative. The exhaust fan draws the spread preservative into the purification filter through the exhaust pipe for purification. The purified air is then discharged through the exhaust pipe, protecting the environment and the health of the operators. Attached Figure Description
[0014] Figure 1 This is a three-dimensional structural diagram of an auxiliary tooling for spraying anti-corrosion agents on aircraft, as proposed in this utility model.
[0015] Figure 2 This is a schematic diagram of the structure of the anticorrosive agent storage tank, heating box, baffle, etc., of an auxiliary tooling for aircraft anticorrosive agent spraying proposed in this utility model.
[0016] Figure 3 This is a schematic diagram of the heat pipe, fan, and other structures of an auxiliary tooling for spraying aircraft corrosion inhibitors proposed in this utility model;
[0017] Figure 4 This is a schematic diagram of the extraction pipe, delivery pipe, and other structures of an auxiliary tooling for spraying aircraft corrosion inhibitors proposed in this utility model.
[0018] In the diagram: 1. Support plate; 2. Lifting plate; 3. Preservative storage tank; 4. Baffle; 5. Nozzle; 6. Preservative delivery mechanism; 61. Delivery pump; 62. Extraction pipe; 63. Delivery pipe; 7. Heating box; 8. Drying mechanism; 81. Heat pipe; 82. Support plate; 83. Fan; 9. Purification mechanism; 91. Purification filter element; 92. Exhaust pipe; 93. Exhaust fan; 94. Exhaust pipe; 10. Height adjustment mechanism; 101. Nut; 102. Height adjustment screw; 103. Adjustment motor; 104. Guide rod; 11. Push handle; 12. Casters; 13. Addition pipe; 14. Holding hose. Detailed Implementation
[0019] The technical solutions of the present utility model will be clearly and completely described below with reference to the accompanying drawings of the embodiments of the present utility model. Obviously, the described embodiments are only some embodiments of the present utility model, and not all embodiments.
[0020] Example:
[0021] like Figure 1-4 As shown, this embodiment provides an auxiliary tooling for spraying aircraft preservatives, including a support plate 1, a horizontally arranged lifting plate 2 above the support plate 1, a preservative storage tank 3, a baffle 4 and a heating box 7 fixedly installed on the lifting plate 2, the baffle 4 being vertically arranged on the lifting plate 2, a nozzle 5 being provided on the preservative storage tank 3, a preservative conveying mechanism 6 for conveying preservatives being provided on the preservative storage tank 3, the nozzle 5 being connected to the preservative conveying mechanism 6 via a gripping hose 14, a heating mechanism 8 for hot drying of preservatives being provided inside the heating box 7, a purification mechanism 9 for air extraction and purification being provided on the lifting plate 2, and a height adjustment mechanism 10 for adjusting the height of the device being provided on the support plate 1 and the lifting plate 2.
[0022] The preservative to be sprayed is added to the preservative storage tank 3 through the addition pipe 13. The amount of preservative added can be observed through the liquid level bar on the preservative storage tank 3. The device is moved and its direction of movement is adjusted, and the device is pushed into the bottom of the aircraft wheel well. The height adjustment mechanism 10 can be used to adjust the device to a suitable spraying height for convenient spraying. The preservative delivery mechanism 6 can draw the preservative from the preservative storage tank 3 to the nozzle 5, and spray it upwards onto the aircraft wheel well through the nozzle 5. During spraying, the operator can... Holding the flexible hose 14, spray the aircraft wheel wells and adjust the spraying position. The position of the adjustment device can be adjusted to adjust the spraying area, making the operation relatively convenient and the spraying of the aircraft wheel wells relatively uniform. The heat drying mechanism 8 can blow hot air to the spraying position and heat dry the sprayed position after spraying to accelerate the drying of the preservative. During spraying, the baffle 4 can block the spread of the preservative on the operator's side and slow down the spread of the preservative. The purification mechanism 9 can purify the air to protect the environment and the health of the operators.
[0023] In this embodiment of the utility model, specifically, the preservative delivery mechanism 6 includes a delivery pump 61 fixedly installed on the top of the preservative storage tank 3. A pumping pipe 62 is fixedly installed at the inlet end of the delivery pump 61, and the pumping pipe 62 is located inside the preservative storage tank 3. A delivery pipe 63 is fixedly installed at the outlet end of the delivery pump 61, and the other end of the delivery pipe 63 is connected to the nozzle 5 through a holding hose 14.
[0024] To achieve the application of the preservative, the delivery pump 61 draws the preservative from the preservative storage tank 3 into the delivery pipe 63 through the delivery pipe 62, and then through the delivery pipe 63 and the holding hose 14 into the nozzle 5. The preservative is then sprayed upwards onto the aircraft wheel wells through the nozzle 5. During spraying, the operator can hold the holding hose 14 to spray the aircraft wheel wells and adjust the spraying position, making the operation convenient and the spraying of the aircraft wheel wells relatively uniform.
[0025] In this embodiment of the utility model, specifically, the heating mechanism 8 includes a heat pipe 81 fixedly installed at the lower end of the heating box 7 and a support plate 82 horizontally installed at the upper end of the heating box 7. A fan 83 is fixedly installed on the support plate 82, and the direction of the fan 83 is vertically upward.
[0026] To heat the sprayed preservative and accelerate its drying process, heat pipe 81 heats the air, and fan 83 blows hot air towards the spraying position, thus heating the sprayed area and accelerating the drying of the preservative.
[0027] In this embodiment of the utility model, specifically, the purification mechanism 9 includes a purification filter element 91 fixedly installed at the bottom of the lifting plate 2. The air inlet end of the purification filter element 91 is connected to the air outlet of the exhaust fan 93. The exhaust pipe 92 is fixed on the baffle 4 in the vertical direction. The air inlet of the exhaust fan 93 is connected to the lower end of the exhaust pipe 92. An exhaust pipe 94 is fixedly installed at the air outlet end of the purification filter element 91.
[0028] To reduce the absorption of airborne preservatives by operators, a vertically installed baffle 4 is used during spraying to block the preservative from spreading to the operator's side, slowing down its diffusion. An exhaust fan 93 draws the diffused preservative through an exhaust pipe 92 into a purification filter 91 for purification. The purified air is then discharged through an exhaust pipe 94, protecting the environment and the health of the operators.
[0029] In this embodiment of the utility model, specifically, the height adjustment mechanism 10 includes a nut 101 fixedly installed on the lifting plate 2, a height adjustment screw 102 rotatably installed on the support plate 1 in the vertical direction, an adjustment motor 103 fixedly installed at the bottom of the support plate 1, the height adjustment screw 102 and the output end of the adjustment motor 103 being coaxially connected, and the nut 101 and the height adjustment screw 102 being threadedly connected.
[0030] To adjust the spraying height of the device, the rotation of the adjusting motor 103 will drive the height adjusting screw 102 to rotate. The rotation of the height adjusting screw 102 will drive the nut 101 to move on the height adjusting screw 102, thereby adjusting the device to a suitable spraying height for convenient spraying.
[0031] In this embodiment of the utility model, a guide rod 104 is fixedly installed on the support plate 1 along the vertical direction, and the lifting plate 2 is slidably installed on the guide rod 104.
[0032] In order to guide the movement of the lifting plate 2, the guide rod 104 can guide the movement of the lifting plate 2, so that the lifting plate 2 can only move up and down along the guide rod 104.
[0033] In this embodiment of the utility model, a push handle 11 is fixedly installed on the support plate 1, a caster wheel 12 is provided at the bottom of the support plate 1, and an addition tube 13 is connected to the upper end of the preservative storage tank 3.
[0034] To facilitate adjusting the position of the device, grasp the push handle 11 and push the device; the casters 12 roll and rotate on the ground to move the device and adjust the direction of movement.
[0035] Working principle: During use, the preservative to be sprayed is added to the preservative storage tank 3 through the addition tube 13. The amount of preservative added can be observed through the level bar on the preservative storage tank 3. Then, hold the push handle 11 and push the device; the casters 12 roll and rotate on the ground, allowing the device to move and its direction of movement to be adjusted. Push the device into the bottom of the aircraft wheel well. Then, start the adjustment motor 103. The rotation of the adjustment motor 103 will drive the height adjustment screw 102 to rotate. The guide rod 104 guides the movement of the lifting plate 2, ensuring that the lifting plate 2 can only move up and down along the guide rod 104, thus adjusting the height. Rotating the height adjustment screw 102 will cause the nut 101 to move on the height adjustment screw 102, which can adjust the device to a suitable spraying height to facilitate spraying. When spraying, the delivery pump 61 is started. The delivery pump 61 will draw the preservative in the preservative storage tank 3 into the delivery pipe 63 through the delivery pipe 62, and then into the nozzle 5 through the delivery pipe 63. The nozzle 5 will then spray the preservative upwards onto the aircraft wheel well. When spraying, the operator can hold the holding hose 14 to spray the aircraft wheel well and adjust the spraying position. The position of the device can be adjusted and the spraying area can be adjusted to ensure that the spraying of the aircraft wheel well is relatively uniform. Heat pipe 81 heats the air, and fan 83 blows hot air toward the spraying position, which can heat the sprayed position after spraying to accelerate the drying of the preservative. During spraying, baffle 4 can block the preservative from spreading to the operator's side and slow down the spread of the preservative. Exhaust fan 93 will draw the spread preservative into the purification filter 91 through exhaust pipe 92 for purification. The purified air will be discharged through exhaust pipe 94 to protect the environment and the health of the operator.
[0036] The above description is only a preferred embodiment of the present utility model, but the protection scope of the present utility model is not limited thereto. Any equivalent substitutions or changes made by those skilled in the art within the technical scope disclosed in the present utility model, based on the technical solution and the inventive concept of the present utility model, should be included within the protection scope of the present utility model.
Claims
1. An auxiliary tooling for spraying aircraft corrosion inhibitors, comprising a support plate (1), characterized in that: A horizontally arranged lifting plate (2) is provided above the support plate (1). A preservative storage tank (3), a baffle (4) and a heating box (7) are fixedly installed on the lifting plate (2). The baffle (4) is vertically arranged on the lifting plate (2). A nozzle (5) is provided on the preservative storage tank (3). A preservative conveying mechanism (6) for conveying preservatives is provided on the preservative storage tank (3). The nozzle (5) is connected to the preservative conveying mechanism (6) through a holding hose (14). A heat drying mechanism (8) for preservative heat drying is provided inside the heating box (7). A purification mechanism (9) for air extraction and purification is provided on the lifting plate (2). A height adjustment mechanism (10) for adjusting the height of the device is provided on the support plate (1) and the lifting plate (2).
2. The auxiliary tooling for spraying aircraft corrosion inhibitors according to claim 1, characterized in that: The preservative delivery mechanism (6) includes a delivery pump (61) fixedly installed on the top of the preservative storage tank (3). A pumping pipe (62) is fixedly installed at the inlet end of the delivery pump (61), and the pumping pipe (62) is located inside the preservative storage tank (3). A delivery pipe (63) is fixedly installed at the outlet end of the delivery pump (61), and the other end of the delivery pipe (63) is connected to the nozzle (5) through a holding hose (14).
3. The auxiliary tooling for spraying aircraft corrosion inhibitors according to claim 1, characterized in that: The heating mechanism (8) includes a heat pipe (81) fixedly installed at the lower end of the heating box (7) and a support plate (82) horizontally installed at the upper end of the heating box (7). A fan (83) is fixedly installed on the support plate (82), and the direction of the fan (83) is vertically upward.
4. The auxiliary tooling for spraying aircraft corrosion inhibitors according to claim 1, characterized in that: The purification mechanism (9) includes a purification filter element (91) fixedly installed at the bottom of the lifting plate (2). The air inlet of the purification filter element (91) is connected to the air outlet of the exhaust fan (93). The exhaust pipe (92) is fixed on the baffle (4) in the vertical direction. The air inlet of the exhaust fan (93) is connected to the lower end of the exhaust pipe (92). The air outlet of the purification filter element (91) is fixedly installed with an air outlet pipe (94).
5. The auxiliary tooling for spraying aircraft corrosion inhibitors according to claim 1, characterized in that: The height adjustment mechanism (10) includes a nut (101) fixedly installed on the lifting plate (2), a height adjustment screw (102) rotatably installed on the support plate (1) in the vertical direction, an adjustment motor (103) fixedly installed at the bottom of the support plate (1), the height adjustment screw (102) and the output end of the adjustment motor (103) are coaxially connected, and the nut (101) and the height adjustment screw (102) are threadedly connected.
6. The auxiliary tooling for spraying aircraft corrosion inhibitors according to claim 2, characterized in that: A guide rod (104) is fixedly installed on the support plate (1) along the vertical direction, and the lifting plate (2) is slidably installed on the guide rod (104).
7. The auxiliary tooling for spraying aircraft corrosion inhibitors according to claim 1, characterized in that: A push handle (11) is fixedly installed on the support plate (1), and a caster wheel (12) is provided at the bottom of the support plate (1). An addition pipe (13) is connected to the upper end of the preservative storage tank (3).