Blind area paint spraying device for wide-body aircraft hangar vertical tail leading edge fuselage section

Abstract

The application discloses a kind of for wide-body aircraft dock vertical tail front edge fuselage section blind area paint spraying device including steel structure installation platform and three groups of operating platform, steel structure installation platform is symmetrically arranged along the two sides of fuselage, and two operating platforms are a group respectively along the width direction installation of steel structure installation platform, and three groups of operating platform are installed along the length direction of steel structure installation platform, operating platform includes fixed steel structure, lifting steel structure, lifting mechanism, guide structure and platform mechanism, fixed steel structure is fixedly connected with steel structure installation platform, lifting steel structure is arranged on fixed steel structure, guide structure is arranged between fixed steel structure and lifting steel structure, lifting mechanism is arranged on lifting steel structure, and platform mechanism is arranged at the lower end of lifting steel structure.The application effectively improves work efficiency, is suitable for different machine types and tail cone paint spraying operation, while effectively ensuring aircraft fuselage safety.

Description

Technical Field

[0001] This invention belongs to the field of blind spot painting technology, and particularly relates to a blind spot painting device for the fuselage section at the leading edge of the vertical tail of a wide-body aircraft dock. Background Technology

[0002] Wide-body aircraft, also known as wide-fuselage aircraft, refer to aircraft with a large-diameter fuselage. During painting operations, the vertical lift painting device has a limited descent height due to the conical shape of the fan tail, resulting in a painting blind spot in the fuselage section below the leading edge of the vertical tail. In the current technology, this area can only be painted using a mobile articulated boom truck, which leads to low work efficiency. In addition, there is the problem of damage to the aircraft due to operational errors when the articulated boom truck approaches the aircraft. Summary of the Invention

[0003] To at least partially solve the technical problems existing in the prior art, the present invention provides a device for blind zone painting of the fuselage section at the leading edge of the vertical tail of a wide-body aircraft dock.

[0004] The present invention provides a device for blind zone painting of the fuselage section at the leading edge of the vertical tail of a wide-body aircraft dock. The device includes a steel structure mounting platform and three sets of operating platforms. The steel structure mounting platform is symmetrically arranged along both sides of the fuselage. Two operating platforms are installed in a group along the width direction of the steel structure mounting platform. One set of operating platforms is located on the left side of the steel structure mounting platform along its length direction, one set is located in the middle of the steel structure mounting platform along its length direction, and one set is located on the right side of the steel structure mounting platform along its length direction. Wherein:

[0005] The operating platform includes a fixed steel structure, a lifting steel structure, a lifting mechanism, a guide structure, and a platform mechanism. The fixed steel structure is fixedly connected to the steel structure installation platform. The lifting steel structure is installed on the fixed steel structure. The guide structure is installed between the fixed steel structure and the lifting steel structure. The lifting mechanism is installed on the lifting steel structure and is used to drive the lifting steel structure to move up and down. The platform mechanism is installed at the lower end of the lifting steel structure.

[0006] Furthermore, in the above-mentioned blind zone painting device for the fuselage section at the leading edge of the vertical tail of a wide-body aircraft dock, the lifting mechanism includes a mounting platform, a geared motor, a coupling, a lifting machine, and a lifting rod. The mounting platform is fixed in the middle of the lifting steel structure, the geared motor is installed on one side of the lifting steel structure, the lifting machine is symmetrically installed at both ends of the mounting platform, the output end of the geared motor is connected to the input end of the lifting machine through the coupling, the lifting rod is installed on the steel structure mounting platform through a hinge, and the output end of the lifting machine is connected to the lifting rod in a lifting connection.

[0007] Furthermore, in the above-mentioned blind zone painting device for the fuselage section at the leading edge of the vertical tail of a wide-body aircraft dock, the guide structure includes a vertical guide wheel, a horizontal guide wheel, and a mounting plate. The vertical guide wheel is vertically arranged on the mounting plate, and the horizontal guide wheel is horizontally arranged on the mounting plate. The mounting plate is fixed to the upper end of the lifting steel structure with rivets. The distance from the mounting plate to the highest point of the vertical guide wheel is higher than the distance from the mounting plate to the highest point of the horizontal guide wheel.

[0008] Furthermore, in the above-mentioned blind zone painting device for the fuselage section at the leading edge of the vertical tail of the wide-body aircraft dock, a limiting groove is provided on the side of the fixed steel structure near the lifting steel structure, the two sides of the limiting groove are slidably connected to the horizontal guide wheel, and the bottom of the limiting groove is slidably connected to the vertical guide wheel 241.

[0009] Furthermore, in the above-mentioned painting device for the blind zone of the fuselage section at the leading edge of the vertical tail of a wide-body aircraft dock, the platform mechanism includes a painting platform, a pull-out plate, a guide wheel, and a railing. The painting platform is fixedly connected to the lifting steel structure. The pull-out plate is slidably disposed inside the painting platform. The guide wheel is installed on one side of the painting platform and is circumferentially connected to the pull-out plate. The railing is disposed on the outside of the painting platform.

[0010] The present invention provides a blind zone painting device for the fuselage section at the leading edge of the vertical tail of a wide-body aircraft dock, which has the following advantages and beneficial effects:

[0011] The invention has a simple overall structure and is easy to operate. The cooperation between the steel structure installation platform and three sets of operating platforms allows for simultaneous painting operations on both sides of the aircraft, effectively improving work efficiency. By adjusting the lifting height of the operating platform and the extension length of the platform mechanism, it can adapt to the taper of the transition section between the wide-body fuselage and the tail, thereby effectively avoiding the generation of blind spots in painting. Attached Figure Description

[0012] To more clearly illustrate the technical solutions in the embodiments of the present invention or the prior art, the drawings used in the description of the embodiments or the prior art will be briefly introduced below. Obviously, the drawings described below are only for further understanding of the embodiments of the present invention and constitute a part of the present invention. For those skilled in the art, other drawings can be obtained based on these drawings without creative effort. In the drawings:

[0013] Figure 1 This is a front view of the blind spot painting device for the fuselage section at the leading edge of the vertical tail of a wide-body aircraft dock according to the present invention;

[0014] Figure 2 This is a right view of the blind spot painting device for the fuselage section leading edge of the vertical tail of a wide-body aircraft dock according to the present invention;

[0015] Figure 3 This is an enlarged structural schematic diagram of the operating platform of the blind zone painting device for the fuselage section at the leading edge of the vertical tail of a wide-body aircraft dock, according to the present invention.

[0016] Explanation of reference numerals in the attached figures:

[0017] 1: Steel structure installation platform;

[0018] 2: Operating platform;

[0019] 21: Fixed steel structure; 211: Limiting groove;

[0020] 22: Lifting steel structure;

[0021] 23: Lifting mechanism; 231: Mounting platform; 232: Gear motor; 234: Coupling; 235: Lifting machine; 236: Lifting rod;

[0022] 24: Guide structure; 241: Vertical guide wheel; 242: Horizontal guide wheel; 243: Mounting plate;

[0023] 25: Platform structure; 251: Painting platform; 252: Pull-out panel; 253: Guide wheel; 254: Railing. Detailed Implementation

[0024] To make the objectives, technical solutions, and advantages of this invention clearer, the technical solutions of this invention will be clearly and completely described below in conjunction with specific embodiments and corresponding drawings. Obviously, the described embodiments are only a part of the embodiments of this invention, and not all of them. All other embodiments obtained by those skilled in the art based on the embodiments of this invention without creative effort are within the scope of protection of this invention.

[0025] like Figures 1 to 3 As shown, the blind zone painting device for the fuselage section at the leading edge of the vertical tail of a wide-body aircraft dock according to the present invention includes a steel structure installation platform 1 and three sets of operating platforms 2. The steel structure installation platform 1 is symmetrically arranged along both sides of the fuselage. Two operating platforms 2 are installed as a group along the width direction of the steel structure installation platform 1. One set of operating platforms 2 is located on the left side of the steel structure installation platform 1 along its length direction, one set of operating platforms 2 is located in the middle of the steel structure installation platform 1 along its length direction, and one set of operating platforms 2 is located on the right side of the steel structure installation platform 1 along its length direction, wherein:

[0026] The operating platform 2 includes a fixed steel structure 21, a lifting steel structure 22, a lifting mechanism 23, a guide structure 24, and a platform mechanism 25. The fixed steel structure 21 is fixedly connected to the steel structure installation platform 1. The lifting steel structure 22 is installed on the fixed steel structure 21. The guide structure 24 is installed between the fixed steel structure 21 and the lifting steel structure 22. The lifting mechanism 23 is installed on the lifting steel structure 22 and is used to drive the lifting steel structure 22 to lift. The platform mechanism 25 is installed at the lower end of the lifting steel structure 22.

[0027] Furthermore, in the blind zone painting device for the fuselage section at the leading edge of the vertical tail of a wide-body aircraft dock according to the present invention, the lifting mechanism 23 includes a mounting platform 231, a reduction motor 232, a coupling 234, a lifting platform 235, and a lifting rod 236. The mounting platform 231 is fixed in the middle of the lifting steel structure 22, the reduction motor 232 is installed on one side of the lifting steel structure 22, the lifting platform 235 is symmetrically installed at both ends of the mounting platform 231, and the output end of the reduction motor 232 is connected to the input end of the lifting platform 235 through the coupling 234. The lifting rod... 236 is mounted on the steel structure installation platform 1 via a hinge shaft. The output end of the lifting machine 235 is connected to the lifting rod 236 for lifting. The driving force generated by the geared motor 232 is distributed to the lifting machine 235 via the coupling 234, causing the lifting machine 235 to move along the lifting rod 236 and drive the lifting steel structure 22 to rise and fall. When the geared motor 232 provides driving force to one end of the lifting machine 235 through the coupling 234, the lifting rod 236 rotates on the steel structure installation platform 1 via the hinge shaft, which allows the lifting steel structure 22 to be tilted and adjusted.

[0028] Furthermore, in the above-mentioned blind spot painting device for the fuselage section at the leading edge of the vertical tail of the wide-body aircraft dock, the guide structure 24 includes a vertical guide wheel 241, a horizontal guide wheel 242, and a mounting plate 243. The vertical guide wheel 241 is vertically arranged on the mounting plate 243, and the horizontal guide wheel 242 is horizontally arranged on the mounting plate 243. The mounting plate 243 is fixed to the upper end of the lifting steel structure 22 with rivets. The distance from the mounting plate 243 to the highest point of the vertical guide wheel 241 is higher than the distance from the mounting plate 243 to the highest point of the horizontal guide wheel 242.

[0029] Furthermore, in the aforementioned blind zone painting device for the fuselage section at the leading edge of the vertical tail of the wide-body aircraft dock, a limiting groove 211 is provided on the side of the fixed steel structure 21 near the lifting steel structure 22. The two sides of the limiting groove 211 are slidably connected to the horizontal guide wheel 242, and the bottom of the limiting groove 211 is slidably connected to the vertical guide wheel 241. When the lifting steel structure 22 is raised and lowered within the fixed steel structure 21, it can be guided and slid by the horizontal guide wheel 242 and the vertical guide wheel 241, effectively avoiding deviation during the raising and lowering process that could cause damage to the aircraft body.

[0030] Furthermore, in the aforementioned painting device for the blind zone of the fuselage section at the leading edge of the vertical tail of a wide-body aircraft dock, the platform mechanism 25 includes a painting platform 251, a pull-out plate 252, a guide wheel 253, and a railing 254. The painting platform 251 is fixedly connected to the lifting steel structure 22. The pull-out plate 252 is slidably disposed inside the painting platform 251. The guide wheel 253 is installed on one side of the painting platform 251 and is circumferentially connected to the pull-out plate 252. The railing 254 is disposed on the outside of the painting platform 251. During painting operations, the pull-out plate 252 can be extended close to the aircraft body by driving the guide wheel 253. The railing 254 effectively ensures the safe passage of platform operators.

[0031] Specifically, during the painting operation, the operating platform 2 installed on the steel structure mounting platform 1 is controlled separately. First, the operating platform 2 closest to the aircraft body is adjusted so that the corresponding lifting steel structures 22 on the left, middle, and right sides are raised and lowered respectively through the lifting mechanism 23. The platform mechanism 25 stops raising and lowering when it approaches the aircraft body, ensuring that the platform mechanism 25 on the inner operating platform 2 will not collide with the aircraft. Then, the outer operating platform 2 is adjusted so that the corresponding lifting steel structures 22 on the left, middle, and right sides are raised and lowered respectively through the lifting mechanism 23. During the raising and lowering process, the reduction motor 232 provides power, which is transmitted to the elevator 235 via the coupling 234. The machine 235 moves up and down along the lifting rod 236, so that the lifting steel structure 22 moves up and down along the upper limit groove 211 of the fixed steel structure 21 through the vertical guide wheel 241 and the horizontal guide wheel 242 installed on the upper two side mounting plates 243. This ensures that the distance between the platform mechanism 25 on the outer operating platform 2 and the platform mechanism 25 on the inner operating platform 2 is greater than the height of the operator, so as to carry out the painting operation. At this time, the pull-out plate 252 inside the painting platform 251 is extended infinitely close to the aircraft body through the guide wheel 253 to adapt to the tail taper of the aircraft. At this time, the operator can enter the pull-out plate 252 through the side of the painting platform 251 with the railing 254 to carry out the painting operation.

[0032] In summary, compared with the prior art, the paint spraying device for the blind zone of the fuselage section at the leading edge of the vertical tail of the wide-body aircraft dock of the present invention has the following advantages and beneficial effects:

[0033] The invention has a simple overall structure and is easy to operate. The cooperation between the steel structure installation platform and three sets of operating platforms allows for simultaneous painting operations on both sides of the aircraft, effectively improving work efficiency. By adjusting the lifting height of the operating platform and the extension length of the platform mechanism, it can adapt to the taper of the transition section between the wide-body fuselage and the tail, thereby effectively avoiding the generation of blind spots in painting.

[0034] It should be noted that, unless otherwise expressly specified and limited, the term "connection" or its synonyms should be interpreted broadly in this document. For example, "connection" can be a fixed connection or a detachable connection; it can be a mechanical connection or an electrical connection; it can be a direct connection or an indirect connection through an intermediate medium; it can be the internal communication of two elements or the interaction between two elements. Those skilled in the art can understand the specific meaning of the above terms in this invention according to the specific circumstances. Furthermore, expressions such as "first" and "second" are merely used to distinguish one entity or operation from another, and do not necessarily require or imply any such actual relationship or order between these entities or operations. Meanwhile, the terms "comprising," "including," or any other variations thereof are intended to cover non-exclusive inclusion, such that a process, method, article, or apparatus that comprises a list of elements includes not only those elements but also other elements not expressly listed, or elements inherent to such a process, method, article, or apparatus. In addition, the terms "front," "rear," "left," "right," "upper," and "lower" in this document refer to the placement states shown in the accompanying drawings.

[0035] Finally, it should be noted that the above embodiments are only used to illustrate the technical solutions of the present invention, and not to limit them; although the present invention has been described in detail with reference to the foregoing embodiments, those skilled in the art should understand that modifications can still be made to the technical solutions described in the foregoing embodiments, or equivalent substitutions can be made to some of the technical features; and these modifications or substitutions do not cause the essence of the corresponding technical solutions to deviate from the spirit and scope of the technical solutions of the embodiments of the present invention.

Claims

1. A device for blind zone painting of the fuselage section at the leading edge of the vertical tail of a wide-body aircraft dock, characterized in that, The device for blind spot painting of the fuselage section at the leading edge of the vertical tail of a wide-body aircraft dock includes a steel structure installation platform and three sets of operating platforms. The steel structure installation platform is symmetrically arranged along both sides of the fuselage. Two operating platforms are installed in a group along the width direction of the steel structure installation platform. One set of operating platforms is located on the left side of the steel structure installation platform along its length direction, one set is located in the middle of the steel structure installation platform along its length direction, and one set is located on the right side of the steel structure installation platform along its length direction. The operating platform includes a fixed steel structure, a lifting steel structure, a lifting mechanism, a guide structure, and a platform mechanism. The fixed steel structure is fixedly connected to the steel structure installation platform. The lifting steel structure is installed on the fixed steel structure. The guide structure is installed between the fixed steel structure and the lifting steel structure. The lifting mechanism is installed on the lifting steel structure and is used to drive the lifting steel structure to lift. The platform mechanism is installed at the lower end of the lifting steel structure. The lifting mechanism includes a mounting platform, a geared motor, a coupling, a lifting platform, and a lifting rod. The mounting platform is fixed in the middle of the lifting steel structure. The geared motor is installed on one side of the lifting steel structure. The lifting platforms are symmetrically installed at both ends of the mounting platform. The output end of the geared motor is connected to the input end of the lifting platform through the coupling. The lifting rod is installed on the steel structure mounting platform through a hinge. The output end of the lifting platform is connected to the lifting rod for lifting. The driving force generated by the geared motor is distributed to the lifting platform through the coupling, causing the lifting platform to move along the lifting rod and drive the lifting steel structure to rise and fall. When the geared motor provides driving force to one end of the lifting platform through the coupling, the lifting rod rotates on the steel structure mounting platform through the hinge, which allows the lifting steel structure to be tilted and adjusted. The guide structure includes a vertical guide wheel, a horizontal guide wheel, and a mounting plate. The vertical guide wheel is vertically mounted on the mounting plate, and the horizontal guide wheel is horizontally mounted on the mounting plate. The mounting plate is fixed to the upper end of the lifting steel structure with rivets. The distance from the mounting plate to the highest point of the vertical guide wheel is greater than the distance from the mounting plate to the highest point of the horizontal guide wheel. The fixed steel structure is provided with a limiting groove on the side near the lifting steel structure. The two sides of the limiting groove are slidably connected to the horizontal guide wheel, and the bottom of the limiting groove is slidably connected to the vertical guide wheel. When the lifting steel structure is raised and lowered within the fixed steel structure, it can be guided and slid by the horizontal guide wheel and the vertical guide wheel. The platform mechanism includes a painting platform, a pull-out plate, guide wheels, and railings. The painting platform is fixedly connected to the lifting steel structure. The pull-out plate is slidably disposed inside the painting platform. The guide wheels are installed on one side of the painting platform and are circumferentially connected to the pull-out plate. The railings are disposed on the outside of the painting platform.

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