A device and method for aligning the slotted nut lock plate holes of an aviation accessory casing

Abstract

The present invention provides a device for aligning the hole position of a slotted nut lock piece of an aviation accessory casing, comprising: an upper electric cylinder and a replacement base, wherein the lower end of the upper electric cylinder is provided with a group of lower pressure rods for controlling the upward and downward movement of the holding base. Compared with the prior art, the present invention has the following beneficial effects: by using a support platform to limit the rotational balance of the driving component, it can be connected to the middle position of the driving component by using a limit bearing, by using a lower screwing head to tighten the slotted nut of the aviation accessory casing, and by using a rear support plate to install and support the slide rail, the lower clamping seat and the replacement base. The beneficial effects of this method are: by using a motor to bear force and drive the driving component to move downward as a whole, and the driving component drives the screwing head to move downward and make the screwing head and the nut to be locked contact with each other, and then the screwing head is driven by the driving component to rotate to make the nut and the aviation accessory casing locked and connected.

Description

Technical Field

[0001] The invention discloses a device and method for aligning slotted nut locking plate holes of an aviation accessory casing, belonging to the technical field of aviation accessory casing installation. Background Art

[0002] The accessory casing of an aircraft engine contains multiple gear shaft assemblies, which are secured at both ends using slotted nuts. Locking plates are often used to secure the slotted nuts. The locking plates are placed in corresponding slots in the slotted nuts and nut mounting bases, with the nut slot width allowing for no more than 0.25mm of clearance on either side.

[0003] Currently, tightening and assembling slotted nuts equipped with locking plates is still primarily a manual process. During the tightening process, the alignment of the nut slots with the mounting base slots is visually observed. Workers must operate the tightening tool to slowly tighten the slotted nut in the same direction, constantly observing the nut slot position. Tightening must stop when a slot aligns with a slot in the mounting base. This process generally requires the worker's experience to ensure and complete.

[0004] Some methods use visual cameras to monitor the slot position for alignment, but due to the accuracy limitations of visual cameras, as well as the influence of the environment, lighting, and product spatial position, they often fail to meet application requirements and are not universal. In existing technical methods, the slotted nut and mounting base slot position alignment relies on manual visual inspection and manual alignment, which has significant disadvantages.

[0005] It did not reduce the labor intensity of the workers;

[0006] The instability of manual operation may result in improper alignment during one tightening, and the nut cannot be reversed, so it may be necessary to loosen and retighten it, which is time-consuming and labor-intensive.

[0007] Human safety is affected;

[0008] It will be difficult to cope with the assembly requirements of higher alignment accuracy in the future;

[0009] Therefore, there is an urgent need for an aviation accessory casing slotted nut lock plate hole alignment device and method to solve the above problems. Summary of the Invention

[0010] In view of the deficiencies in the prior art, the present invention aims to provide a slotted nut lock plate hole alignment device for an aviation accessory casing, comprising: an upper electric cylinder and a replacement base, so as to solve the problems raised in the above-mentioned background technology.

[0011] The technical solution of the present invention is achieved as follows: a device for aligning the slotted nut lock plate holes of an aviation accessory casing, comprising: an upper electric cylinder and a replacement base, wherein the lower end of the upper electric cylinder is provided with a set of lower pressure rods for controlling the upward and downward movement of the pressure holding seat;

[0012] The lower end of the lower pressure rod is provided with a group of pressure holding seats for controlling the upper and lower positions of the motor, the pressure holding seats are fixed to the upper end of the motor by bolts, the outer side of the upper end of the lower pressure rod is provided with a group of upper support frames for supporting the upper electric cylinder, and the lower end of the motor is provided with a group of drive components for transmitting motor power;

[0013] A group of support platforms for limiting the rotational balance of the drive assembly are provided on the outside of the middle position of the drive assembly. The cross-section of the support platform is a rectangular structure when viewed from above, and a circular inner groove is provided inside. A group of limit bearings for interconnecting with the middle position of the drive assembly are provided inside the circular inner groove of the support platform. A group of lower screw-on heads for tightening the slotted nuts of the aviation accessory casing are provided at the lower end of the drive assembly. The rotational balance of the drive assembly can be limited by using the support platform, and the limit bearings can be connected to the middle position of the drive assembly.

[0014] As a preferred embodiment, the upper end of the lower screwing head is provided with an internal connecting thread, the lower screwing head and the lower end of the driving assembly are screwed together, and the rear side of the upper support frame is provided with a plurality of groups of rear slides for driving the upper support frame to move up and down;

[0015] Two groups of slide rails are provided on the rear side of several groups of rear slides for limiting the up and down movement of the rear slides. Several groups of rear slides are movably engaged with the two groups of slide rails respectively. There are two groups of slide rails, and the two groups of slide rails are in a parallel state. The two groups of slide rails are connected and fixed to the rear support plate by bolts, and the slotted nuts of the aviation accessory casing can be tightened by using the lower screw head.

[0016] As a preferred embodiment, a group of rear support plates for mounting and supporting the slide rails, the lower card seat and the replacement base are provided on the rear side of the two groups of slide rails, and two groups of rear support frames for supporting the rear support plates are provided on the rear side of the rear support plates;

[0017] The rear support frame is provided with two groups, and a group of rear support electric cylinders for adjusting the support height of the support platform is provided at the middle position inside the two groups of rear support frames. The upper end of the rear support electric cylinder is provided with a group of force guide plates for connecting and fixing with the support platform and driving the support platform to move synchronously. The lower card seat is a detachable structure, and the replacement base and the lower card seat are installed at the same position. The replacement base and the lower card seat are installed one by one according to the required functions, and the slide rail, the lower card seat and the replacement base can be installed and supported by using the rear support plate, the support height of the support platform can be adjusted by using the rear support electric cylinder, and the force guide plate can be used to connect and fix with the support platform and drive the support platform to move synchronously.

[0018] As a preferred embodiment, the drive assembly includes a lower drive end and a lower support seat, the lower drive end is arranged at the lower end of the motor and is connected to the internal power of the motor, the cross section of the lower drive end is a circular structure, and the lower drive end is an active rotating structure;

[0019] The lower driving end and the lower end are provided with a group of lower connecting shafts for transmitting the motor power, the lower end of the lower connecting shaft is provided with a group of connecting flanges for connecting and fixing with the torque amplifier, the lower end of the connecting flange is provided with a group of internal reinforcement disks for improving the connection torque between the connecting flange and the torque amplifier, the lower end of the internal reinforcement disk is provided with a group of torque amplifiers for amplifying the rotational torque of the lower connecting shaft, the motor power can be transmitted by using the lower connecting shaft, the connecting flange can be connected and fixed with the torque amplifier by using the connecting flange, and the connection torque between the connecting flange and the torque amplifier can be improved by using the torque amplifier.

[0020] As a preferred embodiment, the lower end of the torque amplifier is also provided with a set of connecting flanges for connecting to the lower connecting column, and the connection methods of the two sets of connecting flanges on the upper and lower sides of the torque amplifier are consistent;

[0021] The lower end of the connecting flange is provided with a group of lower connecting columns for transmitting the large torque power transmitted by the torque amplifier, a group of lower positioning seats for stabilizing the rotation of the lower connecting column are provided on the outside of the middle position of the lower connecting column, a group of lower support seats for maintaining the directional rotation of the lower connecting column are provided on the outside of the lower positioning seat, a group of inner grooves for maintaining the engagement of the lower positioning seat are provided inside the lower support seat, and a group of limiting bearings are provided at the connection between the lower positioning seat and the lower connecting column, which can transmit the large torque power transmitted by the torque amplifier by using the lower connecting column, and can maintain the rotation stability of the lower connecting column by using the lower positioning seat.

[0022] As a preferred embodiment, the replacement base includes a rear support beam and a front transmission frame, the rear support beam is located at the rear side of the replacement base, and two groups of rear support beams are provided, and a group of limit plates for movably limiting the movable seat are provided on the left and right sides of the upper ends of the two groups of rear support beams;

[0023] A group of lower moving rails for moving the moving seat forward and backward is provided at the lower end of each group of limiting plates, and a group of moving seats for driving the internal fixed vertical frame, the front transmission frame and the rear transmission frame to move are provided at the upper end of each group of lower moving rails. The moving seats are respectively connected and fixed to the lower ends of the left and right sides of the rear transmission frame and the lower ends of the left and right sides of the front transmission frame by bolts. The front transmission frame and the rear transmission frame have the same specifications and are arranged in an opposite manner.

[0024] The rear side of the front transmission frame and the front side of the rear transmission frame are both provided with several groups of internal rotating shafts for driving the aviation accessories to move left and right, and a group of internal shafts for driving the aviation accessories to move left and right is provided inside each two groups of horizontally arranged internal rotating shafts. A group of screw moving groups for actively providing forward and backward movement potential energy is provided at the lower end of the middle position of the front transmission frame and the rear transmission frame, and a group of carrier plates for supporting the internal fixed vertical frame are provided at the rear side of the upper end of the screw moving group. A group of internal fixed vertical frames for supporting the lifting electric cylinder is provided at the upper end of the rear side of the carrier plates. A group of lifting electric cylinders for adjusting the height of the front transmission frame and the rear transmission frame are provided at the rear side of the internal fixed vertical frame. The screw moving group can be used to actively provide forward and backward movement potential energy for the front transmission frame and the rear transmission frame, and the height of the front transmission frame and the rear transmission frame can be adjusted by using the lifting electric cylinder.

[0025] As a preferred embodiment, the lower card seat includes an upper frame and external positioning teeth.

[0026] As a preferred embodiment, the upper frame is located at the upper end of the lower card seat, and the cross section of the upper frame is a semicircular ring structure. A group of upper fixing holes for interlocking with the force guide columns are provided inside the left and right ends of the upper frame, and the force guide columns and the upper frame are connected and fixed by bolts. The lower end of each group of upper fixing holes corresponds to a group of force guide columns for connection and fixation, and a group of extrusion springs for supporting the force guide columns are provided on the outside of the force guide columns;

[0027] The lower end of the extrusion spring is provided with a group of external positioning frames for supporting the lower end of the extrusion spring, and the outer side of the rear end of the external positioning frame is provided with a group of side connecting seats for connecting and fixing the external positioning frame, and the side connecting seats are fixed to the external positioning frame by bolts. The lower ends of the external positioning frame and the side connecting seats are each provided with a group of support bases for supporting and connecting their lower ends, and the lower end of each group of the guide columns is provided with a group of positioning seat rods for positioning the internal nuts of the aviation accessory casing, and the lower ends of the positioning seat rods are provided with a group of positioning holes corresponding to the positions of the positioning seat rods;

[0028] There are two groups of positioning holes, and the two groups of positioning holes are mutually positioned and embedded with the lower end of a group of positioning seat rods. A group of upper positioning sleeves for positioning the aviation accessory casing components are provided on the outside of the two groups of positioning holes. A group of upper embedding seats for mutually embedding with the upper positioning sleeves are provided at the lower end of the upper embedding seat. A group of lower positioning plates for being embedded and connected with the lower end of the upper embedding seat and maintaining positioning are provided at the lower end of the upper embedding seat. Several groups of side support inserts for positioning the lower positioning plate and supporting the lower positioning plate on the outside are evenly distributed and fixed on the outside of the lower positioning plate.

[0029] The lower end of the lower positioning plate is provided with a group of nuts for locking the internal nuts of the aviation accessory casing; the outer side of the aviation accessory casing is provided with a group of external spiral threads for threaded engagement with the bottom of the lower card seat for positioning; the inner side of the upper end of the upper engaging seat is evenly distributed with four groups of internal locking grooves for engaging with the internal nuts of the aviation accessory casing that need to be locked; each group of the internal engaging grooves is provided with a group of connecting inner bolts for connecting and fixing the upper engaging seat to the lower positioning plate; the inner side of the lower positioning plate is provided with a group of fastening inner cavities for placing the bottom of the nut;

[0030] A group of internal positioning sensors for accurately positioning the nut position is provided in the middle position inside the fastening inner cavity, a group of internal positioning cone seats for limiting the position of the internal positioning sensor are provided on the outside of the internal positioning sensor, a group of internal embedding grooves for mutual engagement with the lower end of the lower positioning plate are provided on the outside of the upper end of the internal positioning cone seat, and several groups of external positioning teeth for mutual engagement and positioning of the inner side of the aviation accessory casing are provided on the outside of the internal positioning cone seat.

[0031] A method for aligning the holes of a slotted nut lock piece of an aviation accessory casing comprises the following steps: first, a worker places the aviation accessory casing whose nut needs to be tightened on the inner side of the lower end of a lower holder, screws the outer spiral thread into the inner thread of the lower end of the lower holder, and then places the nut to be tightened on the inner side of an upper positioning sleeve;

[0032] Then replace the screwing head corresponding to the size of the nut to be locked, and then the staff starts the upper electric cylinder, and drives the upper electric cylinder to squeeze the lower pressure rod and the holding seat to move the motor downward. After the motor is subjected to force, it drives the drive assembly to move downward as a whole, and drives the screwing head downward to make the screwing head contact with the nut to be locked. Then, the screwing head is driven by the drive assembly to rotate to lock the nut and the aviation accessory casing.

[0033] After adopting the above technical solution, the beneficial effects of the present invention are as follows: by using the support platform to limit the rotation balance of the drive assembly, it can be connected to the middle position of the drive assembly by using the limit bearing, by using the lower screwing head to tighten the slotted nut of the aviation accessory casing, and by using the rear support plate to install and support the slide rail, the lower card seat and the replacement base;

[0034] The support height of the support platform can be adjusted by using the rear support electric cylinder, the force guide plate can be used to connect and fix with the support platform and drive the support platform to move synchronously, the motor power can be transmitted by using the lower connecting shaft, the connecting flange can be used to connect and fix with the torque amplifier, and the torque amplifier can be used to increase the connection torque between the connecting flange and the torque amplifier;

[0035] The high torque power transmitted by the torque amplifier is transmitted by using the lower connecting column, the rotation stability of the lower connecting column can be maintained by using the lower positioning seat, the front and rear transmission frames are actively provided with moving potential energy by using the screw moving group, and the height of the front and rear transmission frames can be adjusted by using the lifting electric cylinder.

[0036] After adopting the above technical solution, the beneficial effect of this method is: by using the motor to drive the driving assembly to move downward as a whole after being subjected to force, and the driving assembly drives the screwing head to move downward and makes the screwing head contact with the nut to be locked, and then the driving assembly drives the screwing head to rotate to lock the nut and the aviation accessory casing. BRIEF DESCRIPTION OF THE DRAWINGS

[0037] In order to more clearly illustrate the embodiments of the present invention or the technical solutions in the prior art, the following briefly introduces the drawings required for use in the embodiments or the description of the prior art. Obviously, the drawings described below are only some embodiments of the present invention. For ordinary technicians in this field, other drawings can be obtained based on these drawings without paying any creative work.

[0038] Figure 1 This is a schematic diagram of a left oblique top view of a slotted nut lock plate hole alignment device for an aviation accessory casing according to the present invention;

[0039] Figure 2 This is a front and side structural diagram of a driving component and a motor of a slotted nut lock plate hole alignment device for an aviation accessory casing according to the present invention;

[0040] Figure 3 This is a schematic diagram of the structure of the force guide plate and the rear support electric cylinder in a slotted nut lock plate hole alignment device for an aviation accessory casing according to the present invention, viewed from the rear side;

[0041] Figure 4This is a schematic diagram of the front side top view of the lower clamping seat in a slotted nut lock piece hole alignment device for an aviation accessory casing according to the present invention;

[0042] Figure 5 This is a schematic diagram of the structure of the interior of a replacement base in a slotted nut lock piece hole alignment device for an aviation accessory casing according to the present invention, viewed from the left oblique front side;

[0043] Figure 6 This is a schematic diagram of the front side top view of an aviation accessory casing in a device for aligning slotted nut lock pieces of an aviation accessory casing according to the present invention;

[0044] Figure 7 This is a schematic diagram of the front side plan view of the inner positioning cone seat in the slotted nut lock piece hole alignment device of an aviation accessory casing of the present invention;

[0045] Figure 8 For the present invention Figure 2 A magnified view of the structure at center A;

[0046] In the figure: 1-upper electric cylinder, 2-upper support frame, 3-lower pressure rod, 4-pressing seat, 5-motor, 6-drive assembly, 7-support platform, 8-lower screwing head, 9-rear slide, 10-slide rail, 11-rear support plate, 12-lower clamping seat, 13-rear support frame, 14-force guide plate, 15-rear support electric cylinder, 16-replaceable base;

[0047] 61-lower driving end, 62-lower connecting shaft, 63-connecting flange, 64-inner reinforcement plate, 65-torque amplifier, 66-lower connecting column, 67-lower positioning seat, 68-lower support seat;

[0048] 16a-rear support beam, 16b-limiting plate, 16c-lower moving rail, 16d-moving seat, 16e-side support frame plate, 16f-rear transmission frame, 16g-internal fixed vertical frame, 16h-lifting electric cylinder, 16i-internal rotating shaft, 16j-screw moving group, 16k-front transmission frame;

[0049] 12a-upper frame, 12b-upper fixing hole, 12c-force guide column, 12d-extrusion spring, 12e-positioning seat rod, 12f-positioning hole, 12g-external positioning frame, 12h-side connecting seat, 12i-support base, 12j-upper fitting seat, 12k-lower positioning plate, 12l-external bolt thread, 12m-inner embedded groove, 12n-connecting inner bolt, 12o-inner positioning cone seat, 12p-inner positioning sensor, 12q-side support plug plate, 12r-inner locking groove, 12s-external positioning gear. DETAILED DESCRIPTION

[0050] The following will clearly and completely describe the technical solutions in the embodiments of the present invention in conjunction with the accompanying drawings. Obviously, the described embodiments are only part of the embodiments of the present invention, not all of the embodiments. All other embodiments obtained by ordinary technicians in this field based on the embodiments of the present invention without making any creative efforts shall fall within the scope of protection of the present invention.

[0051] See also Figures 1-8 A slotted nut lock plate hole alignment device for an aviation accessory casing includes: an upper electric cylinder 1, a drive assembly 6, a lower clamping seat 12, and a replacement base 16. A set of lower pressure rods 3 for controlling the upward and downward movement of a holding seat 4 is provided at the lower end of the upper electric cylinder 1;

[0052] A set of holding seats 4 for controlling the up and down positions of the motor 5 are provided at the lower end of the lower pressure rod 3. The holding seats 4 are fixed to the upper end of the motor 5 by bolts. A set of upper support frames 2 for supporting the upper electric cylinder 1 are provided on the outer side of the upper end of the lower pressure rod 3. A set of driving components 6 for transmitting power from the motor 5 are provided at the lower end of the motor 5.

[0053] A group of support platforms 7 for limiting the rotational balance of the drive assembly 6 are provided on the outside of the middle position of the drive assembly 6. The cross-section of the support platform 7 is a rectangular structure when viewed from above, and a circular inner groove is provided inside. A group of limit bearings for interconnecting with the middle position of the drive assembly 6 are provided inside the circular inner groove of the support platform 7. A group of lower screw-on heads 8 for tightening the slotted nuts of the aviation accessory casing are provided at the lower end of the drive assembly 6. The rotational balance of the drive assembly 6 can be limited by using the support platform 7, and the limit bearings can be used to interconnect with the middle position of the drive assembly 6.

[0054] See also Figure 1-Figure 3 , the upper end of the lower screwing head 8 is provided with an internal connecting thread, the lower screwing head 8 and the lower end of the driving assembly 6 are screwed together, and the rear side of the upper support frame 2 is provided with several groups of rear slide seats 9 for driving the upper support frame 2 to move up and down;

[0055] Two groups of slide rails 10 are provided on the rear side of several groups of rear slides 9 for limiting the up and down movement of the rear slides 9. Several groups of rear slides 9 are movably engaged with the two groups of slide rails 10 respectively. There are two groups of slide rails 10, and the two groups of slide rails 10 are parallel. The two groups of slide rails 10 are connected and fixed to the rear support plate 11 by bolts, and the slotted nuts of the aviation accessory casing can be tightened by using the lower screw-on head 8.

[0056] A set of rear support plates 11 for mounting and supporting the slide rails 10, the lower card seat 12 and the replacement base 16 are provided on the rear side of the two sets of slide rails 10. Two sets of rear support frames 13 for supporting the rear support plates 11 are provided on the rear side of the rear support plates 11.

[0057] There are two groups of rear support frames 13, and a group of rear support electric cylinders 15 for adjusting the support height of the support platform 7 is provided at the middle position inside the two groups of rear support frames 13. The upper end of the rear support electric cylinder 15 is provided with a group of force guide plates 14 for connecting and fixing with the support platform 7 and driving the support platform 7 to move synchronously. The lower card seat 12 is a detachable structure. The replacement base 16 and the lower card seat 12 are installed at the same position. The replacement base 16 and the lower card seat 12 are installed according to the required functions. The slide rail 10, the lower card seat 12 and the replacement base 16 can be installed and supported by using the rear support plate 11. The rear support electric cylinder 15 can be used to adjust the support height of the support platform 7. The force guide plate 14 can be used to connect and fix with the support platform 7 and drive the support platform 7 to move synchronously.

[0058] See also Figures 1-8 When the screw thread 12 is tightened, the screw thread 12 is tightened to the inner side of the lower end of the lower clamping seat 12, and the screw thread 12 is screwed into the inner side of the lower end of the lower clamping seat 12 to be connected and positioned. Then, the nut to be locked is placed on the inner side of the upper positioning sleeve, and then the screwing head corresponding to the size of the nut to be locked is replaced. Then, the staff starts the upper electric cylinder 1, and the upper electric cylinder 1 drives the extrusion lower pressure rod 3 and the holding seat 4 to move the motor 5 downward. After the motor 5 is subjected to force, it drives the driving component 6 to move downward as a whole, and drives the screwing head to move downward and make the screwing head contact with the nut to be locked. Then, the screwing head is driven by the driving component 6 to rotate so that the nut and the aviation accessory casing are locked and connected, thereby completing the locking process of the slotted nut of the aviation accessory casing. At the same time, when the locking process is completed, the staff can remove the lower clamping seat 12 and install the replacement base 16 at the lower end of the rear support plate 11, so as to transmit the aviation accessory casing to the external process line in batches.

[0059] See also Figure 1-Figure 3 as well as Figure 8 The driving assembly 6 includes a lower driving end 61, a torque amplifier 65 and a lower support seat 68. The lower driving end 61 is arranged at the lower end of the motor 5 and is connected to the internal power of the motor 5. The cross section of the lower driving end 61 is a circular structure, and the lower driving end 61 is an active rotating structure.

[0060] The lower driving end 61 and the lower end are provided with a group of lower connecting shafts 62 for transmitting the power of the motor 5. The lower end of the lower connecting shaft 62 is provided with a group of connecting flanges 63 for connecting and fixing with the torque amplifier 65. The lower end of the connecting flange 63 is provided with a group of internal reinforcement plates 64 for increasing the connection torque between the connecting flange 63 and the torque amplifier 65. The lower end of the internal reinforcement plate 64 is provided with a group of torque amplifiers 65 for amplifying the rotational torque of the lower connecting shaft 62. The power of the motor 5 can be transmitted by using the lower connecting shaft 62, the connecting flange 63 can be connected and fixed to the torque amplifier 65, and the torque amplifier 65 can be used to increase the connection torque between the connecting flange 63 and the torque amplifier 65.

[0061] The lower end of the torque amplifier 65 is also provided with a set of connecting flanges 63 for connecting to the lower connecting column 66, and the two sets of connecting flanges 63 are connected in the same manner on the upper and lower sides of the torque amplifier 65;

[0062] A group of lower connecting columns 66 for transmitting the high torque power transmitted by the torque amplifier 65 are provided at the lower end of the lower connecting flange 63, and a group of lower positioning seats 67 for stabilizing the rotation of the lower connecting column 66 are provided on the outer side of the middle position of the lower connecting column 66. A group of lower support seats 68 for maintaining the directional rotation of the lower connecting column 66 are provided on the outer side of the lower positioning seat 67. A group of inner grooves for maintaining the engagement of the lower positioning seat 67 are provided inside the lower support seat 68, and a group of limit bearings are provided at the connection between the lower positioning seat 67 and the lower connecting column 66. The high torque power transmitted by the torque amplifier 65 can be transmitted by using the lower connecting column 66, and the rotation stability of the lower connecting column 66 can be maintained by using the lower positioning seat 67.

[0063] See also Figures 1-8As the second embodiment of the present invention: based on the explanation in the first embodiment, further, when the electric cylinder controls the motor 5 to move downward, the motor 5 drives the lower driving end 61 to rotate, and the lower driving end 61 drives the lower connecting shaft 62 and the upper connecting flange 63 to rotate. Since the lower end of the torque amplifier 65 is also provided with a group of connecting flanges 63 for connecting with the lower connecting column 66, and the two groups of connecting flanges 63 are connected to the upper and lower sides of the torque amplifier 65 in the same manner, the rotational force of the lower connecting shaft 62 is amplified by the torque amplifier 65, and the torque is amplified by the torque amplifier 65. The high torque power is transmitted through the lower connecting column 66, and the two sets of connecting flanges 63 and the two sets of inner reinforcement plates 64 strengthen the connection effect with the torque amplifier 65, thereby preventing the torque at the lower end of the torque amplifier 65 from being too large, resulting in a decrease in the connection effect and causing the shaft to break. After the lower connecting column 66 rotates, it can drive the lower screw-on head 8 to screw and lock the nut. Since a set of limit bearings is provided at the connection between the lower positioning seat 67 and the lower connecting column 66, the lower positioning seat 67 can be used to keep the lower connecting column 66 stable in rotation, thereby improving the stable locking effect of the nut.

[0064] See also Figure 1-Figure 3 as well as Figure 5 The replacement base 16 includes a rear support beam 16a and a front transmission frame 16k. The rear support beam 16a is located at the rear side of the replacement base 16. There are two groups of rear support beams 16a, and a group of limit plates 16b for movably limiting the movable seat 16d are provided on the left and right sides of the upper ends of the two groups of rear support beams 16a.

[0065] A set of lower movable rails 16c for moving the movable seat 16d forward and backward is provided at the lower end of each set of limiting plates 16b. A set of movable seats 16d for driving the internal fixed vertical frame 16g, the front transmission frame 16k, and the rear transmission frame 16f to move are provided at the upper end of each set of limiting plates 16b. The movable seats 16d are respectively connected and fixed to the lower ends of the left and right sides of the rear transmission frame 16f and the lower ends of the left and right sides of the front transmission frame 16k by bolts. The front transmission frame 16k and the rear transmission frame 16f have the same specifications and are arranged in an opposing manner.

[0066] The rear side of the front transmission frame 16k and the front side of the rear transmission frame 16f are both provided with several groups of inner rotating shafts 16i for driving the aviation accessories to move left and right, and each two groups of horizontally arranged inner rotating shafts 16i are equipped with a group of inner shafts for driving the aviation accessories to move left and right. The lower end of the middle position between the front transmission frame 16k and the rear transmission frame 16f is provided with a group of screw moving groups 16j for actively providing them with moving potential energy back and forth, and the rear end of the screw moving group 16j is provided with a group of carrier plates for supporting the internal fixed vertical frame 16g. The upper end of the rear side of the carrier plate is provided with a group of internal fixed vertical frames 16g for supporting the lifting electric cylinder 16h, and the rear side of the internal fixed vertical frame 16g is provided with a group of lifting electric cylinders for adjusting the height of the front transmission frame 16k and the rear transmission frame 16f. The screw moving group 16j can be used to actively provide moving potential energy back and forth to the front transmission frame 16k and the rear transmission frame 16f can be adjusted in height by using the lifting electric cylinder.

[0067] See also Figure 1-Figure 3 as well as Figure 5 As the third embodiment of the present invention: based on the explanation in the first embodiment, further, when the staff completes the nut locking of the aviation accessory casing, the staff can directly release the connection effect of the lower clamping seat 12 from the rear support plate 11, and fix the replacement base 16 to the rear support plate 11 by bolts. Subsequently, since the rear side of the front transmission frame 16k and the front side of the rear transmission frame 16f are provided with several groups of inner rotating shafts 16i for driving the aviation accessories to move left and right, each two groups of horizontally arranged inner rotating shafts 16i are provided with a group of inner shafts for driving the aviation accessories to move left and right. By using multiple inner shafts, multiple aviation accessory casings can be exported in batches to an external processing flow line. At the same time, since a group of carrier plates for supporting the internal fixed vertical frame 16g is provided on the rear side of the upper end of the screw moving group 16j, a group of internal fixed vertical frames 16g for supporting the lifting electric cylinder 16h are provided on the upper end of the rear side of the carrier plate. The lifting electric cylinder 16h can adjust the height of the front transmission frame 16k and the rear transmission frame 16f so as to transport aviation accessory casings of different heights.

[0068] See also Figure 1-Figure 4 as well as Figure 6-Figure 7 The lower card seat 12 includes an upper frame 12a and an outer positioning tooth 12s.

[0069] The upper frame 12a is located at the upper end of the lower base 12. The cross section of the upper frame 12a is a semicircular ring structure. A group of upper fixing holes 12b for interlocking with the force guide columns 12c are provided inside the left and right ends of the upper frame 12a. The force guide columns 12c and the upper frame 12a are connected and fixed by bolts. The lower end of each group of upper fixing holes 12b corresponds to a group of force guide columns 12c for connection and fixation. A group of extrusion springs 12d for supporting the force guide columns 12c are provided on the outside of the force guide columns 12c.

[0070] A group of external positioning frames 12g for supporting the lower end of the extrusion spring 12d is provided at the lower end of the extrusion spring 12d. A group of side connecting seats 12h for connecting and fixing the external positioning frames 12g are provided on the outer side of the rear end of the external positioning frames 12g. The side connecting seats 12h are fixed to the external positioning frames 12g by bolts. The lower ends of the external positioning frames 12g and the side connecting seats 12h are each provided with a group of supporting bases 12i for supporting and connecting their lower ends. The lower end of each group of guide columns 12c is provided with a group of positioning seat rods 12e for positioning nuts inside the aviation accessory casing. The lower end of the positioning seat rods 12e is provided with a group of positioning holes 12f corresponding to the positions of the positioning seat rods 12e.

[0071] There are two groups of positioning holes 12f, and both groups of positioning holes 12f are positioned and engaged with the lower ends of a group of positioning seat rods 12e. A group of upper positioning sleeves for positioning the aviation accessory casing components are provided on the outside of the two groups of positioning holes 12f. A group of upper engaging seats 12j for engaging with the upper positioning sleeves are provided at the lower ends of the upper positioning sleeves. A group of lower positioning plates 12k for engaging with the lower ends of the upper engaging seats 12j and maintaining positioning are provided at the lower ends of the upper engaging seats 12j. Several groups of side support inserts 12q for positioning the lower positioning plates 12k and supporting the lower positioning plates 12k are evenly distributed and fixed on the outside of the lower positioning plates 12k.

[0072] A group of external spiral threads 12l for threaded engagement with the bottom of the lower holder 12 are provided on the outer side of the lower positioning plate 12k for locking the internal nuts of the aviation accessory casing. Four groups of internal embedding grooves 12m for interlocking the internal nuts of the aviation accessory casing that need to be locked are evenly distributed on the inner side of the upper embedding seat 12j. Each group of internal embedding grooves 12m is provided with a group of connecting inner bolts 12n for connecting and fixing the upper embedding seat 12j to the lower positioning plate 12k. A group of fastening inner cavities for placing the bottom of the nut are provided on the inner side of the lower positioning plate 12k.

[0073] A group of internal positioning sensors 12p for accurately positioning the nut position is provided in the middle position inside the fastening inner cavity, a group of internal positioning cone seats 12o for limiting the position of the internal positioning sensor 12p are provided on the outside of the internal positioning sensor 12p, a group of internal locking grooves 12r for mutual engagement with the lower end of the lower positioning plate 12k are provided on the outside of the upper end of the internal positioning cone seat 12o, and several groups of external positioning teeth 12s for mutual engagement and positioning of the inner side of the aviation accessory casing are provided on the outside of the internal positioning cone seat 12o.

[0074] See also Figures 1-8As the fourth embodiment of the present invention: based on the description in the first and second embodiments, further, when the staff is locking the nut and the aviation accessory casing, the lower screwing head 8 drives the nut to rotate downward and screws it. When the staff installs the nut, the nut is placed inside the upper fitting seat 12j. Since the inner side of the upper end of the upper fitting seat 12j is evenly distributed with four groups of inner fitting grooves 12m for fitting the nuts inside the aviation accessory casing that need to be locked, each group of inner fitting grooves 12m is provided with a group of connecting inner bolts 12n for connecting and fixing the upper fitting seat 12j to the lower positioning plate 12k, the nut and the upper fitting seat are fixed. When the interior of 12j is in an engaged state, the nut rotates together with the upper positioning sleeve until the two groups of positioning holes 12f are fully engaged with the lower ends of a group of positioning seat rods 12e respectively, and its two groups of extrusion springs 12d release the two groups of lower pressure rods 3 respectively to support their positions and perform brief positioning. At the same time, since a group of internal positioning sensors 12p for accurately positioning the nut position is provided in the middle position inside the fastening inner cavity, when the nut is squeezed and threaded with the aviation accessory, the height position of the nut changes, and its internal positioning sensor 12p can effectively monitor the screwing position of the nut, thereby determining whether the nut installation is complete.

[0075] See also Figures 1-8 A method for aligning the slotted nut locking plate holes of an aviation accessory casing. First, a worker places the aviation accessory casing whose nut needs to be tightened on the inner side of the lower end of the lower clamping seat 12, and screws the outer spiral thread 12l into the inner thread of the lower end of the lower clamping seat 12 for positioning. Then, the nut to be locked is placed on the inner side of the upper positioning sleeve.

[0076] Then replace the screwing head corresponding to the size of the nut to be locked, and then the staff starts the upper electric cylinder 1, and drives the upper electric cylinder 1 to squeeze the lower pressure rod 3 and the holding seat 4 to move the motor 5 downward. After the motor 5 is subjected to force, it drives the driving component 6 to move downward as a whole, and drives the driving component 6 to drive the screwing head downward and make the screwing head contact with the nut to be locked. Then, the screwing head is driven by the driving component 6 to rotate to lock the nut and the aviation accessory casing.

[0077] The above description is only a preferred embodiment of the present invention and is not intended to limit the present invention. Any modifications, equivalent substitutions, improvements, etc. made within the spirit and principles of the present invention should be included in the scope of protection of the present invention.

Claims

1. A slotted nut lock plate hole alignment device for an aviation accessory casing, comprising: An upper electric cylinder (1), a driving assembly (6), a lower clamping seat (12) and a replacement base (16), characterized in that: a group of lower pressing rods (3) for controlling the upward and downward movement of the holding seat (4) are provided at the lower end of the upper electric cylinder (1); The lower end of the lower pressure rod (3) is provided with a group of pressure holding seats (4) for controlling the upper and lower positions of the motor (5), the pressure holding seats (4) and the upper end of the motor (5) are fixed by bolts, the outer side of the upper end of the lower pressure rod (3) is provided with a group of upper support frames (2) for supporting the upper electric cylinder (1), and the lower end of the motor (5) is provided with a group of driving components (6) for transmitting the power of the motor (5); A group of support platforms (7) for limiting the rotational balance of the drive assembly (6) are provided on the outer side of the middle position of the drive assembly (6); the cross section of the support platform (7) is a rectangular structure when viewed from above, and a circular inner groove is provided inside the support platform (7); a group of limit bearings for interconnecting with the middle position of the drive assembly (6) are provided inside the circular inner groove of the support platform (7); and a group of lower screwing heads (8) for tightening the slotted nuts of the aviation accessory casing are provided at the lower end of the drive assembly (6); The upper end of the lower screw-on head (8) is provided with an internal connecting thread, and the lower end of the lower screw-on head (8) and the lower end of the driving assembly (6) are screw-connected with each other, and the rear side of the upper support frame (2) is provided with a plurality of groups of rear slide seats (9) for driving the upper support frame (2) to move up and down; Two groups of slide rails (10) are provided on the rear side of the plurality of groups of rear slide seats (9) for limiting the upward and downward movement of the rear slide seats (9). The plurality of groups of rear slide seats (9) are movably engaged with the two groups of slide rails (10). The slide rails (10) are provided in two groups, and the two groups of slide rails (10) are in a parallel state. The two groups of slide rails (10) are connected and fixed to the rear support plate (11) by bolts. A set of rear support plates (11) for mounting and supporting the slide rails (10), the lower card seat (12) and the replacement base (16) are provided on the rear side of the two sets of slide rails (10); and two sets of rear support frames (13) for supporting the rear support plates (11) are provided on the rear side of the rear support plates (11); The rear support frame (13) is provided with two groups, and a group of rear support electric cylinders (15) for adjusting the support height of the support platform (7) is provided at the middle position of the inner side of the two groups of rear support frames (13), and a group of guide plates (14) for connecting and fixing with the support platform (7) and driving the support platform (7) to move synchronously are provided at the upper end of the rear support electric cylinder (15). The lower card seat (12) is a detachable structure, and the replacement base (16) and the lower card seat (12) are installed at the same position. The replacement base (16) and the lower card seat (12) are installed in a selective manner according to the required function. The lower card seat (12) includes an upper frame (12a) and external positioning teeth (12s); The upper frame (12a) is located at the upper end of the lower seat (12), and the cross section of the upper frame (12a) is a semicircular ring structure. A group of upper fixing holes (12b) for interlocking with the force guide columns (12c) are provided inside the left and right ends of the upper frame (12a), and the force guide columns (12c) and the upper frame (12a) are connected and fixed by bolts. The lower end of each group of upper fixing holes (12b) corresponds to a group of force guide columns (12c) for connection and fixation. A group of extrusion springs (12d) for supporting the force guide columns (12c) are provided on the outside of the force guide columns (12c); The lower end of the extrusion spring (12d) is provided with a group of external positioning frames (12g) for supporting the lower end of the extrusion spring (12d); the outer side of the rear end of the external positioning frame (12g) is provided with a group of side connecting seats (12h) for connecting and fixing the external positioning frame (12g); the side connecting seats (12h) and the external positioning frame (12g) are connected and fixed by bolts; the lower ends of the external positioning frame (12g) and the side connecting seats (12h) are provided with a group of supporting bases (12i) for supporting and connecting their lower ends; the lower end of each group of the guide columns (12c) is provided with a group of positioning seat rods (12e) for positioning nuts inside the aviation accessory casing; the lower end of the positioning seat rods (12e) is provided with a group of positioning holes (12f) corresponding to the positions of the positioning seat rods (12e); There are two groups of positioning holes (12f), and both groups of positioning holes (12f) are mutually positioned and engaged with the lower end of a group of positioning seat rods (12e). A group of upper positioning sleeves for positioning the aviation accessory casing components are provided on the outside of the two groups of positioning holes (12f). The lower ends of the upper positioning sleeves are provided with a group of upper engaging seats (12j) for mutually engaging with the upper positioning sleeves. The lower ends of the upper engaging seats (12j) are provided with a group of lower positioning plates (12k) for engaging with the lower ends of the upper engaging seats (12j) and maintaining positioning. Several groups of side support inserts (12q) for positioning the lower positioning plate (12k) and supporting the lower positioning plate (12k) on the outside are evenly distributed and fixed on the outside of the lower positioning plate (12k). The lower end of the lower positioning plate (12k) is provided with a group of nuts for locking the aviation accessory casing; the outer side of the aviation accessory casing is provided with a group of external spiral threads (12l) for threaded engagement with the bottom of the lower clamping seat (12); the inner side of the upper end of the upper engaging seat (12j) is evenly distributed with four groups of internal embedding grooves (12m) for interengaging nuts inside the aviation accessory casing that need to be locked; each group of the internal embedding grooves (12m) is provided with a group of connecting inner bolts (12n) for connecting and fixing the upper engaging seat (12j) and the lower positioning plate (12k); the inner side of the lower positioning plate (12k) is provided with a group of fastening inner cavities for placing the bottom of the nut; A group of internal positioning sensors (12p) for accurately positioning the nut position is provided at the middle position inside the fastening inner cavity, a group of internal positioning cone seats (12o) for limiting the position of the internal positioning sensor (12p) are provided on the outside of the internal positioning sensor (12p), a group of internal locking grooves (12r) for interlocking with the lower end of the lower positioning plate (12k) are provided on the outside of the upper end of the internal positioning cone seat (12o), and a plurality of groups of external positioning teeth (12s) for interlocking and positioning the inner side of the aviation accessory casing are provided on the outside of the internal positioning cone seat (12o).

2. The device for aligning slotted nut lock plate holes of an aviation accessory casing according to claim 1, characterized in that: The driving assembly (6) includes a lower driving end (61), a torque amplifier (65) and a lower support seat (68); the lower driving end (61) is arranged at the lower end of the motor (5) and is connected to the internal power of the motor (5); the cross section of the lower driving end (61) is a circular structure; the lower driving end (61) is an active rotating structure; The lower driving end (61) and the lower end are provided with a group of lower connecting shafts (62) for transmitting the power of the motor (5), the lower end of the lower connecting shaft (62) is provided with a group of connecting flanges (63) for connecting and fixing with the torque amplifier (65), the lower end of the connecting flange (63) is provided with a group of inner reinforcing disks (64) for increasing the connecting torque between the connecting flange (63) and the torque amplifier (65), and the lower end of the inner reinforcing disk (64) is provided with a group of torque amplifiers (65) for amplifying the rotational torque of the lower connecting shaft (62).

3. The device for aligning the slotted nut lock plate holes of an aviation accessory casing according to claim 2, characterized in that: The lower end of the torque amplifier (65) is also provided with a set of connecting flanges (63) for connecting to the lower connecting column (66), and the two sets of connecting flanges (63) are connected to the upper and lower sides of the torque amplifier (65) in the same manner; The lower end of the connecting flange (63) is provided with a group of lower connecting columns (66) for transmitting the large torque power transmitted by the torque amplifier (65), and the outer side of the middle position of the lower connecting column (66) is provided with a group of lower positioning seats (67) for stabilizing the rotation of the lower connecting column (66). The outer side of the lower positioning seat (67) is provided with a group of lower support seats (68) for maintaining the directional rotation of the lower connecting column (66), and the interior of the lower support seat (68) is provided with a group of inner grooves for maintaining the engagement of the lower positioning seat (67). A group of limit bearings are provided at the connection between the lower positioning seat (67) and the lower connecting column (66).

4. The device for aligning slotted nut lock pieces of an aviation accessory casing according to claim 1, characterized in that: The replacement base (16) includes a rear support beam (16a) and a front transmission frame (16k), wherein the rear support beam (16a) is located at the rear side of the replacement base (16), and two groups of the rear support beams (16a) are provided, and a group of limiting plates (16b) for movably limiting the movable seat (16d) are provided on the left and right sides of the upper ends of the two groups of rear support beams (16a); A group of lower moving rails (16c) for moving the moving seat (16d) forward and backward is provided at the lower end of each group of the limiting plates (16b), and a group of moving seats (16d) for driving the internal fixed vertical frame (16g), the front transmission frame (16k) and the rear transmission frame (16f) to move are provided at the upper end of each group of the limiting plates (16b). The moving seats (16d) are respectively connected and fixed to the lower ends of the left and right sides of the rear transmission frame (16f) and the lower ends of the left and right sides of the front transmission frame (16k) by bolts. The front transmission frame (16k) and the rear transmission frame (16f) have the same specifications, and the front transmission frame (16k) and the rear transmission frame (16f) are arranged in an opposite manner. The rear side of the front transmission frame (16k) and the front side of the rear transmission frame (16f) are both provided with a plurality of groups of inner rotating shafts (16i) for driving the aviation accessories to move left and right. Each two groups of horizontally arranged inner rotating shafts (16i) are provided with a group of inner shafts for driving the aviation accessories to move left and right. A group of screw moving groups (16j) for actively providing forward and backward movement potential energy to the front transmission frame (16k) and the rear transmission frame (16f) are provided at the lower end of the middle position. A group of carrier plates for supporting the internal fixed vertical frame (16g) are provided at the rear side of the upper end of the carrier plate. A group of internal fixed vertical frames (16g) for supporting the lifting electric cylinder (16h) are provided at the upper end of the rear side of the carrier plate. A group of lifting electric cylinders for adjusting the height of the front transmission frame (16k) and the rear transmission frame (16f) are provided at the rear side of the internal fixed vertical frame (16g).

5. A method for aligning slotted nut locking plate holes in an aviation accessory casing according to any one of claims 1 to 4, characterized in that: First, the staff places the aviation accessory casing whose nut needs to be tightened on the inner side of the lower end of the lower holder (12), and screws the outer spiral thread (12l) with the inner thread of the lower end of the lower holder (12) to connect and position it, and then places the nut that needs to be locked on the inner side of the upper positioning sleeve; Then, the screwing head corresponding to the size of the nut to be locked is replaced, and then the staff starts the upper electric cylinder (1), and the upper electric cylinder (1) drives the extrusion lower pressure rod (3) and the pressure holding seat (4) to move the motor (5) downward. After the motor (5) is subjected to force, it drives the driving component (6) to move downward as a whole, and the driving component (6) drives the screwing head to move downward and makes the screwing head contact with the nut to be locked. Then, the screwing head is driven by the driving component (6) to rotate so that the nut is locked and connected with the aviation accessory casing.

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