CN114346627B - Portable flight attaches installation debugging frock - Google Patents
Portable flight attaches installation debugging frock Download PDFInfo
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- CN114346627B CN114346627B CN202111411217.8A CN202111411217A CN114346627B CN 114346627 B CN114346627 B CN 114346627B CN 202111411217 A CN202111411217 A CN 202111411217A CN 114346627 B CN114346627 B CN 114346627B
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Abstract
The invention relates to a movable type flyer installation and debugging tool which comprises an AGV chassis, an ear type supporting device, a bolt type supporting device and a flyer supporting device, wherein the ear type supporting device and the bolt type supporting device are used for supporting a gas engine, the flyer supporting device is used for supporting flying accessories of the engine, two ear type supporting devices are symmetrically arranged, each ear type supporting device comprises a first upright post fixed on the AGV chassis, lifting suspension lug assemblies are fixed at the upper ends of the first upright posts, two bolt type supporting devices are symmetrically arranged, each bolt type supporting device comprises a second upright post fixed on the AGV chassis, a pin shaft assembly capable of transversely stretching is fixed at the upper ends of the second upright posts, each flyer supporting device comprises a supporting frame installed on the AGV chassis through a longitudinal moving mechanism, a lifting frame is installed in the supporting frame through a lifting mechanism, a slewing bearing is installed on the lifting frame through a transverse moving mechanism, and a flyer bracket is fixed on the slewing bearing. The integrated circuit has the advantages of high integration level, simplicity and convenience in operation, safety, reliability and strong applicability.
Description
Technical Field
The invention relates to a tool, in particular to a movable engine flight accessory installation and debugging tool.
Background
The gas engine is used as a power device of an airplane, and is required to be connected and debugged with an engine flight accessory (for short, the flight accessory) in the assembly process, and the gas engine is transferred to the next working procedure after the debugging is finished so as to ensure that the flight accessory works normally. The prior art aims at the problems of large control difficulty, poor safety and low working efficiency in practical application of the mode of connecting and debugging the gas engine and the flyer by adopting a lifting appliance to lift and connect generally and transferring through the lifting appliance after the debugging is completed.
Disclosure of Invention
The invention aims to provide a movable type flying installation and debugging tool which has the advantages of high integration level, simplicity and convenience in operation, safety, reliability and strong applicability.
In order to solve the problems in the prior art, the movable flyer installation debugging tool provided by the invention comprises an AGV chassis, and an ear-type supporting device, a bolt-type supporting device and a flyer supporting device which are arranged on the AGV chassis, wherein the ear-type supporting device and the bolt-type supporting device are used for supporting a gas engine, the flyer supporting device is used for supporting engine flying accessories, two symmetrical ear-type supporting devices are arranged on the left half part of the AGV chassis, each ear-type supporting device comprises a first upright post fixed on the AGV chassis, two lifting hanging lug assemblies are fixed at the upper end of each first upright post, each bolt-type supporting device is symmetrically arranged on the right half part of the AGV chassis, each bolt-type supporting device comprises a second upright post fixed on the AGV chassis, each transverse telescopic pin shaft assembly is fixed at the upper end of each second upright post, each flyer supporting device is positioned between the two bolt-type supporting devices, each flyer supporting device comprises a supporting frame installed on the AGV chassis through a longitudinal moving mechanism, each lifting frame is installed in each supporting frame through a lifting mechanism, and each lifting frame is installed on each lifting frame through a rotary supporting bracket.
Furthermore, the movable type flying installation and debugging tool comprises a first bottom plate fixed on a first upright post, a rotatable first nut is clamped on the first bottom plate, a screw rod in threaded fit is sleeved on the first nut, a first guide sleeve is further fixed on the first bottom plate, a guide rod in sliding fit is sleeved on the first guide sleeve, a connecting seat is fixed at the upper ends of the screw rod and the guide rod, and a hanging lug is arranged on the connecting seat.
Furthermore, the movable type flying installation and debugging tool disclosed by the invention is characterized in that the first nut is provided with the rotary operation holes distributed along the circumferential direction, two first guide sleeves are arranged, and the two first guide sleeves are correspondingly arranged on two sides of the first nut.
Furthermore, the movable type flying installation and debugging tool comprises a second bottom plate fixed on a second upright post, a supporting seat is arranged on the second bottom plate, a rotatable second nut is clamped on the supporting seat, a second guide sleeve is further fixed on the supporting seat, a telescopic rod is arranged in a penetrating mode through the second nut and the second guide sleeve, threads matched with the second nut and a pin cutting flat opening matched with the second guide sleeve are arranged on the peripheral wall of the telescopic rod, and a pin shaft integrated with the telescopic rod is arranged at the end portion of the telescopic rod.
Furthermore, the movable type flying installation and debugging tool is characterized in that two pin cutting flat openings are arranged, the two pin cutting flat openings are correspondingly arranged on two sides of the telescopic rod, and the second nut is fixedly provided with a rotary hand wheel.
Furthermore, the invention relates to a movable type fly attachment installation and debugging tool, wherein the longitudinal movement mechanism comprises two first guide rails longitudinally fixed on an AGV chassis, the first guide rails are provided with first sliding blocks in sliding fit, the first sliding blocks are fixed on a supporting frame, and longitudinal movement locking screws are screwed on the first sliding blocks.
Furthermore, the invention relates to a movable type flying installation and debugging tool, wherein the lifting mechanism comprises two second guide rails vertically fixed on a supporting frame, second sliding blocks in sliding fit are arranged on the second guide rails, the second sliding blocks are fixed on the lifting frame, the lifting mechanism further comprises a bracket fixed on the supporting frame, a transmission case is fixed on the bracket, two ends of a worm in the transmission case are correspondingly connected with a servo motor and an operation hand wheel, a screw rod in threaded fit is sleeved on a worm wheel in the transmission case, and the upper end of the screw rod is fixedly connected with the lifting frame.
Furthermore, the movable type flying installation and debugging tool disclosed by the invention comprises two third guide rails transversely fixed on the lifting frame, wherein the third guide rails are provided with third sliding blocks in sliding fit, the third sliding blocks are provided with transverse moving locking screws in a rotating mode, and the third sliding blocks are fixedly connected with the slewing bearing through the supporting platen.
Furthermore, the invention relates to a movable type flying attachment installation and debugging tool, wherein the flying attachment bracket comprises a bracket, three support columns are arranged on the bracket, and positioning columns matched with positioning holes on an engine flying attachment are arranged on the support columns.
Furthermore, the mobile type flying installation and debugging tool disclosed by the invention is characterized in that a first connecting plate and a second connecting plate corresponding to the lug type supporting device and the bolt type supporting device are fixed on the AGV chassis, screw holes which are distributed at intervals are respectively arranged on the first connecting plate and the second connecting plate, a groove is arranged at the position between the two bolt type supporting devices on the AGV chassis, the lug type supporting device is fixed on the first connecting plate through a first mounting hole on the base of the AGV chassis, the bolt type supporting device is fixed on the second connecting plate through a second mounting hole on the base of the AGV chassis, the first mounting hole and the second mounting hole are strip-shaped holes, and the flying supporting device is positioned in the groove of the AGV chassis.
Compared with the prior art, the mobile type flying installation and debugging tool has the following advantages: according to the invention, the AGV chassis, the lug type supporting device, the bolt type supporting device and the flying accessory supporting device are arranged, wherein the lug type supporting device and the bolt type supporting device are used for supporting a gas engine, and the flying accessory supporting device is used for supporting an engine flying accessory. Make ear formula strutting arrangement set up two in the left half symmetry of AGV chassis, let ear formula strutting arrangement set up the first stand of fixing on the AGV chassis, and fix liftable hangers subassembly in the upper end of first stand, make bolt formula strutting arrangement set up two in the right half symmetry of AGV chassis, let bolt formula strutting arrangement set up the second stand of fixing on the AGV chassis, and fix the horizontal flexible round pin axle subassembly in the upper end of second stand, make the setting of flight support device between two bolt formula strutting arrangement, let flight support device set up the braced frame who moves the mechanism through indulging on the AGV chassis, install lifting frame through elevating system in braced frame, install slewing bearing through sideslip mechanism on lifting frame, fix the flight support on slewing bearing. Therefore, the movable type flying installation and debugging tool is formed, and in practical application, the gas engine is fixed on the ear type supporting device and the bolt type supporting device, wherein the ear type supporting device is connected with an ear plate at a first combination position on the gas engine, and the bolt type supporting device is connected with a pin hole at a second combination position on the gas engine; the engine flight accessory is fixed on the flying accessory supporting device, the relative position between the engine flight accessory and the gas engine is adjusted through the flying accessory supporting device, the engine flight accessory and the gas engine can be connected and debugged after being adjusted in place, and the engine flight accessory and the gas engine can be transported to the next procedure through the AGV chassis after the debugging is completed. According to the invention, by arranging the AGV chassis, the stability and safety of the flying accessory of the transfer engine and the gas engine are improved; by arranging two lifting ear-type supporting devices, the gas engine can be vertically and circumferentially adjusted, and by arranging two bolt-type supporting devices capable of transversely stretching, the gas engine can be transversely and axially adjusted, so that the convenience of connection operation is improved, and the accurate adjustment and positioning of the posture of the gas engine are realized; the flying accessory supporting device is provided with the longitudinal moving mechanism, the lifting mechanism, the transverse moving mechanism and the slewing bearing, so that the multi-degree-of-freedom adjustment of the flying accessory of the engine is realized, and the simplicity of position adjustment and connection with the gas engine is improved. Compared with the prior art, the invention has the advantages of high integration level, simple and convenient operation, safety, reliability and strong applicability, and can effectively improve the working efficiency.
The invention relates to a movable type flying installation and debugging tool, which is described in detail below with reference to the specific embodiments shown in the drawings.
Drawings
FIG. 1 is a front view of a mobile attachment installation and debugging tool of the present invention;
FIG. 2 is an isometric view of a mobile pendant installation and debugging tool of the present invention;
FIG. 3 is a front view of a middle ear type support device of a mobile type aerial attachment installation and debugging tool of the present invention;
FIG. 4 is an isometric view of a middle ear type support device of a mobile type aerial attachment installation and debugging tool of the present invention;
FIG. 5 is a front view of a hanger assembly in a mobile pendant installation and debugging tool of the present invention;
FIG. 6 isbase:Sub>A view in the direction A-A of FIG. 7;
FIG. 7 is a top view of a hanger assembly in a mobile pendant installation and debugging tool of the present invention;
FIG. 8 is an isometric view of a hanger assembly in a mobile pendant installation and debugging tool of the present invention;
FIG. 9 is a front view of a bolt-type support device in a mobile type aerial installation and debugging tool of the present invention;
FIG. 10 is an isometric view of a bolt-type support device in a mobile type aerial installation and debugging tool according to the present invention;
FIG. 11 is a front view of a pin assembly in a mobile aircraft installation and debugging tool of the present invention;
FIG. 12 is a top view of a pin assembly in a mobile aircraft installation and debugging tool of the present invention;
FIG. 13 is a view in the B-B direction of FIG. 11;
FIG. 14 is an isometric view of a pin assembly in a mobile aircraft installation and debugging tool of the present invention;
FIG. 15 is a front view of the attachment support device in the mobile attachment installation and adjustment tool of the present invention;
FIG. 16 is a top view of an attachment support device in a mobile attachment installation and adjustment tool of the present invention;
FIG. 17 is an isometric view of an attachment support device in a mobile attachment installation and adjustment tool of the present invention;
FIG. 18 is a front view of the internal structure of the attachment support device in the mobile attachment installation and debugging tool of the present invention;
FIG. 19 is an isometric view of an inner structure of an attachment support device in a mobile attachment installation and debugging tool according to the present invention;
FIG. 20 is a rear view of the internal structure of the attachment support device in the mobile attachment installation and debugging tool of the present invention;
FIG. 21 is a second perspective view of the internal structure of the attachment support device in the mobile attachment installation and adjustment tool according to the present invention;
FIG. 22 is a working state diagram of the mobile type flying installation and debugging tool.
Detailed Description
First, it should be noted that the terms of up, down, left, right, front, back, etc. in the present invention are merely described according to the drawings, so as to facilitate understanding, and are not limited to the technical solution of the present invention and the scope of protection claimed.
The embodiment of the mobile type flyer installation and debugging tool comprises an AGV chassis 1, and an ear type supporting device 2, a bolt type supporting device 3 and a flyer supporting device 4 which are arranged on the AGV chassis 1, wherein the ear type supporting device 2 and the bolt type supporting device 3 are used for supporting a gas engine 100, and the flyer supporting device 4 is used for supporting an engine flight accessory 200. Make ear formula strutting arrangement 2 set up two in the left half symmetry of AGV chassis 1, let ear formula strutting arrangement 2 set up the first stand 21 of fixing on AGV chassis 1 to the hangers subassembly 22 of liftable is fixed to the upper end at first stand 21. Two bolt type supporting devices 3 are symmetrically arranged on the right half part of the AGV chassis 1, the bolt type supporting devices 3 are provided with second upright posts 31 fixed on the AGV chassis 1, and pin shaft assemblies 32 capable of transversely stretching and retracting are fixed at the upper ends of the second upright posts 31. The fly supporting device 4 is provided between the two pin supporting devices 3, the fly supporting device 4 is provided with a supporting frame 41 mounted on the AGV chassis 1 by a vertical movement mechanism, a lifting frame 42 is mounted on the supporting frame 41 by a lifting mechanism, a slewing bearing 43 is mounted on the lifting frame 42 by a lateral movement mechanism, and a fly bracket 44 is fixed on the slewing bearing 43.
The movable type flying installation and debugging tool is formed through the structure, in practical application, the gas engine is fixed on the ear type supporting device 2 and the bolt type supporting device 3, wherein the ear type supporting device 2 is connected with an ear plate at a first combination position on the gas engine, and the bolt type supporting device 3 is connected with a pin hole at a second combination position on the gas engine; the engine flight accessory is fixed on the flying accessory supporting device 4, the relative position between the engine flight accessory and the gas engine is adjusted through the flying accessory supporting device 4, the engine flight accessory and the gas engine can be connected and debugged after being adjusted in place, and the engine flight accessory and the gas engine can be transported to the next procedure through the AGV chassis 1 after the debugging is completed. According to the invention, by arranging the AGV chassis 1, the stability and safety of the flying accessory of the one-to-one transfer engine and the gas engine are improved; by arranging two lifting ear type supporting devices 2, the gas engine can be vertically and circumferentially adjusted, and by arranging two bolt type supporting devices 3 which can transversely stretch out and draw back, the gas engine can be transversely and axially adjusted, so that the convenience of connection operation is improved, and the accurate adjustment and positioning of the posture of the gas engine are realized; by arranging the vertical moving mechanism, the lifting mechanism, the transverse moving mechanism and the rotary support on the flying accessory supporting device 4, the multi-degree-of-freedom adjustment of the flying accessory of the engine is realized, and the simplicity of position adjustment and connection with the gas engine is improved. Compared with the prior art, the invention has the advantages of high integration level, simple and convenient operation, safety, reliability and strong applicability, and can effectively improve the working efficiency. In the present invention, when the gas engine is fixed, the gas engine is generally connected with the two ear-type supporting devices and then connected with the two bolt-type supporting devices, so as to improve the simplicity of operation and adjustment.
As a specific embodiment, the present invention allows the hanger assembly 22 to be constructed as follows: a first bottom plate 221 fixed on the first upright 21 is provided, a rotatable first nut 222 is clamped on the first bottom plate 221, a screw 223 in threaded engagement is sleeved on the first nut 222, a first guide sleeve 224 is fixed on the first bottom plate 221, a guide rod 225 in sliding engagement is sleeved on the first guide sleeve 224, a connecting seat 226 is fixed on the upper ends of the screw 223 and the guide rod 225, and a hanging lug 2261 is provided on the connecting seat 226. The hanging ear assembly 22 has the characteristics of simple structure, flexible operation and control and stable lifting, and the lifting purpose of the connecting seat 226 and the hanging ear 2261 can be realized only by rotating the first nut 222. In order to improve the convenience of operation and the stability of the structure, the present embodiment provides rotation operation holes distributed along the circumferential direction on the first nut 222, so that two first guide sleeves 224 are provided, and the two first guide sleeves 224 are correspondingly provided at two sides of the first nut 222. As a specific embodiment, the pin shaft assembly 32 adopts the following structure: the second bottom plate 321 fixed on the second upright post 31 is arranged, the supporting seat 322 is arranged on the second bottom plate 321, the rotatable second nut 323 is clamped on the supporting seat 322, the second guide sleeve 324 is fixed on the supporting seat 322, the telescopic rod 325 is arranged in the second nut 323 and the second guide sleeve 324 in a penetrating way, threads matched with the second nut 323 and a pin cutting flat port 3251 matched with the second guide sleeve 324 are arranged on the peripheral wall of the telescopic rod 325, and a pin shaft 3252 integrated with the telescopic rod 325 is arranged at the end part of the telescopic rod 325. The pin shaft assembly 32 has the characteristics of simple structure, flexible operation and control and stable extension, and the extension purpose of the extension rod 325 can be realized only by rotating the second nut 323. In order to improve the convenience of operation and the stability of the structure, the present embodiment fixes the rotation hand wheel 326 on the second nut 323, so that two pin-cutting flat openings 3251 are provided, and the two pin-cutting flat openings 3251 are correspondingly provided at both sides of the telescopic rod 325.
As a specific embodiment, the longitudinal moving mechanism is provided with two first guide rails 11 longitudinally fixed on the AGV chassis 1, and a first sliding block 411 in sliding fit is arranged on the first guide rails 11, wherein the first sliding block 411 is fixed on the supporting frame 41, and a longitudinal moving locking screw 412 is screwed on the first sliding block 411. The vertical moving mechanism has the characteristics of simple structure, flexible operation and control and stable movement, can move on the first guide rail 11 only by manually pushing and pulling the flying support device 4 in practical application, can lock the flying support device 4 in the longitudinal direction by screwing the vertical moving locking screw 412 after being longitudinally adjusted in place, and can effectively avoid the influence of the self-sliding of the flying support device 4 on the safety and reliability of debugging.
As a specific embodiment, the lifting mechanism is provided with two second guide rails 413 vertically fixed on the supporting frame 41, and a second sliding block 421 in sliding fit is arranged on the second guide rails 413, wherein the second sliding block 421 is fixed on the lifting frame 42; the lifting mechanism is provided with a bracket 414 fixed on the supporting frame 41, a transmission box 415 is fixed on the bracket 414, wherein two ends of a worm in the transmission box 415 are correspondingly connected with a servo motor 416 and an operation hand wheel 417, a worm wheel in the transmission box 415 is sleeved with a screw 418 in threaded fit, and the upper end of the screw 418 is fixedly connected with the lifting frame 42. The lifting mechanism has the characteristics of simple structure, flexible operation and control and stable lifting, can not only electrically lift through the servo motor 416, but also manually lift through the operation hand wheel 417, and can vertically lock the lifting frame 42 and the parts above through the self-locking function of the transmission case 415 after the height is adjusted in place, thereby ensuring the safety and reliability of debugging.
As a specific embodiment, the traversing mechanism is provided with two third guide rails 422 transversely fixed on the lifting frame 42, and a third sliding block 431 in sliding fit is arranged on the third guide rails 422, wherein a traversing locking screw 432 is screwed on the third sliding block 431, and the third sliding block 431 is fixedly connected with the slewing bearing 43 through a supporting platen 433. The transverse moving mechanism has the characteristics of simple structure, flexible operation and control and stable movement, and can slide on the third guide rail 422 only by manually pushing and pulling the slewing bearing 43 or the flying bracket 44 in practical application, and can lock the slewing bearing 43 and the parts above in the transverse direction by screwing the transverse moving locking screw 432 after the transverse moving mechanism is transversely adjusted in place, so that the safety and the reliability of debugging are ensured. In a specific embodiment, the following configuration is adopted for the attachment bracket 44 in the present invention: a bracket 441 fixed to the slewing bearing 43 is provided, three support columns 442 are provided on the bracket 441, and a positioning column 443 that mates with a positioning hole on an engine flight accessory is provided on the support columns 442. The flying bracket 44 has the characteristics of single structure and convenient connection, and only the positioning posts 443 on the three supporting posts 442 are correspondingly inserted into the positioning holes on the flying accessories of the engine.
In practical application, the invention also fixes a first connecting plate 12 and a second connecting plate 13 corresponding to the ear type supporting device 2 and the bolt type supporting device 3 on the AGV chassis 1, and sets screw holes which are distributed at intervals on the first connecting plate 12 and the second connecting plate 13 respectively, and sets a groove on the AGV chassis 1 at the position between the two bolt type supporting devices 3, wherein the ear type supporting device 2 is fixed on the first connecting plate 12 through a first mounting hole 211 and a screw on the base of the ear type supporting device, the bolt type supporting device 3 is fixed on the second connecting plate 13 through a second mounting hole 311 and a screw on the base of the ear type supporting device, the first mounting hole 211 and the second mounting hole 311 are bar-shaped holes, and the flying supporting device 4 is positioned in the groove of the AGV chassis 1. According to the structure, the first connecting plate 12 and the second connecting plate 13 are respectively provided with the screw holes which are distributed at intervals, so that the ear type supporting device 2 and the bolt type supporting device 3 can select different screw holes to be correspondingly connected with the first connecting plate 12 and the second connecting plate 13 so as to adapt to different types of gas engines 100; by adopting the strip-shaped holes for the first mounting holes 211 and the second mounting holes 311, the positions of the ear type supporting device 2 and the bolt type supporting device 3 can be finely adjusted, so that the adaptability is improved; through making AGV chassis 1 set up the recess, and make the flight attach strutting arrangement 4 set up in the recess of AGV chassis 1, be favorable to reducing the barycenter height, improved fail safe nature.
The above examples are merely illustrative of the preferred embodiments of the present invention and are not intended to limit the scope of the invention as claimed, and various modifications made by those skilled in the art according to the technical solution of the present invention should fall within the scope of the invention as defined in the claims without departing from the design concept of the present invention.
Claims (8)
1. The utility model provides a portable flyer installation debugging frock, includes AGV chassis (1) and sets up otic bracing device (2), bolt strutting arrangement (3) and flyer strutting arrangement (4) on AGV chassis (1), otic bracing device (2) and bolt strutting arrangement (3) are used for supporting gas engine, flyer strutting arrangement (4) are used for supporting engine flight annex, a serial communication port, otic bracing device (2) are equipped with two in the left half symmetry of AGV chassis (1), otic bracing device (2) including fixing first stand (21) on AGV chassis (1), the upper end of first stand (21) is fixed with liftable hangers subassembly (22), bolt strutting arrangement (3) are equipped with two in the right half symmetry of AGV chassis (1), and bolt strutting arrangement (3) are including fixing second stand (31) on AGV chassis (1), and the upper end of second stand (31) is fixed with scalable round pin axle subassembly (32) of horizontal, flyer strutting arrangement (4) are in the frame (41) through installing on AGV chassis (41) between two flyer strutting arrangement (4) support frames (41), a slewing bearing (43) is arranged on the lifting frame (42) through a traversing mechanism, and a flying bracket (44) is fixed on the slewing bearing (43);
the hanging lug assembly (22) comprises a first bottom plate (221) fixed on the first upright post (21), a rotatable first nut (222) is clamped on the first bottom plate (221), a screw rod (223) in threaded fit is sleeved on the first nut (222), a first guide sleeve (224) is further fixed on the first bottom plate (221), a guide rod (225) in sliding fit is sleeved on the first guide sleeve (224), a connecting seat (226) is fixed at the upper ends of the screw rod (223) and the guide rod (225), and hanging lugs (2261) are arranged on the connecting seat (226); the pin shaft assembly (32) comprises a second bottom plate (321) fixed on a second upright post (31), a supporting seat (322) is arranged on the second bottom plate (321), a rotatable second nut (323) is clamped on the supporting seat (322), a second guide sleeve (324) is further fixed on the supporting seat (322), a telescopic rod (325) is arranged through the second nut (323) and the second guide sleeve (324), threads matched with the second nut (323) and a pin cutting flat opening (3251) matched with the second guide sleeve (324) are arranged on the peripheral wall of the telescopic rod (325), and a pin shaft (3252) integrated with the telescopic rod (325) is arranged at the end part of the telescopic rod (325).
2. The mobile type flying installation and debugging tool according to claim 1, wherein the first nuts (222) are provided with rotation operation holes distributed along the circumferential direction, the first guide sleeves (224) are provided with two, and the two first guide sleeves (224) are correspondingly arranged on two sides of the first nuts (222).
3. The mobile type flying installation and debugging tool according to claim 1, wherein two pin cutting flat openings (3251) are arranged, the two pin cutting flat openings (3251) are correspondingly arranged on two sides of the telescopic rod (325), and the second nut (323) is fixedly provided with a rotary hand wheel (326).
4. The mobile type flying installation and debugging tool according to claim 1, wherein the longitudinal moving mechanism comprises two first guide rails (11) longitudinally fixed on the AGV chassis (1), first sliding blocks (411) in sliding fit are arranged on the first guide rails (11), the first sliding blocks (411) are fixed on the supporting frame (41), and longitudinal moving locking screws (412) are screwed on the first sliding blocks (411).
5. The movable type flyer installation and debugging tool according to claim 4, wherein the lifting mechanism comprises two second guide rails (413) vertically fixed on the supporting frame (41), second sliding blocks (421) in sliding fit are arranged on the second guide rails (413), the second sliding blocks (421) are fixed on the lifting frame (42), the lifting mechanism further comprises a support (414) fixed on the supporting frame (41), a transmission case (415) is fixed on the support (414), two ends of a worm in the transmission case (415) are correspondingly connected with a servo motor (416) and an operation hand wheel (417), a worm wheel in the transmission case (415) is sleeved with a screw rod (418) in threaded fit, and the upper end of the screw rod (418) is fixedly connected with the lifting frame (42).
6. The mobile type flying installation and debugging tool according to claim 5, wherein the transverse moving mechanism comprises two third guide rails (422) transversely fixed on the lifting frame (42), third sliding blocks (431) in sliding fit are arranged on the third guide rails (422), transverse moving locking screws (432) are screwed on the third sliding blocks (431), and the third sliding blocks (431) are fixedly connected with the slewing bearing (43) through supporting tables (433).
7. The mobile aircraft installation and debugging tool according to claim 6, wherein the aircraft bracket (44) comprises a bracket (441), three support columns (442) are arranged on the bracket (441), and positioning columns (443) matched with positioning holes on an engine flight accessory are arranged on the support columns (442).
8. The mobile type fly attachment installation and debugging tool according to claim 1, wherein a first connecting plate (12) and a second connecting plate (13) which correspond to the ear type supporting device (2) and the bolt type supporting device (3) are fixed on the AGV chassis (1), screw holes which are distributed at intervals are formed in the first connecting plate (12) and the second connecting plate (13) respectively, grooves are formed in the position, between the two bolt type supporting devices (3), of the AGV chassis (1), the ear type supporting device (2) is fixed on the first connecting plate (12) through a first mounting hole (211) in a base of the ear type supporting device, the bolt type supporting device (3) is fixed on the second connecting plate (13) through a second mounting hole (311) in the base of the ear type supporting device, the first mounting hole (211) and the second mounting hole (311) are strip-shaped holes, and the fly attachment supporting device (4) is located in the grooves of the AGV chassis (1).
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| Application Number | Priority Date | Filing Date | Title |
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| CN202111411217.8A CN114346627B (en) | 2021-11-25 | 2021-11-25 | Portable flight attaches installation debugging frock |
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| Application Number | Priority Date | Filing Date | Title |
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| CN202111411217.8A CN114346627B (en) | 2021-11-25 | 2021-11-25 | Portable flight attaches installation debugging frock |
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| CN114346627A CN114346627A (en) | 2022-04-15 |
| CN114346627B true CN114346627B (en) | 2023-04-25 |
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| CN114858464B (en) * | 2022-07-05 | 2022-12-06 | 中国航发四川燃气涡轮研究院 | Aircraft accessory machine casket mounting bracket |
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| Publication number | Priority date | Publication date | Assignee | Title |
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| US7637471B2 (en) * | 2007-01-05 | 2009-12-29 | Gm Global Technology Operations, Inc. | Component loading tool for assembly operations |
| CN201881138U (en) * | 2010-12-15 | 2011-06-29 | 北车风电有限公司 | Large-sized wind driven generator spindle and gear case centering device |
| US10525524B2 (en) * | 2014-07-09 | 2020-01-07 | The Boeing Company | Dual-interface coupler |
| CN104999268A (en) * | 2015-07-17 | 2015-10-28 | 大连四达高技术发展有限公司 | Auxiliary airplane engine installing system |
| CN107352043B (en) * | 2017-06-26 | 2019-10-29 | 大连理工大学 | A kind of six axis posture adjustment platforms for the installation of aircraft engine complete machine |
| CN108000135B (en) * | 2017-12-05 | 2020-02-18 | 上海交通大学 | Automatic butt joint posture-adjusting positioning device for large cylindrical component with coordinated movement function |
| FR3089209B1 (en) * | 2018-12-04 | 2020-12-18 | Airbus Operations Sas | TRANSPORT AND REFERENCE TROLLEY FOR AIRCRAFT WINGS |
| CN211465350U (en) * | 2019-12-04 | 2020-09-11 | 江西洪都航空工业集团有限责任公司 | Rail butt joint movable aircraft engine tooling mechanism |
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