CN116638296B - Device and method for disassembling and assembling connecting nuts in shaft cavity of aero-engine - Google Patents
Device and method for disassembling and assembling connecting nuts in shaft cavity of aero-engine Download PDFInfo
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- CN116638296B CN116638296B CN202310443421.0A CN202310443421A CN116638296B CN 116638296 B CN116638296 B CN 116638296B CN 202310443421 A CN202310443421 A CN 202310443421A CN 116638296 B CN116638296 B CN 116638296B
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23P—METAL-WORKING NOT OTHERWISE PROVIDED FOR; COMBINED OPERATIONS; UNIVERSAL MACHINE TOOLS
- B23P19/00—Machines for simply fitting together or separating metal parts or objects, or metal and non-metal parts, whether or not involving some deformation; Tools or devices therefor so far as not provided for in other classes
- B23P19/04—Machines for simply fitting together or separating metal parts or objects, or metal and non-metal parts, whether or not involving some deformation; Tools or devices therefor so far as not provided for in other classes for assembling or disassembling parts
- B23P19/06—Screw or nut setting or loosening machines
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23P—METAL-WORKING NOT OTHERWISE PROVIDED FOR; COMBINED OPERATIONS; UNIVERSAL MACHINE TOOLS
- B23P19/00—Machines for simply fitting together or separating metal parts or objects, or metal and non-metal parts, whether or not involving some deformation; Tools or devices therefor so far as not provided for in other classes
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Abstract
The application belongs to aeroengine spindle intra-cavity connection nut dismouting technical field, concretely relates to aeroengine spindle intra-cavity connection nut dismouting device, including automatic the tightening subassembly, automatic tightening subassembly further includes electronic folding spanner, vertical lifting mechanism, horizontal movement mechanism, horizontal slewing mechanism, wherein: the bottom end of the electric folding wrench is used for connecting the wrench head, the wrench head can be horizontally folded, and an industrial camera is arranged in a sleeve which is used for sleeving a connecting nut on the wrench head; the vertical lifting mechanism is used for lifting the electric folding wrench in the vertical direction and comprises a lifting platform, a lifting servo motor, a ball screw and a lifting guide post; the horizontal moving mechanism is used for moving the electric folding wrench in the horizontal direction and comprises a moving platform, a moving servo electric cylinder, a guide rail and a sliding block; the horizontal rotary mechanism is used for horizontally rotating the electric folding wrench and comprises a rotary platform, a rotary servo motor and a rotary support.
Description
Technical Field
The application belongs to the technical field of disassembly and assembly of nuts in the shaft cavity of an aeroengine, and particularly relates to a disassembly and assembly device and a disassembly and assembly method of nuts in the shaft cavity of an aeroengine.
Background
The aeroengine shaft cavity is internally connected with components by utilizing the connecting nut to be matched with the connecting screw, currently, the connecting nut in the shaft cavity is assembled and disassembled by manually utilizing a wrench, the opening of the shaft cavity is small, the whole is slender, under the condition that the internal space is small, the cap recognition of the connecting nut is difficult to be efficiently completed, the connecting nut is difficult to screw, the operation is inconvenient, and the collision damage is easily caused in the shaft cavity.
The present application has been made in view of the existence of the above-mentioned technical drawbacks.
It should be noted that the above disclosure of the background art is only for aiding in understanding the inventive concept and technical solution of the present invention, which is not necessarily prior art to the present application, and should not be used for evaluating the novelty and the creativity of the present application in the case where no clear evidence indicates that the above content has been disclosed at the filing date of the present application.
Disclosure of Invention
The invention aims to provide an aircraft engine shaft cavity inner connecting nut dismounting device and a method thereof, which overcome or alleviate the technical defects of at least one aspect of the prior art.
The technical scheme of the application is as follows:
the aspect provides an aircraft engine axle intracavity coupling nut dismouting device, including automatic tightening the subassembly, automatic tightening the subassembly further includes electronic folding spanner, vertical lifting mechanism, horizontal movement mechanism, horizontal slewing mechanism, wherein:
the bottom end of the electric folding wrench is used for connecting the wrench head, the wrench head can be horizontally folded, and an industrial camera is arranged in a sleeve which is used for sleeving a connecting nut on the wrench head;
the vertical lifting mechanism is used for lifting the electric folding wrench in the vertical direction and comprises a lifting platform, a lifting servo motor, a ball screw and a lifting guide post;
the horizontal moving mechanism is used for moving the electric folding wrench in the horizontal direction and comprises a moving platform, a moving servo electric cylinder, a guide rail and a sliding block;
the horizontal rotary mechanism is used for horizontally rotating the electric folding wrench and comprises a rotary platform, a rotary servo motor and a rotary support;
the electric folding wrench is positioned on a lifting platform among four lifting guide posts in the vertical lifting mechanism, one side of each lifting guide post is provided with a lifting servo motor and a ball screw, and the upper surfaces of the four lifting guide posts in the vertical lifting mechanism are connected with a lifting platform;
the lower parts of the four lifting guide posts in the vertical lifting mechanism are connected with a moving platform, four sliding blocks are fixed below the moving platform, and two groups of the four sliding blocks are respectively positioned above the two guide rails;
the movable servo electric cylinder is arranged on the rotary platform, a rotary support is arranged below the rotary platform, the rotary servo motor is arranged on one side of the rotary support, and the rotary support and the rotary servo motor are arranged on the fixed base.
According to at least one embodiment of the present application, in the above-mentioned aircraft engine shaft cavity connection nut dismounting device, D < D;
wherein,
d is the inner diameter of the fixed base;
d is the radial dimension of the shaft lumen opening.
According to at least one embodiment of the present application, in the above-mentioned device for assembling and disassembling an aircraft engine shaft cavity connection nut, a pressure-sensitive sensor is disposed on a wrench head surface.
According to at least one embodiment of the present application, in the above-mentioned assembly and disassembly device for connecting nuts in an aeroengine shaft cavity, the assembly and disassembly device further comprises a fixed platform, a torque calibrator, a roller car bottom and an electrical operation cabinet;
the fixed platform is connected to the roller bottom and used for fixing the automatic tightening assembly;
the torque calibrator is arranged on the automatic tightening assembly and used for calibrating the torque of the automatic tightening assembly;
the electric operation cabinet is connected to the roller car bottom, can record a program, is connected with the driving mechanism of the electric folding wrench, the vertical lifting mechanism, the horizontal moving mechanism and the horizontal rotating mechanism, and is connected with the industrial camera, and can screw each connecting nut one by one according to the recorded program under the condition that each connecting nut is uniformly distributed in the shaft cavity, so that the disassembly and assembly are completed.
According to at least one embodiment of the present application, in the above-mentioned assembling and disassembling device for connecting nuts in a shaft cavity of an aeroengine, the electric folding wrench comprises an electric wrench mechanism, a wrench head folding mechanism and a wrench rod positioning mechanism;
the electric spanner mechanism is used for electrically tightening nuts and consists of an electric spanner, a spanner extension bar and a spanner head;
the spanner head folding mechanism is used for folding the spanner head and consists of a folding mechanism servo electric cylinder, a guide sleeve, a guide pillar, a folding driving seat, a folding rod, a switching rod and the spanner head;
the spanner rod positioning mechanism is used for positioning and butting the spanner extension rod and the spanner head and consists of a positioning mechanism servo electric cylinder, a positioning mechanism driving seat, a positioning mechanism sliding block, a positioning mechanism guide rail, a positioning mechanism mounting seat and the spanner extension rod.
On the other hand, the invention provides a method for dismounting and mounting the connecting nut in the shaft cavity of the aero-engine, which is implemented based on any one of the connecting nut dismounting and mounting devices in the shaft cavity of the aero-engine, and comprises the following steps:
folding the spanner head into a vertical state by using an electric folding spanner;
the spanner head is sent into the shaft cavity along the vertical direction by the vertical lifting mechanism, and the position of the connecting nut is observed by an industrial camera, so that the spanner head descends to the vicinity of the connecting nut;
folding the spanner head into a horizontal state by using an electric folding spanner;
under the condition that the rotation center of the wrench head is positioned at the center of the reference circle of the connecting nut, the wrench head is driven by the horizontal moving mechanism to move horizontally, and is driven by the horizontal rotating mechanism to rotate, so that the wrench head is positioned above the rotor connecting nut;
photographing the outer circle of the connecting nut through an industrial camera, calculating and analyzing the position deviation of the sleeve axis and the connecting nut axis on the wrench head, driving the wrench head to horizontally move through a horizontal moving mechanism, driving the wrench head to rotate through a horizontal rotating mechanism, and adjusting to enable the sleeve axis and the connecting nut axis on the wrench head to be consistent;
the spanner head is driven by the vertical lifting mechanism to descend along the vertical direction, so that a sleeve on the spanner head is sleeved on the connecting nut, the connecting nut is loaded, and the connecting nut is screwed for disassembly and assembly.
In some optional embodiments, in the above method for assembling and disassembling the connecting nuts in the shaft cavity of the aeroengine, under the condition that the connecting nuts in the shaft cavity are uniformly distributed, the distance I between the sleeve axis on the wrench head and the rotation center of the connecting nut and the angle θ between the adjacent connecting nuts are recorded once, and accordingly, a program is recorded, and the assembling and disassembling of all the connecting nuts in the shaft cavity are completed one by controlling the vertical lifting mechanism, the horizontal moving mechanism and the horizontal rotating mechanism.
Drawings
FIG. 1 is a schematic view of a method for assembling and disassembling an attachment nut in an aircraft engine shaft cavity provided in an embodiment of the present application;
FIG. 2 is a schematic view of a part of a structure of an assembly and disassembly device for connecting nuts in a shaft cavity of an aeroengine according to an embodiment of the present application;
FIG. 3 is a schematic view of another angle of a portion of the structure of an assembly and disassembly device for connecting nuts in a shaft cavity of an aircraft engine according to an embodiment of the present application;
FIG. 4 is a partial schematic view of an aircraft engine shaft cavity connection nut assembly and disassembly device according to an embodiment of the present disclosure;
FIG. 5 is a schematic diagram of a wrench head and an industrial camera according to an embodiment of the present application;
FIG. 6 is an illustration of an aircraft engine in-cavity coupling nut removal device with cap recognition for coupling nuts, provided in an embodiment of the present application;
FIG. 7 is a schematic illustration of the positional deviation of the attachment nut assembly and disassembly device in an aircraft engine shaft cavity for attaching and detaching the attachment nut provided in an embodiment of the present application;
8-10 are schematic diagrams of an electric folding wrench when an aircraft engine shaft cavity connection nut dismounting device provided by the embodiment of the application works;
wherein:
1-automatic tightening of the assembly; 2-a fixed platform; 3-torque calibrator; 4-roller bottom; 5-an electrical operation cabinet; 6-an electric folding wrench; 7-a vertical lifting mechanism; 8-a horizontal movement mechanism; 9-a horizontal slewing mechanism; 10-hoisting a platform; 11-lifting platform; 12-a mobile platform; 13-a rotary servo motor; 14-fixing a base; 15-slewing bearing; 16-a slider; 17-a guide rail; 18-a rotary platform; 19-moving a servo cylinder; 20-lifting guide posts; 21-ball screw; 22-lifting servo motor; 23-engine stator case; 24-engine rotor; 25-connecting nuts; 26-spanner head; 27-an electric wrench mechanism; 28-spanner head folding mechanism; 30-a spanner bar positioning mechanism; 31-a positioning mechanism servo cylinder; 32-a positioning mechanism driving seat; 33-positioning mechanism slide blocks; 34-positioning mechanism guide rails; 35-a positioning mechanism mounting seat; 36-wrench extension bar; 37-a folding mechanism fixing seat; 38-folding the rod; 39-a transfer rod; 40-folding driving seat; 41-guide posts; 42-guiding sleeve; 43-folding mechanism servo cylinder; 44-an electric wrench; 45-fixing a guide seat; 100-industrial camera.
For the purpose of better illustrating the present embodiments, certain elements of the drawings may be omitted, enlarged or reduced and do not represent the actual product dimensions, and furthermore, the drawings are for illustrative purposes only and are not to be construed as limiting the present patent.
Detailed Description
In order to make the technical solution of the present application and the advantages thereof more apparent, the technical solution of the present application will be more fully described in detail below with reference to the accompanying drawings, it being understood that the specific embodiments described herein are only some of the embodiments of the present application, which are for explanation of the present application, not for limitation of the present application. It should be noted that, for convenience of description, only the portion relevant to the present application is shown in the drawings, and other relevant portions may refer to a general design, and without conflict, the embodiments and technical features in the embodiments may be combined with each other to obtain new embodiments.
Furthermore, unless defined otherwise, technical or scientific terms used in the description of this application should be given the ordinary meaning as understood by one of ordinary skill in the art to which this application belongs. The terms "upper," "lower," "left," "right," "center," "vertical," "horizontal," "inner," "outer," and the like as used in this description are merely used to indicate relative directions or positional relationships, and do not imply that a device or element must have a particular orientation, be configured and operated in a particular orientation, and that the relative positional relationships may be changed when the absolute position of the object being described is changed, and thus should not be construed as limiting the present application. The terms "first," "second," "third," and the like, as used in the description herein, are used for descriptive purposes only and are not to be construed as indicating or implying any particular importance to the various components. The use of the terms "a," "an," or "the" and similar referents in the description of the invention are not to be construed as limited in number to the precise location of at least one. As used in this description, the terms "comprises," "comprising," or the like are intended to cover an element or article that appears before the term and that is listed after the term and its equivalents, without excluding other elements or articles.
Furthermore, unless specifically stated and limited otherwise, the terms "mounted," "connected," and the like in the description herein are to be construed broadly and refer to either a fixed connection, a removable connection, or an integral connection, for example; can be mechanically or electrically connected; can be directly connected or indirectly connected through an intermediate medium, and can also be communicated with the inside of two elements, and the specific meaning of the two elements can be understood by a person skilled in the art according to specific situations.
The present application is described in further detail below with reference to fig. 1-10.
As shown in fig. 1, the device for dismounting and mounting the connecting nuts in the shaft cavity of the aeroengine consists of an automatic tightening assembly 1, a fixed platform 2, a torque calibrator 3, a roller car bottom 4 and an electric operation cabinet 5.
As shown in fig. 2 and 3, the automatic tightening assembly 1 is composed of an electric folding wrench 6, a vertical lifting mechanism 7, a horizontal moving mechanism 8 and a horizontal turning mechanism 9.
The vertical lifting mechanism 7 is positioned at the rear side of the electric folding wrench 6, the horizontal moving mechanism 8 is positioned below the electric folding wrench 6, and the horizontal turning mechanism 9 is positioned below the horizontal moving mechanism 8.
The electric folding spanner 6 is used for horizontally folding the spanner head 26 to realize electric rotation loading of the connecting nut 25, and an industrial camera 100 is arranged in a sleeve of the spanner head 26 for sleeving the connecting nut 25;
the vertical lifting mechanism 7 realizes the vertical Z-axis lifting of the electric folding wrench 6;
the horizontal moving mechanism 8 is used for moving the electric folding spanner 6 in the horizontal x-axis direction;
the horizontal turning mechanism 9 is used for turning the electric folding wrench 6 in the horizontal θ direction.
As shown in fig. 2 and 3, the vertical lift mechanism 7 is composed of a lift platform 11, a lift servo motor 22, a ball screw 21, a lift guide post 20, and the like.
As shown in fig. 8 to 10, the electric folding wrench 6 is composed of an electric wrench mechanism 27, a wrench head folding mechanism 28, and a wrench rod positioning mechanism 30.
The power wrench mechanism 27 is used for power tightening of nuts, the wrench end folding mechanism 28 is used for folding the wrench end 26, and the wrench rod positioning mechanism 30 is used for positioning and butting the wrench extension bar 36 with the wrench end 26.
The electric wrench mechanism 27 is composed of an electric wrench 44, a wrench extension 36, and a wrench head 26.
The spanner head folding mechanism 28 consists of a folding mechanism servo cylinder 43, a guide sleeve 42, a guide pillar 41, a folding driving seat 40, a folding rod 38, an adapter rod 39 and a spanner head 26.
The spanner rod positioning mechanism 30 consists of a positioning mechanism servo cylinder 31, a positioning mechanism driving seat 32, a positioning mechanism sliding block 33, a positioning mechanism guide rail 34, a positioning mechanism mounting seat 35 and a spanner extension bar 36.
The spanner extension bar 36 is connected below the electric spanner 44, and the spanner extension bar 36 is arranged on the folding mechanism fixing seat 37 and is restrained in the vertical direction by virtue of four fixing guide seats 45.
The electric wrench 44 is mounted on the positioning mechanism driving seat 32, and meanwhile, the positioning mechanism driving seat 32 is fixed with the cylinder head of the positioning mechanism servo cylinder 31, the positioning mechanism driving seat 32 is fixed on the positioning mechanism sliding block 33, the positioning mechanism sliding block 33 is mounted on the positioning mechanism guide rail 34, and the positioning mechanism guide rail 34 is fixed on the positioning mechanism mounting seat 35, so that the downward movement extension of the wrench extension bar 36 is realized by driving the positioning mechanism servo cylinder 31.
The positioning mechanism mounting seat 35 is fixed on one side of the lifting platform 11, the folding mechanism fixing seat 37 is fixed below the lifting platform 11, the folding mechanism servo cylinder 43 is fixed on one side of the lifting platform 11, two guide sleeves 42 are installed on the lifting platform 11, two guide posts 41 are installed in the guide sleeves 42, the two guide posts 41 are fixed on the folding driving seat 40, the folding driving seat 40 is fixed with a cylinder head of the folding mechanism servo cylinder 43, the folding driving seat 40 is connected with the folding rod 38 through a pin shaft, meanwhile, the folding rod 38 is restrained in the vertical direction through four fixing guide seats 45, the folding rod 38 is connected with the switching rod 39 through a pin shaft, the switching rod 39 is connected with the spanner head 26 through a pin shaft, thus the spanner head 26 is horizontally folded through driving the folding mechanism servo cylinder 43, the positioning mechanism servo cylinder 31 is driven again, the spanner head 36 is operated to move downwards, sleeve teeth at the front end of the spanner head 26 are positioned and butted with sleeve teeth in the spanner head 26, the spanner head 26 is composed of a gear pair, the driving gear pair is connected through the sleeve teeth, and the sleeve rotation of the driving gear pair to the spanner head 26 is transmitted to the spanner head 26, and the connecting nut 25 is loaded.
The horizontal moving mechanism 8 is composed of a moving platform 12, a moving servo cylinder 19, a guide rail 17, a slide block 16 and the like.
The horizontal slewing mechanism 9 consists of a slewing platform 18, a slewing servo motor 13, a slewing bearing 15 and the like.
As shown in fig. 2 and 3, the electric folding wrench 6 is located on a lifting platform 11 in the middle of four lifting guide posts 20 in the vertical lifting mechanism 7, lifting servo motors 22 and ball screws 21 are arranged on one side of the four lifting guide posts 20, a lifting platform 10 is connected to the upper surface of the four lifting guide posts 20 in the vertical lifting mechanism 7, and the lifting platform 10 is used for lifting and transferring of the automatic tightening assembly 1. The vertical lifting mechanism 7 is characterized in that the lower parts of four lifting guide posts 20 are connected with a movable platform 12, four sliding blocks 16 are fixed below the movable platform 12, a left sliding block 16 and a right sliding block 16 are respectively positioned above a left guide rail 17 and a right guide rail 17, a movable servo motor cylinder 19 is arranged on a rotary platform 18, a rotary support 15 is arranged below the rotary platform 18, a rotary servo motor 13 is arranged on one side of the rotary support 15, the rotary support 15 and the rotary servo motor 13 are arranged on a fixed base 14, and the fixed base 14 is used for centering and fixing the mounting edge of an engine stator case 23.
As shown in fig. 4, the automatic tightening assembly 1 is mounted on the mounting edge of the engine stator casing 23 through the fixing base 14, and is centered through the mounting edge spigot of the engine stator casing 23, because the axis of the engine stator casing 23 coincides with the axis of the engine rotor 24, the axis of the electric folding wrench 6 coincides with the axis of the fixing base 14, so that the axis of the electric folding wrench 6 coincides with the axis of the engine rotor 24, and the rotation center of the electric folding wrench 6 is the theoretical position center of the reference circle of the rotor connecting nut 25.
The inner diameter D of the fixed base 14 is designed to be smaller than the inner diameter D of the front shaft neck of the engine rotor 24, so that the shaft lever of the electric folding wrench 6 can not collide with the inner wall of the shaft cavity of the engine rotor 24 during operation, a pressure-sensitive sensor can be arranged on the surface of the wrench head 26, slight collision stress can be generated between the wrench head 26 and the inner wall of the inner cavity of the engine rotor 24, the alarm is immediately given, and the problem of collision damage of the inner wall of the shaft cavity is solved.
The device and the method for assembling and disassembling the connecting nut in the shaft cavity of the aeroengine can be used for assembling and disassembling the connecting nut, and can be carried out by referring to the following steps:
folding the wrench head 26 into an upright state with the electric folding wrench 6;
the spanner head 26 is sent into the shaft cavity along the vertical direction by the vertical lifting mechanism 7, the position of the connecting nut 25 is observed by the industrial camera 100, and the spanner head 26 is lowered to the vicinity of the connecting nut 25;
folding the wrench head 26 into a horizontal state with the electric folding wrench 6;
under the condition that the rotation center of the wrench head 26 is positioned at the center of the reference circle of the connecting nut 25 and is overlapped, the wrench head 26 is driven to horizontally move by the horizontal moving mechanism 8, the wrench head 26 is driven to rotate by the horizontal rotating mechanism 9, and the wrench head 26 is positioned above the rotor connecting nut 25;
photographing the outer circle of the connecting nut 25 by the industrial camera 100, calculating and analyzing the position deviation of the sleeve axis on the wrench head 26 and the axis of the connecting nut 25, driving the wrench head 26 to horizontally move by the horizontal moving mechanism 8, driving the wrench head 26 to rotate by the horizontal rotating mechanism 9, adjusting to enable the sleeve axis on the wrench head 26 and the axis of the connecting nut 25 to be consistent, and recognizing caps;
the spanner head 26 is driven by the vertical lifting mechanism 7 to descend along the vertical direction, so that a sleeve on the spanner head 26 is sleeved on the connecting nut 25, the connecting nut 25 is loaded, and the connecting nut 25 is screwed for dismounting, so that the spanner is convenient and quick.
If the connecting nuts 25 in the shaft cavity are uniformly distributed, the distance I between the sleeve axis on the spanner head 26 and the rotation center of the connecting nut 25 and the angle theta between the adjacent connecting nuts 25, which are consistent with the sleeve axis on the spanner head 26 and the connecting nut 25 axis, can be recorded once, and the program is recorded according to the distance I, and the disassembly and assembly of all the connecting nuts 25 in the shaft cavity are completed one by controlling the vertical lifting mechanism 7, the horizontal moving mechanism 8 and the horizontal rotation mechanism 9, as shown in fig. 6.
If the connecting nuts 25 in the shaft cavity are not uniformly distributed, the positions of the connecting nuts 25 can be found one by one through the vertical lifting mechanism 7, the horizontal moving mechanism 8 and the horizontal rotating mechanism 9, so that the dismounting of all the connecting nuts 25 is completed;
after the connection nuts 25 are disassembled and assembled, the electric folding wrench 6 exits the shaft cavity of the engine rotor 24 in the original path, the lifting appliance is arranged on the lifting platform 10, and the lifting automatic tightening assembly 1 is arranged on the fixed platform 2.
After the complete installation action of each connecting nut 25 in the shaft cavity of the aero-engine is finished for the first time, an automatic operation program is set through the whole action and the position information track of the electric folding wrench 6 which are completely recorded by the servo motors of all mechanisms, and the next time when the connecting nuts 25 in the shaft cavity of the aero-engine with the same type are dismounted, the dismounting can be automatically carried out according to the program.
As shown in FIG. 6, the axis of the coupling nut 25 is actually O 1 When the calculated axis of the coupling nut 25 is O as measured by the camera of the industrial camera 100, the measured eccentricity of the axis of the coupling nut 25 is O O 1 Feedback by industrial camera 100Is adjusted to obtain the actual axis of the sleeve of the spanner head 26 as O 2 The adjustment deviation is O O 2 Eccentricity e=o of the sleeve axis of the actual wrench head 26 and the axis of the coupling nut 25 1 O 2 Should e be less than or equal to OO 1 ±OO 2 ；
The outer diameter of the connecting nut 25 is set as D, the inner diameter of the sleeve of the wrench head 25 is set as D, in order to realize that the sleeve of the wrench head 25 can be matched and sleeved with the connecting nut 25 by overcoming the measurement adjustment deviation, the radial installation clearance t=D-D/2 between the inner diameter of the sleeve of the wrench head 25 and the outer diameter of the connecting nut 25 should be larger than the maximum deviation e max 。
In the description, each embodiment is described in a progressive manner, and each embodiment is mainly described by the differences from other embodiments, so that the same similar parts among the embodiments are mutually referred.
Having thus described the technical aspects of the present application with reference to the preferred embodiments illustrated in the accompanying drawings, it should be understood by those skilled in the art that the scope of the present application is not limited to the specific embodiments, and those skilled in the art may make equivalent changes or substitutions to the relevant technical features without departing from the principles of the present application, and those changes or substitutions will now fall within the scope of the present application.
Claims (5)
1. The utility model provides an aircraft engine shaft intra-cavity connection nut dismouting device, its characterized in that, including automatic tightening subassembly (1), automatic tightening subassembly (1) include electronic folding spanner (6), vertical lifting mechanism (7), horizontal movement mechanism (8), horizontal slewing mechanism (9), wherein:
the bottom end of the electric folding spanner (6) is used for being connected with a spanner head (26), the spanner head (26) can be horizontally folded, and an industrial camera (100) is arranged in a sleeve which is used for sleeving a connecting nut (25) on the spanner head (26);
the vertical lifting mechanism (7) is used for lifting the electric folding wrench (6) in the vertical direction and comprises a lifting platform (11), a lifting servo motor (22), a ball screw (21) and a lifting guide post (20);
the horizontal moving mechanism (8) is used for moving the electric folding wrench (6) in the horizontal direction and comprises a moving platform (12), a moving servo electric cylinder (19), a guide rail (17) and a sliding block (16);
the horizontal rotary mechanism (9) is used for horizontally rotating the electric folding wrench (6) and comprises a rotary platform (18), a rotary servo motor (13) and a rotary support (15);
the electric folding wrench (6) is positioned on a lifting platform (11) in the middle of four lifting guide posts (20) in the vertical lifting mechanism (7), a lifting servo motor (22) and a ball screw (21) are arranged on one side of the four lifting guide posts (20), and the upper surfaces of the four lifting guide posts (20) in the vertical lifting mechanism (7) are connected with a lifting platform (10);
the lower parts of four lifting guide posts (20) in the vertical lifting mechanism (7) are connected with a movable platform (12), four sliding blocks (16) are fixed below the movable platform (12), and two groups of the four sliding blocks (16) are respectively positioned above two guide rails (17);
the movable servo motor cylinder (19) is arranged on the rotary platform (18), a rotary support (15) is arranged below the rotary platform (18), the rotary servo motor (13) is arranged on one side of the rotary support (15), and the rotary support (15) and the rotary servo motor (13) are arranged on the fixed base (14);
the fixed base (14) is used for centering and fixing with the mounting edge of the engine stator case (23);
d < D; wherein,
d is the inner diameter of the fixed base (14);
d is the radial dimension of the shaft cavity opening;
the electric folding wrench (6) comprises an electric wrench mechanism (27), a wrench head folding mechanism (28) and a wrench rod positioning mechanism (30);
the electric wrench mechanism (27) is used for electrically tightening nuts, the wrench head folding mechanism (28) is used for folding the wrench heads (26), and the wrench rod positioning mechanism (30) is used for positioning and butting the wrench extension rod (36) with the wrench heads (26);
the electric wrench mechanism (27) comprises an electric wrench (44) and a wrench extension bar (36);
the spanner head folding mechanism (28) comprises a folding mechanism servo electric cylinder (43), a guide sleeve (42), a guide pillar (41), a folding driving seat (40), a folding rod (38) and a switching rod (39);
the spanner rod positioning mechanism (30) comprises a positioning mechanism servo cylinder (31), a positioning mechanism driving seat (32), a positioning mechanism sliding block (33), a positioning mechanism guide rail (34), a positioning mechanism mounting seat (35) and a spanner extension bar (36);
the lower part of the electric wrench (44) is connected with a wrench extension bar (36), the wrench extension bar (36) is arranged on a folding mechanism fixing seat (37), and the four fixing guide seats (45) are used for restraining in the vertical direction;
the electric wrench (44) is arranged on the positioning mechanism driving seat (32), meanwhile, the positioning mechanism driving seat (32) is fixed with the electric cylinder head of the positioning mechanism servo electric cylinder (31), the positioning mechanism driving seat (32) is fixed on the positioning mechanism sliding block (33), the positioning mechanism sliding block (33) is arranged on the positioning mechanism guide rail (34), the positioning mechanism guide rail (34) is fixed on the positioning mechanism mounting seat (35), and the downward movement extension of the wrench extension bar (36) can be realized by driving the positioning mechanism servo electric cylinder (31);
the positioning mechanism mounting seat (35) is fixed on one side of the lifting platform (11), the folding mechanism fixing seat (37) is fixed below the lifting platform (11), the folding mechanism servo electric cylinder (43) is hinged below the folding mechanism fixing seat (37), two guide sleeves (42) are mounted on the lifting platform (11), two guide posts (41) are mounted in the guide sleeves (42), the two guide posts (41) are fixed on the folding driving seat (40), the folding driving seat (40) is fixed with the electric cylinder head of the folding mechanism servo electric cylinder (43), the folding driving seat (40) is connected with the folding rod (38) through a pin shaft, meanwhile, the folding rod (38) is constrained in the vertical direction through four fixed guide seats (45), the folding rod (38) is connected with the transfer rod (39) through a pin shaft, the transfer rod (39) is connected with the wrench head (26) through a pin shaft, the horizontal folding of the wrench head (26) can be realized through driving the folding mechanism servo electric cylinder (43), the positioning mechanism servo electric cylinder (31) is driven to operate the wrench to move downwards, the wrench head (26) is connected with the front end of the wrench head (26) through a pin shaft, the gear pair is connected with the inner sleeve gear pair (26) through the rotating teeth, the gear pair is formed by the inner sleeve gear pair, furthermore, loading of the coupling nut (25) can be achieved.
2. The device for assembling and disassembling an internal connection nut in a shaft cavity of an aircraft engine according to claim 1, characterized in that a pressure-sensitive sensor is arranged on the surface of the wrench head (26).
3. The device for dismounting and mounting the connection nut in the axial cavity of the aeroengine according to claim 1, further comprising a fixed platform (2), a torque calibrator (3), a roller bottom (4) and an electrical operation cabinet (5);
the fixed platform (2) is connected to the roller bottom (4) and is used for fixing the automatic tightening assembly (1);
the torque calibrator (3) is arranged on the automatic tightening assembly (1) and is used for calibrating the torque of the automatic tightening assembly (1);
the electric operation cabinet (5) is connected to the roller car bottom (4), can record programs, is connected with the driving mechanisms of the electric folding wrench (6), the vertical lifting mechanism (7), the horizontal moving mechanism (8) and the horizontal rotating mechanism (9), and is connected with the industrial camera (100), and can screw each connecting nut (25) one by one according to the recorded programs under the condition that each connecting nut (25) is uniformly distributed in the shaft cavity, so that the disassembly and assembly are completed.
4. A method for assembling and disassembling an aircraft engine shaft cavity internal connection nut, based on the device for assembling and disassembling an aircraft engine shaft cavity internal connection nut according to any one of claims 1 to 3, comprising:
folding the wrench head (26) into a vertical state by an electric folding wrench (6);
the spanner head (26) is sent into the shaft cavity along the vertical direction by the vertical lifting mechanism (7), the position of the connecting nut (25) is observed by the industrial camera (100), and the spanner head (26) is lowered to the vicinity of the connecting nut (25);
folding the wrench head (26) into a horizontal state by an electric folding wrench (6);
under the condition that the rotation center of the wrench head (26) is positioned at the center of the reference circle of the connecting nut (25), the wrench head (26) is driven to horizontally move by the horizontal moving mechanism (8), the wrench head (26) is driven to rotate by the horizontal rotating mechanism (9), and the wrench head (26) is positioned above the rotor connecting nut (25);
photographing the outer circle of the connecting nut (25) through an industrial camera (100), calculating and analyzing the position deviation of the sleeve axis on the wrench head (26) and the axis of the connecting nut (25), driving the wrench head (26) to horizontally move through a horizontal moving mechanism (8), driving the wrench head (26) to rotate through a horizontal rotating mechanism (9), and adjusting to enable the sleeve axis on the wrench head (26) and the axis of the connecting nut (25) to be consistent;
the spanner head (26) is driven by the vertical lifting mechanism (7) to descend along the vertical direction, so that a sleeve on the spanner head (26) is sleeved on the connecting nut (25), the sleeve is connected with the electric folding spanner (6) through the toothed pattern, the connecting nut (25) is loaded, and the connecting nut (25) is screwed for dismounting.
5. The method for assembling and disassembling an internal connection nut in an aircraft engine shaft cavity according to claim 4, wherein,
under the condition that all the connecting nuts (25) in the shaft cavity are uniformly distributed, recording the distance I between the sleeve axis on the wrench head (26) and the rotation center of the connecting nuts (25) and the angle theta between the adjacent connecting nuts (25) which enable the sleeve axis on the wrench head (26) and the axis of the connecting nuts (25) to be consistent at one time, and recording a program according to the distance I, and completing the disassembly and assembly of all the connecting nuts (25) in the shaft cavity one by controlling the vertical lifting mechanism (7), the horizontal moving mechanism (8) and the horizontal rotation mechanism (9).
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202211522238.1A CN115890216A (en) | 2022-11-30 | 2022-11-30 | Device and method for dismounting connecting nut in shaft cavity of aircraft engine |
| CN2022115222381 | 2022-11-30 |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN116638296A CN116638296A (en) | 2023-08-25 |
| CN116638296B true CN116638296B (en) | 2024-03-19 |
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Family Applications (2)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202211522238.1A Withdrawn CN115890216A (en) | 2022-11-30 | 2022-11-30 | Device and method for dismounting connecting nut in shaft cavity of aircraft engine |
| CN202310443421.0A Active CN116638296B (en) | 2022-11-30 | 2023-04-23 | Device and method for disassembling and assembling connecting nuts in shaft cavity of aero-engine |
Family Applications Before (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202211522238.1A Withdrawn CN115890216A (en) | 2022-11-30 | 2022-11-30 | Device and method for dismounting connecting nut in shaft cavity of aircraft engine |
Country Status (1)
| Country | Link |
|---|---|
| CN (2) | CN115890216A (en) |
Citations (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP0862967A2 (en) * | 1997-03-07 | 1998-09-09 | Mathias Bihler | Screwing device |
| JP2008142824A (en) * | 2006-12-08 | 2008-06-26 | Honda Motor Co Ltd | Method and device for attaching/detaching member |
| KR100862396B1 (en) * | 2008-04-29 | 2008-10-13 | 원일파템 주식회사 | Nut automatic supply tightening device |
| CN110561098A (en) * | 2019-09-03 | 2019-12-13 | 大连理工大学 | A flexible shaft-driven tightening device and method for an internal nut of an aero-engine |
| CN111660085A (en) * | 2020-06-16 | 2020-09-15 | 中国航发航空科技股份有限公司 | Assembling device for connecting nut in narrow space of high-pressure rotor of engine and operation method |
| CN112045405A (en) * | 2020-09-22 | 2020-12-08 | 沈阳航空航天大学 | Fast and large torque tightening device and tightening method for blind cavity in narrow and long space |
| CN112589408A (en) * | 2020-12-11 | 2021-04-02 | 北京航空航天大学 | Automatic tightening device and method for blind cavity nut of aero-engine compressor rotor |
| CN114850845A (en) * | 2021-02-03 | 2022-08-05 | 中国科学院沈阳自动化研究所 | An automatic tightening mechanism suitable for narrow spaces |
| CN115673744A (en) * | 2022-11-30 | 2023-02-03 | 中国航发沈阳发动机研究所 | Dismounting device for connecting nut in shaft cavity of aircraft engine |
| CN115741070A (en) * | 2022-11-30 | 2023-03-07 | 中国航发沈阳发动机研究所 | Tool and method for disassembling and assembling connecting nut in shaft cavity of aircraft engine |
-
2022
- 2022-11-30 CN CN202211522238.1A patent/CN115890216A/en not_active Withdrawn
-
2023
- 2023-04-23 CN CN202310443421.0A patent/CN116638296B/en active Active
Patent Citations (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP0862967A2 (en) * | 1997-03-07 | 1998-09-09 | Mathias Bihler | Screwing device |
| JP2008142824A (en) * | 2006-12-08 | 2008-06-26 | Honda Motor Co Ltd | Method and device for attaching/detaching member |
| KR100862396B1 (en) * | 2008-04-29 | 2008-10-13 | 원일파템 주식회사 | Nut automatic supply tightening device |
| CN110561098A (en) * | 2019-09-03 | 2019-12-13 | 大连理工大学 | A flexible shaft-driven tightening device and method for an internal nut of an aero-engine |
| CN111660085A (en) * | 2020-06-16 | 2020-09-15 | 中国航发航空科技股份有限公司 | Assembling device for connecting nut in narrow space of high-pressure rotor of engine and operation method |
| CN112045405A (en) * | 2020-09-22 | 2020-12-08 | 沈阳航空航天大学 | Fast and large torque tightening device and tightening method for blind cavity in narrow and long space |
| CN112589408A (en) * | 2020-12-11 | 2021-04-02 | 北京航空航天大学 | Automatic tightening device and method for blind cavity nut of aero-engine compressor rotor |
| CN114850845A (en) * | 2021-02-03 | 2022-08-05 | 中国科学院沈阳自动化研究所 | An automatic tightening mechanism suitable for narrow spaces |
| CN115673744A (en) * | 2022-11-30 | 2023-02-03 | 中国航发沈阳发动机研究所 | Dismounting device for connecting nut in shaft cavity of aircraft engine |
| CN115741070A (en) * | 2022-11-30 | 2023-03-07 | 中国航发沈阳发动机研究所 | Tool and method for disassembling and assembling connecting nut in shaft cavity of aircraft engine |
Also Published As
| Publication number | Publication date |
|---|---|
| CN115890216A (en) | 2023-04-04 |
| CN116638296A (en) | 2023-08-25 |
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