CN102721563A - Experimental device for simulating aircraft wing stringer assembly - Google Patents
Experimental device for simulating aircraft wing stringer assembly Download PDFInfo
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- CN102721563A CN102721563A CN2012102173928A CN201210217392A CN102721563A CN 102721563 A CN102721563 A CN 102721563A CN 2012102173928 A CN2012102173928 A CN 2012102173928A CN 201210217392 A CN201210217392 A CN 201210217392A CN 102721563 A CN102721563 A CN 102721563A
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Abstract
The invention discloses an experimental device for simulating aircraft wing stringer assembly. The experimental device comprises a test table bottom platform, a stringer, skin, and an edge longitudinal positioning device, an edge vertical positioning device, a sliding transverse support force measuring device, a slider transverse positioning device and a sliding vertical clamping device which are arranged on the test table bottom platform and connected with the stringer and the skin. The experimental device has a rational structure, is stable in positioning and can realize the simulation of different machining deformation, clamping positions and clamping force; during the simulation of the aircraft wing stringer assembling process, different machining deformation, different positioning errors, different clamping force and different clamping areas can be simulated by various devices, and the assembling deformation of the stringer when the factors change can be measured, so that the relation between the assembling deformation of the stringer and the variables can be determined, and the law of the aircraft wing stringer assembly can be disclosed. The experimental device for simulating the aircraft wing stringer assembly has the advantages of multiple variable factors and high adaptability.
Description
Technical field
The present invention relates to aircraft mounting technology field, specifically is the long purlin assembling of a kind of aircraft wing analogue experiment installation.
Background technology
China's Aviation Industry is wanted accelerated development, strides into world's rank of advanced units, and in market competition, wins certain market share, need produce the reliable product of high-quality.And the aircraft assembling is an of paramount importance ring in the aircraft manufacturing link; Have and common mechanical product assembling different features; Wherein, cause difficult quality control in its assembling, become exigence so invent a kind of experiment table that can the simulated plane wing large thin-wall element assembles and then disclose its rule thereby be prone to produce distortion in the processing because the part of aircraft wing be a large thin-wall element mostly; And long purlin typical yielding large thin-wall element in the wing just; Its length can reach about 10 meters, and assembling deviation control difficulty is so serve as the characteristics that the assembling object can reflect the wing assembling preferably to grow the purlin.
Through inquiry, existing aircraft wing type frame mainly is to improve the flexible or efficiency of assembling of assembling, but fails to study the deformation rule of assembling process.These type framves are overproof for assembling to be to force assembling through adding measures such as pad, tries hard to guarantee that part can assemble, but does not pay close attention for the rule of assembly deflections.So becoming, experiment table that can research aircraft wing part assembling process deformation rule presses for.
Summary of the invention
The present invention is directed to the above-mentioned deficiency that exists in the prior art, the long purlin assembling of a kind of aircraft wing analogue experiment installation is provided.
The present invention realizes through following technical scheme.
The long purlin assembling of a kind of aircraft wing analogue experiment installation; Comprise testing table bottom platform, long purlin and covering, and the vertical locating device in edge longitudinal locating device, edge, slip cross-brace device for measuring force, slip horizontal positioning device and the vertical clamp device that slides that are arranged on the testing table bottom platform and are connected with covering with long purlin.
The vertical locating device of said edge longitudinal locating device and edge is respectively 2, and is symmetrically distributed respectively; Said slip cross-brace device for measuring force, slip horizontal positioning device and the vertical clamp device that slides are respectively 14, and are symmetrically distributed respectively.
Said edge longitudinal locating device comprises: the replaceable location-plate in first bottom, covering support the locating piece and the first screw thread locating device; Wherein, The replaceable location-plate in said first bottom is fixed on the said experiment table bottom platform; Said covering supports locating piece and is connected with the replaceable location-plate in first bottom; And through with the replaceable location-plate in said first bottom on different bolts hole location realize the location scalable, the said first screw thread locating device supports locating piece with covering and is connected, and realizes locating scalable through the different bolts hole location that covering supports on the locating piece.
The vertical locating device in said edge comprises: transverse slider; The horizontal concrete chute and first longitudinal sliding block, wherein, being slidingly connected of said first longitudinal sliding block and experiment table bottom platform; Said horizontal concrete chute is fixedly connected with said first longitudinal sliding block, and said transverse slider and horizontal concrete chute are slidingly connected.
Said slip cross-brace device for measuring force comprises: first Displaying Meter, first pull pressure sensor, first screw gear; First upright slide block, second upright slide block, first upright slide rail; Second longitudinal sliding block, wherein, said second longitudinal sliding block and experiment table bottom platform are slidingly connected; Said first upright slide rail is fixedly connected with second longitudinal sliding block, and said first upright slide block is fixedly connected with first upright slide rail or is slidingly connected, and said second upright slide block is fixedly connected with first upright slide rail or is slidingly connected; Said first screw gear is fixedly connected with first upright slide block; Said first screw gear is fixedly connected with second upright slide block, and said first pull pressure sensor is fixedly connected with first screw gear, and said first Displaying Meter is connected with first pull pressure sensor; Said first screw gear is given said first pull pressure sensor through rocking arm rotation loading force, and said first Displaying Meter is used to read the pressure size.
Said slip horizontal positioning device comprises: the second screw thread locating device, the 3rd upright slide block, second upright slide rail; The 3rd longitudinal sliding block; Wherein, said the 3rd longitudinal sliding block and experiment table bottom platform are slidingly connected, and said second upright slide rail is fixedly connected with the 3rd longitudinal sliding block; Said the 3rd upright slide block is fixedly connected with second upright slide rail or is slidingly connected, and the said second screw thread locating device is fixedly connected with the 3rd upright slide block.
The vertical clamp device of said slip comprises: second Displaying Meter, the 4th longitudinal sliding block, the 3rd upright slide rail; The 4th upright slide block, second screw gear, second pull pressure sensor; Long purlin back-up block, the replaceable location-plate in second bottom, wherein; Said the 4th longitudinal sliding block and experiment table bottom platform are slidingly connected, and said the 3rd upright slide rail is fixedly connected with the 4th longitudinal sliding block, and said the 4th upright slide block is fixedly connected with the 3rd upright slide rail or is slidingly connected; Said second screw gear is fixedly connected with the 4th upright slide block, and said second pull pressure sensor is fixedly connected with long purlin back-up block, and said long purlin back-up block is fixedly connected with the replaceable location-plate in second bottom; The replaceable location-plate in said second bottom is connected with the experiment table bottom platform, and said second Displaying Meter is connected with second pull pressure sensor; Said second screw gear is passed to second pull pressure sensor through rocking arm rotation loading force through covering again, and said second Displaying Meter is used to read the pressure size.
The covering that said covering is positioned the edge longitudinal locating device supports locating piece, and said covering is clamped in second pull pressure sensor of the vertical clamp device that slides.
Said long purlin is positioned the transverse slider of the vertical locating device of the first screw thread locating device and edge of edge longitudinal locating device; Said long purlin is clamped between second screw gear of first pull pressure sensor of slip cross-brace device for measuring force, the second screw thread locating device of slip horizontal positioning device and the vertical clamp device that slides, and said covering is assembled together through connecting hole with long purlin.
The invention provides that structure is relatively reasonable, positioning stablity and can realize the different machining deformations of simulation, clamped position, clamping force, be used for aircraft wing and grow the experiment table that the purlin assembling process is simulated.
The present invention has adopted technique scheme, and zone assembling simulated experiment platform in the long purlin of aircraft wing comprises said experiment table bottom platform; Said edge longitudinal locating device; The vertical locating device in said edge, said slip cross-brace device for measuring force, said slip horizontal positioning device; The vertical clamp device of said slip, said long purlin covering.For the assembling process simulation of the long purlin of aircraft wing; Said various device can be simulated different machining deformations, different positioning errors, different clamping forces; Different clamping regions; And measure the assembly deflections of these factors vary duration purlins, thereby confirm the relation of long purlin assembly deflections and above-mentioned variable, be beneficial to the rule that discloses aircraft wing long purlin assembling.It is many that the present invention has variable factor, adaptable advantage.
Description of drawings
Fig. 1 is one-piece construction figure of the present invention;
Fig. 2 is an end of the present invention amplification assumption diagram;
Fig. 3 is an edge longitudinal locating device of the present invention;
Fig. 4 is the vertical locating device in edge of the present invention;
Fig. 5 is a slip cross-brace device for measuring force of the present invention;
Fig. 6 is a slip horizontal positioning device of the present invention;
Fig. 7 is the vertical clamp device of slip of the present invention;
Fig. 8 is a long purlin of the present invention covering;
Fig. 9 is an experiment table bottom platform of the present invention;
Figure 10 is the replaceable location-plate in bottom of the present invention;
Among the figure: 1. experiment table bottom platform, 2. edge longitudinal locating device, the 3. vertical locating device in edge, 4. slip cross-brace device for measuring force, 5. slip horizontal positioning device; 6. the vertical clamp device that slides, 7. covering is 8. grown the purlin, and 9. covering supports locating piece, the 10. first screw thread locating device; 11. the replaceable location-plate in first bottom, 12. transverse sliders, 13. horizontal concrete chutes, 14. first longitudinal sliding blocks, 15. first Displaying Meters; 16. first pull pressure sensor, 17. first screw gears, 18. first upright slide blocks, 19. second upright slide blocks, 20. first upright slide rails; 21. second longitudinal sliding block, 22. second screw thread locating devices, 23. the 3rd upright slide blocks, 24. second upright slide rails, 25. the 3rd longitudinal sliding blocks; 26. second Displaying Meter, 27. the 4th longitudinal sliding blocks, 28. the 3rd upright slide rails, 29. the 4th upright slide blocks; 30. second screw gear, 31. second pull pressure sensor, 32. long purlin back-up blocks, the replaceable location-plate in 33. second bottoms.
Embodiment
Elaborate in the face of embodiments of the invention down: present embodiment provided detailed embodiment and concrete operating process, but protection scope of the present invention is not limited to following embodiment being to implement under the prerequisite with technical scheme of the present invention.
Present embodiment comprises: testing table bottom platform 1, long purlin 8 and covering 7, and be arranged on the testing table bottom platform 1 and the vertical locating device in the edge longitudinal locating device 2, the edge that are connected with covering 7 with long purlin 83, slip cross-brace device for measuring force 4, slip horizontal positioning device 5 and the vertical clamp device 6 that slides.
The vertical locating device 3 in edge longitudinal locating device 2 and edge is respectively 2, and is symmetrically distributed respectively; Slip cross-brace device for measuring force 4, slip horizontal positioning device 5 and the vertical clamp device 6 that slides are respectively 14, and are symmetrically distributed respectively.
Be specially, as can beappreciated from fig. 1, the present invention can simulate different machining deformations, different positioning errors; Different clamping forces, the long purlin assembling of the aircraft wing of different clamped positions simulated experiment platform allows the long purlin maximum length of assembling can reach 9 meters, as can be seen from Figure 2 specifically comprises experiment table bottom platform 1; Edge longitudinal locating device 2, the vertical locating device 3 in edge, slip cross-brace device for measuring force 4, slip horizontal positioning device 5; The vertical clamp device 6 that slides, covering 7, long purlin 8.
The annexation that can find out them from Fig. 1, Fig. 2 is: edge longitudinal locating device 2 is done plane positioning through its replaceable web joint 11 in bottom in experiment table bottom platform 1; The vertical locating device 3 in edge is connected with experiment table bottom platform 1 through slide rail; Slip cross-brace device for measuring force 4 is connected with experiment table bottom platform 1 through slide rail; Slip horizontal positioning device 5 is connected with experiment table bottom platform 1 through slide rail; The vertical clamp device 6 that slides is done plane positioning through its replaceable web joint 33 in bottom on experiment table bottom platform 1, the vertical clamp device 6 that slides is connected with experiment table bottom platform 1 through slide rail, and covering 7 is positioned edge longitudinal locating device 2; Covering 7 is clamped in and slides between the vertical clamp device 6; Long purlin 8 is positioned edge longitudinal locating device 2, the vertical locating device 3 in edge, and long purlin 8 is clamped in slip cross-brace device for measuring force 4, slip horizontal positioning device 5, slides between the vertical clamp device 6, and covering 7 and long purlin 8 are assembled together through connecting hole.
In the present embodiment; The edge longitudinal locating device comprises: the replaceable location-plate in first bottom, covering support the locating piece and the first screw thread locating device; Wherein, The replaceable location-plate in first bottom is fixed on the experiment table bottom platform, and covering supports locating piece and is connected with the replaceable location-plate in first bottom, and through with the replaceable location-plate in first bottom on different bolts hole location realize locating scalable; The first screw thread locating device supports locating piece with covering and is connected, and realizes the location scalable through the different bolts hole location that covering supports on the locating piece.
Be specially, as can beappreciated from fig. 3, edge longitudinal locating device 2 comprises: covering supports the replaceable location-plate 11 in locating piece 9, the first screw thread locating devices, 10, the first bottoms.The replaceable location-plate 11 in first bottom is through being fixed on the experiment table bottom platform 1; Covering support locating piece 9 can through with the replaceable location-plate 11 in first bottom on different bolts hole location realize the location scalable, the first screw thread locating device 10 is realized the location scalable through supporting on the locating piece 9 different bolts hole location with covering.
In the present embodiment, the vertical locating device in edge comprises: transverse slider, the horizontal concrete chute and first longitudinal sliding block; Wherein, Being slidingly connected of first longitudinal sliding block and experiment table bottom platform, horizontal concrete chute is fixedly connected with first longitudinal sliding block, and transverse slider and horizontal concrete chute are slidingly connected.
Be specially, as can beappreciated from fig. 4, the vertical locating device 3 in edge comprises: transverse slider 12, horizontal concrete chute 13, the first longitudinal sliding blocks 14.First longitudinal sliding block 14 is through chute longitudinal sliding motion on experiment table bottom platform 1, and horizontal concrete chute 13 is connected with first longitudinal sliding block 14 through bolt, and transverse slider 12 laterally slides on horizontal concrete chute 13 through chute.
In the present embodiment, slip cross-brace device for measuring force comprises: first Displaying Meter, first pull pressure sensor; First screw gear, first upright slide block, second upright slide block; First upright slide rail, second longitudinal sliding block, wherein; Second longitudinal sliding block and experiment table bottom platform are slidingly connected, and first upright slide rail is fixedly connected with second longitudinal sliding block, and first upright slide block is fixedly connected with first upright slide rail or is slidingly connected; Second upright slide block is fixedly connected with first upright slide rail or is slidingly connected, and first screw gear is fixedly connected with first upright slide block, and first screw gear is fixedly connected with second upright slide block; First pull pressure sensor is fixedly connected with first screw gear, and first Displaying Meter is connected with first pull pressure sensor; First screw gear is given first pull pressure sensor through rocking arm rotation loading force, and first Displaying Meter is used to read the pressure size.
Be specially, as can beappreciated from fig. 5, slip cross-brace device for measuring force 4 comprises: first Displaying Meter 15; First pull pressure sensor, 16, the first screw gears, 17, the first upright slide blocks 18; Second upright slide block, 19, the first upright slide rails, 20, the second longitudinal sliding blocks 21.Second longitudinal sliding block 21 is through chute longitudinal sliding motion on experiment table bottom platform 1; First upright slide rail 20 is connected with second longitudinal sliding block 21 through bolt; First upright slide block 18 vertically slides on first upright slide rail 20 through chute; First upright slide block 18 also can be fixedly connected with first upright slide rail 20 through bolt, and second upright slide block 19 vertically slides on first upright slide rail 20 through chute, and second upright slide block 19 also can be fixedly connected with first upright slide rail 20 through bolt; First screw gear 17 is connected with first upright slide block 18 through bolt; First screw gear 17 is connected with second upright slide block 19 through bolt, and first pull pressure sensor 16 is connected with first screw gear 17 through bolt, and first Displaying Meter 15 is connected with first pull pressure sensor 16 through wire harness; First screw gear 17 can read the pressure size for first pull pressure sensor, 16, the first Displaying Meters 15 through rocking arm rotation loading force.
In the present embodiment, the slip horizontal positioning device comprises: the second screw thread locating device, the 3rd upright slide block; Second upright slide rail, the 3rd longitudinal sliding block, wherein; The 3rd longitudinal sliding block and experiment table bottom platform are slidingly connected; Second upright slide rail 24 is fixedly connected with the 3rd longitudinal sliding block, and the 3rd upright slide block is fixedly connected with second upright slide rail or is slidingly connected, and the second screw thread locating device is fixedly connected with the 3rd upright slide block.
Be specially, as can beappreciated from fig. 6, slip horizontal positioning device 5 comprises: the second screw thread locating device, 22, the three upright slide blocks, 23, the second upright slide rails, 24, the three longitudinal sliding blocks 25.The 3rd longitudinal sliding block 25 is through chute longitudinal sliding motion on experiment table bottom platform 1; Second upright slide rail 24 is connected with the 3rd longitudinal sliding block 25 through bolt; The 3rd upright slide block 23 vertically slides on second upright slide rail 24 through chute; The 3rd upright slide block 23 also can be fixedly connected with second upright slide rail 24 through bolt, and the second screw thread locating device 22 is connected with the 3rd upright slide block 23 through bolt.
In the present embodiment, the vertical clamp device that slides comprises: second Displaying Meter, the 4th longitudinal sliding block; The 3rd upright slide rail, the 4th upright slide block, second screw gear; Second pull pressure sensor, long purlin back-up block, the replaceable location-plate in second bottom; Wherein, the 4th longitudinal sliding block and experiment table bottom platform are slidingly connected, and the 3rd upright slide rail is fixedly connected with the 4th longitudinal sliding block; The 4th upright slide block is fixedly connected with the 3rd upright slide rail or is slidingly connected, and second screw gear is fixedly connected with the 4th upright slide block, and second pull pressure sensor is fixedly connected with long purlin back-up block; Long purlin back-up block is fixedly connected with the replaceable location-plate in second bottom, and the replaceable location-plate in second bottom is connected with the experiment table bottom platform, and second Displaying Meter is connected with second pull pressure sensor; Second screw gear is passed to second pull pressure sensor through rocking arm rotation loading force through covering again, and second Displaying Meter is used to read the pressure size.
Be specially, as can beappreciated from fig. 7, the vertical clamp device 6 that slides comprises: second Displaying Meter, 26, the four longitudinal sliding blocks 27; The 3rd upright slide rail 28, the four upright slide blocks 29, the second screw gears 30; Second pull pressure sensor 31, the replaceable location-plate 33 in long back-up block 32, the second bottoms, purlin.The 4th longitudinal sliding block 27 is through chute longitudinal sliding motion on experiment table bottom platform 1; The 3rd upright slide rail 28 is connected with the 4th longitudinal sliding block 27 through bolt; The 4th upright slide block 29 vertically slides on the 3rd upright slide rail 28 through chute; The 4th upright slide block 29 also can be fixedly connected with the 3rd upright slide rail 28 through bolt, and second screw gear 30 is connected with the 4th upright slide block 29 through bolt, and second pull pressure sensor 31 is connected with long purlin back-up block 32 through bolt; Long purlin back-up block 32 is connected with the replaceable location-plate 33 in second bottom; The replaceable location-plate 33 in second bottom is done plane positioning on experiment table bottom platform 1, second Displaying Meter 26 is connected with second pull pressure sensor 31 through wire harness, and second screw gear 30 can be given covering 7 through rocking arm rotation loading force; Last power will be passed to second pull pressure sensor 31, and second Displaying Meter 26 can be read the pressure size.
In the present embodiment, the covering that covering is positioned the edge longitudinal locating device supports locating piece, and covering is clamped in second pull pressure sensor of the vertical clamp device that slides.Long purlin is positioned the transverse slider of the vertical locating device of the first screw thread locating device and edge of edge longitudinal locating device; Long purlin is clamped between second screw gear of first pull pressure sensor of slip cross-brace device for measuring force, the second screw thread locating device of slip horizontal positioning device and the vertical clamp device that slides, and covering is assembled together through connecting hole with long purlin.
Be specially, as can beappreciated from fig. 8, the rigging position relation of covering 7 and long purlin 8.Covering 7 is positioned covering and supports locating piece 9; Covering 7 is clamped in second pull pressure sensor 31; Long purlin 8 is positioned the first screw thread locating device 10, transverse slider 12; Long purlin 8 is clamped between first pull pressure sensor 16, the second screw thread locating device 22, second screw gear 30, and covering 7 and long purlin 8 are assembled together through connecting hole.
The present invention slides on horizontal concrete chute 13 through transverse slider 12 and grows the lateral deviation of the multiple simulation machining deformation in purlin; Horizontal concrete chute 13 slides on first longitudinal sliding block 14 and grows the along track bias of the multiple simulation machining deformation in purlin; Horizontal concrete chute 13 can through with the joint face of first longitudinal sliding block 14 on shimming grow the vertical deflection of the multiple simulation machining deformation in purlin; The second screw thread locating device 22 can be confirmed long position location, purlin and can simulate different positioning errors; Thereby first Displaying Meter 15 can read with strained long purlin force be pushed into the assembling and positioning position force power size to know to force assembling influence size; Size reaches the control to clamping force thereby second Displaying Meter 26 can be read clamping force, and can measure is having the covering 7 under the machining deformation situation to assemble the long purlin skin morph of front and back with long purlin 8.Through above-mentioned means, the present invention can reach the different machining deformations in the simulated plane wing long purlin assembling, different deviations; Different clamping forces; Different clamped positions, thus they and the relation of long purlin assembly deflections disclosed, be that the control of aircraft wing assembly deflections proposes advisory opinion.
More than specific embodiment of the present invention is described.It will be appreciated that the present invention is not limited to above-mentioned specific implementations, those skilled in the art can make various distortion or modification within the scope of the claims, and this does not influence flesh and blood of the present invention.
Claims (9)
1. analogue experiment installation is assembled in the long purlin of aircraft wing; It is characterized in that; Comprise testing table bottom platform, long purlin and covering, and the vertical locating device in edge longitudinal locating device, edge, slip cross-brace device for measuring force, slip horizontal positioning device and the vertical clamp device that slides that are arranged on the testing table bottom platform and are connected with covering with long purlin.
2. the long purlin assembling of aircraft wing according to claim 1 analogue experiment installation is characterized in that the vertical locating device of said edge longitudinal locating device and edge is respectively 2, and is symmetrically distributed respectively; Said slip cross-brace device for measuring force, slip horizontal positioning device and the vertical clamp device that slides are respectively 14, and are symmetrically distributed respectively.
3. the long purlin assembling of aircraft wing according to claim 1 analogue experiment installation; It is characterized in that; Said edge longitudinal locating device comprises: the replaceable location-plate in first bottom, covering support the locating piece and the first screw thread locating device; Wherein, The replaceable location-plate in said first bottom is fixed on the said experiment table bottom platform, and said covering supports locating piece and is connected with the replaceable location-plate in first bottom, and through with the replaceable location-plate in said first bottom on different bolts hole location realize locating scalable; The said first screw thread locating device supports locating piece with covering and is connected, and realizes the location scalable through the different bolts hole location that covering supports on the locating piece.
4. the long purlin assembling of aircraft wing according to claim 1 analogue experiment installation; It is characterized in that the vertical locating device in said edge comprises: transverse slider, the horizontal concrete chute and first longitudinal sliding block; Wherein, Being slidingly connected of said first longitudinal sliding block and experiment table bottom platform, said horizontal concrete chute is fixedly connected with said first longitudinal sliding block, and said transverse slider and horizontal concrete chute are slidingly connected.
5. the long purlin assembling of aircraft wing according to claim 1 analogue experiment installation is characterized in that said slip cross-brace device for measuring force comprises: first Displaying Meter; First pull pressure sensor, first screw gear, first upright slide block; Second upright slide block, first upright slide rail, second longitudinal sliding block; Wherein, said second longitudinal sliding block and experiment table bottom platform are slidingly connected, and said first upright slide rail is fixedly connected with second longitudinal sliding block; Said first upright slide block is fixedly connected with first upright slide rail or is slidingly connected; Said second upright slide block is fixedly connected with first upright slide rail or is slidingly connected, and said first screw gear is fixedly connected with first upright slide block, and said first screw gear is fixedly connected with second upright slide block; Said first pull pressure sensor is fixedly connected with first screw gear, and said first Displaying Meter is connected with first pull pressure sensor; Said first screw gear is given said first pull pressure sensor through rocking arm rotation loading force, and said first Displaying Meter is used to read the pressure size.
6. the long purlin assembling of aircraft wing according to claim 1 analogue experiment installation is characterized in that said slip horizontal positioning device comprises: the second screw thread locating device; The 3rd upright slide block; Second upright slide rail, the 3rd longitudinal sliding block, wherein; Said the 3rd longitudinal sliding block and experiment table bottom platform are slidingly connected; Said second upright slide rail is fixedly connected with the 3rd longitudinal sliding block, and said the 3rd upright slide block is fixedly connected with second upright slide rail or is slidingly connected, and the said second screw thread locating device is fixedly connected with the 3rd upright slide block.
7. the long purlin assembling of aircraft wing according to claim 1 analogue experiment installation is characterized in that the vertical clamp device of said slip comprises: second Displaying Meter; The 4th longitudinal sliding block, the 3rd upright slide rail, the 4th upright slide block; Second screw gear, second pull pressure sensor, long purlin back-up block; The replaceable location-plate in second bottom, wherein, said the 4th longitudinal sliding block and experiment table bottom platform are slidingly connected; Said the 3rd upright slide rail is fixedly connected with the 4th longitudinal sliding block, and said the 4th upright slide block is fixedly connected with the 3rd upright slide rail or is slidingly connected, and said second screw gear is fixedly connected with the 4th upright slide block; Said second pull pressure sensor is fixedly connected with long purlin back-up block; Said long purlin back-up block is fixedly connected with the replaceable location-plate in second bottom, and the replaceable location-plate in said second bottom is connected with the experiment table bottom platform, and said second Displaying Meter is connected with second pull pressure sensor; Said second screw gear is passed to second pull pressure sensor through rocking arm rotation loading force through covering again, and said second Displaying Meter is used to read the pressure size.
8. the long purlin assembling of aircraft wing according to claim 1 analogue experiment installation is characterized in that the covering that said covering is positioned the edge longitudinal locating device supports locating piece, and said covering is clamped in second pull pressure sensor of the vertical clamp device that slides.
9. the long purlin assembling of aircraft wing according to claim 1 analogue experiment installation; It is characterized in that; Said long purlin is positioned the transverse slider of the vertical locating device of the first screw thread locating device and edge of edge longitudinal locating device; Said long purlin is clamped between second screw gear of first pull pressure sensor of slip cross-brace device for measuring force, the second screw thread locating device of slip horizontal positioning device and the vertical clamp device that slides, and said covering is assembled together through connecting hole with long purlin.
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| Application Number | Priority Date | Filing Date | Title |
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| CN201210217392.8A CN102721563B (en) | 2012-06-28 | 2012-06-28 | Experimental device for simulating aircraft wing stringer assembly |
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| CN201210217392.8A CN102721563B (en) | 2012-06-28 | 2012-06-28 | Experimental device for simulating aircraft wing stringer assembly |
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| CN102721563A true CN102721563A (en) | 2012-10-10 |
| CN102721563B CN102721563B (en) | 2014-10-15 |
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| CN102980750A (en) * | 2012-11-09 | 2013-03-20 | 上海交通大学 | Aircraft wing long purlin assembling process and automatic simulation experiment set of clamp force |
| CN103376233A (en) * | 2013-07-05 | 2013-10-30 | 上海交通大学 | R angle deviation detection and prestressing force infliction experiment table for composite material C-type beam |
| CN103934682A (en) * | 2014-04-14 | 2014-07-23 | 上海交通大学 | Assembling simulation experiment table for aircraft wing wedge-shaped spar |
| CN105109706A (en) * | 2015-08-26 | 2015-12-02 | 西北工业大学 | Locating and gripping experimental device for aircraft thin-wall parts |
| CN105500698A (en) * | 2016-01-20 | 2016-04-20 | 哈尔滨飞机工业集团有限责任公司 | Clamping device connected with skin assembly |
| CN105912823A (en) * | 2016-05-12 | 2016-08-31 | 电子科技大学 | N-2-1 positioning based skin and stringer assembling deviation analyzing method of airplane |
| CN107140231A (en) * | 2017-04-27 | 2017-09-08 | 浙江大学 | A kind of wing tip rib alignment system and positioner |
| CN107414711A (en) * | 2017-07-31 | 2017-12-01 | 中航通飞华南飞机工业有限公司 | A kind of new rear body is glued assembling jig |
| CN109460599A (en) * | 2018-10-30 | 2019-03-12 | 南昌航空大学 | A kind of the transmitting quantization analysis method and system of assembly features deviation |
| CN110877221A (en) * | 2019-12-04 | 2020-03-13 | 北京神工科技有限公司 | Stringer skin tool structure |
| CN114261531A (en) * | 2021-12-21 | 2022-04-01 | 电子科技大学 | Intelligent flexible clamping equipment for wing |
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| CN102980750B (en) * | 2012-11-09 | 2015-07-08 | 上海交通大学 | Aircraft wing long purlin assembling process and automatic simulation experiment set of clamp force |
| CN102980750A (en) * | 2012-11-09 | 2013-03-20 | 上海交通大学 | Aircraft wing long purlin assembling process and automatic simulation experiment set of clamp force |
| CN103376233A (en) * | 2013-07-05 | 2013-10-30 | 上海交通大学 | R angle deviation detection and prestressing force infliction experiment table for composite material C-type beam |
| CN103376233B (en) * | 2013-07-05 | 2016-02-10 | 上海交通大学 | Composite material C-type beam R angular displacement detection and prestress application experiment table |
| CN103934682A (en) * | 2014-04-14 | 2014-07-23 | 上海交通大学 | Assembling simulation experiment table for aircraft wing wedge-shaped spar |
| CN103934682B (en) * | 2014-04-14 | 2016-04-13 | 上海交通大学 | Aircraft wing wedged spars assembly simulation experimental bench |
| CN105109706A (en) * | 2015-08-26 | 2015-12-02 | 西北工业大学 | Locating and gripping experimental device for aircraft thin-wall parts |
| CN105109706B (en) * | 2015-08-26 | 2017-05-31 | 西北工业大学 | One kind is used for aircraft thin-wall part positioning clamping experimental provision |
| CN105500698A (en) * | 2016-01-20 | 2016-04-20 | 哈尔滨飞机工业集团有限责任公司 | Clamping device connected with skin assembly |
| CN105912823B (en) * | 2016-05-12 | 2018-11-20 | 电子科技大学 | Aircraft skin and stringer assembling deviation analysis method based on N-2-1 positioning |
| CN105912823A (en) * | 2016-05-12 | 2016-08-31 | 电子科技大学 | N-2-1 positioning based skin and stringer assembling deviation analyzing method of airplane |
| CN107140231A (en) * | 2017-04-27 | 2017-09-08 | 浙江大学 | A kind of wing tip rib alignment system and positioner |
| CN107414711A (en) * | 2017-07-31 | 2017-12-01 | 中航通飞华南飞机工业有限公司 | A kind of new rear body is glued assembling jig |
| CN107414711B (en) * | 2017-07-31 | 2023-12-22 | 中航通飞华南飞机工业有限公司 | Novel assembly jig for cementing of rear machine body |
| CN109460599A (en) * | 2018-10-30 | 2019-03-12 | 南昌航空大学 | A kind of the transmitting quantization analysis method and system of assembly features deviation |
| CN109460599B (en) * | 2018-10-30 | 2022-06-28 | 南昌航空大学 | Transmission quantitative analysis method and system for assembly characteristic deviation |
| CN110877221A (en) * | 2019-12-04 | 2020-03-13 | 北京神工科技有限公司 | Stringer skin tool structure |
| CN110877221B (en) * | 2019-12-04 | 2021-11-09 | 北京神工科技有限公司 | Stringer skin tool structure |
| CN114261531A (en) * | 2021-12-21 | 2022-04-01 | 电子科技大学 | Intelligent flexible clamping equipment for wing |
| CN114261531B (en) * | 2021-12-21 | 2023-04-11 | 电子科技大学 | Intelligent flexible clamping equipment for wing |
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