CN101975329A - A support device with aluminum honeycomb sandwich and carbon fiber skin - Google Patents
A support device with aluminum honeycomb sandwich and carbon fiber skin Download PDFInfo
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- CN101975329A CN101975329A CN 201010521738 CN201010521738A CN101975329A CN 101975329 A CN101975329 A CN 101975329A CN 201010521738 CN201010521738 CN 201010521738 CN 201010521738 A CN201010521738 A CN 201010521738A CN 101975329 A CN101975329 A CN 101975329A
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- metal
- metal connecting
- carbon fiber
- support device
- aluminum honeycomb
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- 229920000049 Carbon (fiber) Polymers 0.000 title claims abstract description 22
- 239000004917 carbon fiber Substances 0.000 title claims abstract description 22
- 229910052782 aluminium Inorganic materials 0.000 title claims abstract description 21
- VNWKTOKETHGBQD-UHFFFAOYSA-N methane Chemical compound C VNWKTOKETHGBQD-UHFFFAOYSA-N 0.000 title claims abstract description 21
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 title claims abstract description 20
- 239000002184 metal Substances 0.000 claims abstract description 93
- 229910052751 metal Inorganic materials 0.000 claims abstract description 90
- 239000011229 interlayer Substances 0.000 claims description 11
- 229910001069 Ti alloy Inorganic materials 0.000 claims description 4
- 239000012790 adhesive layer Substances 0.000 claims description 3
- 229910001092 metal group alloy Inorganic materials 0.000 claims description 3
- 239000010936 titanium Substances 0.000 claims description 3
- 239000004411 aluminium Substances 0.000 claims 7
- 239000010410 layer Substances 0.000 description 3
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 description 2
- 239000003292 glue Substances 0.000 description 2
- 229910052719 titanium Inorganic materials 0.000 description 2
- 238000010586 diagram Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 238000000034 method Methods 0.000 description 1
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Abstract
本发明涉及一种带有铝蜂窝夹层和碳纤维蒙皮的支撑装置,包括支撑板,所述支撑板包括铝蜂窝夹层以及固定在铝蜂窝夹层两侧面的碳纤维蒙皮,其还包括一个金属连接环以及至少三个金属连接座;金属连接环均匀分布有与金属连接座数量相应且向外凸出的连接耳片;连接耳片上设置有多个通孔;金属连接座包括与连接耳片形状相应的金属连接片以及与金属连接片垂直固连的金属连接柱,金属连接柱内设置有多个螺纹孔;支撑板的外圆周均匀分布有与金属连接柱形状相适应的多个缺口。本发明解决了现有的支撑装置强度不高、稳定性不好、精度低的技术问题,本发明具有强度高、稳定性好、精度高、重量轻等的优点。
The invention relates to a support device with an aluminum honeycomb sandwich and a carbon fiber skin, comprising a support plate, the support plate including an aluminum honeycomb sandwich and carbon fiber skins fixed on both sides of the aluminum honeycomb sandwich, and a metal connecting ring And at least three metal connecting seats; the metal connecting ring is evenly distributed with connecting lugs corresponding to the number of metal connecting seats and protruding outward; the connecting lugs are provided with a plurality of through holes; the metal connecting seat includes a shape corresponding to the shape of the connecting lugs The metal connecting piece and the metal connecting column vertically fixed to the metal connecting piece, the metal connecting column is provided with a plurality of threaded holes; the outer circumference of the support plate is evenly distributed with a plurality of gaps suitable for the shape of the metal connecting column. The invention solves the technical problems of low strength, poor stability and low precision of the existing support device, and the invention has the advantages of high strength, good stability, high precision and light weight.
Description
技术领域technical field
本发明涉及一种带有铝蜂窝夹层和碳纤维蒙皮的支撑装置。The invention relates to a supporting device with an aluminum honeycomb interlayer and a carbon fiber skin.
背景技术Background technique
现有的支撑装置有两种结构,一种是由铝蜂窝夹层和碳纤维蒙皮构成,但是由于碳纤维蒙皮精度不够,不能满足需要。因此就出现了第二种支撑装置,就在第一种结构的基础上在碳纤维蒙皮上设置金属层,通过胶接和螺钉连接固定在碳纤维蒙皮上,这种结构虽然相对前一种结构提高了精度,但是因为仅仅依靠胶接和螺钉连接的方式不能将金属层与碳纤维蒙皮很好的固定连接,强度不高、稳定性不好,还是不能满足精度的要求。The existing supporting device has two structures, one is composed of aluminum honeycomb interlayer and carbon fiber skin, but the precision of the carbon fiber skin is not enough to meet the needs. Therefore, the second supporting device appeared, which is based on the first structure, on which a metal layer is set on the carbon fiber skin, and fixed on the carbon fiber skin by bonding and screwing, although this structure is relatively The accuracy is improved, but because the metal layer and the carbon fiber skin cannot be fixed and connected only by glue and screw connection, the strength is not high and the stability is not good, which still cannot meet the accuracy requirements.
发明内容Contents of the invention
为了解决现有的支撑装置强度不高、稳定性不好、精度低的技术问题,本发明提供一种通过金属接头将金属层很好地固定在碳纤维蒙皮上的支撑装置。In order to solve the technical problems of low strength, poor stability and low precision of the existing support device, the present invention provides a support device that well fixes the metal layer on the carbon fiber skin through metal joints.
本发明的技术方案为:Technical scheme of the present invention is:
一种带有铝蜂窝夹层和碳纤维蒙皮的支撑装置,包括支撑板2,所述支撑板2包括铝蜂窝夹层21以及固定在铝蜂窝夹层两侧面的碳纤维蒙皮22,其特殊之处在于:其还包括一个金属连接环1以及至少三个金属连接座3;A support device with an aluminum honeycomb sandwich and a carbon fiber skin, including a
所述金属连接环1均匀分布有与金属连接座3数量相应且向外凸出的连接耳片11;所述连接耳片11上设置有多个通孔12;The metal connecting ring 1 is evenly distributed with connecting
所述金属连接座3包括与连接耳片11形状相应的金属连接片31以及与金属连接片31垂直固连的金属连接柱32,所述金属连接柱32内设置有多个螺纹孔33;The
所述支撑板2的外圆周均匀分布有与金属连接柱32形状相适应的多个缺口;所述缺口的数量与金属连接座3的数量一致。The outer circumference of the
所述金属连接柱32分别镶嵌于相应的缺口中,所述金属连接座3和金属连接环1分别位于支撑板2的两侧;所述多个螺钉4穿过金属连接环1的通孔12后拧在金属连接柱的相应螺纹孔33内。The
上述的金属连接片31与支撑板2之间以及金属连接环1与支撑板2之间设置有胶粘层。Adhesive layers are provided between the
上述金属连接柱32的外侧面设置有端部外露的螺纹杆5。The outer surface of the
上述金属连接座3的数量为三个。The number of the above-mentioned
上述金属连接环1、金属连接座3为钛金属或钛合金。The above-mentioned metal connection ring 1 and
本发明的技术效果为:Technical effect of the present invention is:
1、强度高。本发明在支撑板上很牢固的设置了金属连接环和金属连接座,使其和支撑板结合紧密,提高了支撑装置的强度。1. High strength. In the present invention, a metal connection ring and a metal connection seat are firmly arranged on the support plate, so that they are closely combined with the support plate, and the strength of the support device is improved.
2、稳定性好、精度高。本发明采用胶接和螺接的方式将金属连接环和金属连接座金属很好的固定在支撑板上,提高了支撑装置的稳定性和精度。2. Good stability and high precision. In the present invention, the metal connection ring and the metal connection seat are well fixed on the support plate by means of glue connection and screw connection, thereby improving the stability and precision of the support device.
3、重量轻。铝蜂窝夹层、碳纤维蒙皮结构本身重量轻,本发明的金属接头采用钛合金,重量轻。3. Light weight. The aluminum honeycomb interlayer and the carbon fiber skin structure are light in weight, and the metal joint of the present invention is made of titanium alloy, which is light in weight.
4、本发明在金属连接柱的外侧面设置有端部外露的螺纹杆,便于支撑和吊装。4. In the present invention, a threaded rod with an exposed end is provided on the outer surface of the metal connecting column, which is convenient for support and hoisting.
附图说明Description of drawings
图1为本发明金属连接环的结构示意图;其中1-1为主视图,1-2为侧视图,1-3为立体图;Fig. 1 is the structural representation of metal connection ring of the present invention; Wherein 1-1 is main view, 1-2 is side view, 1-3 is perspective view;
图2为本发明金属连接环与金属连接座连接后的结构示意图;其中2-1为俯视图,2-2为侧视图,2-3为立体图;Fig. 2 is a schematic structural view of the metal connection ring and the metal connection seat of the present invention after being connected; wherein 2-1 is a top view, 2-2 is a side view, and 2-3 is a perspective view;
图3为本发明金属连接座的结构示意图;其中3-1为主视图,3-2为侧视图,3-3为立体图,3-4为立体图;Fig. 3 is a schematic structural view of the metal connecting seat of the present invention; wherein 3-1 is a front view, 3-2 is a side view, 3-3 is a perspective view, and 3-4 is a perspective view;
图4为本发明支撑板、金属连接环、金属连接座的结构示意图;其中4-1为立体图,4-2为侧视图,4-3为图4-2中的A部放大剖视图;Fig. 4 is a schematic structural view of a support plate, a metal connecting ring, and a metal connecting seat of the present invention; wherein 4-1 is a perspective view, 4-2 is a side view, and 4-3 is an enlarged sectional view of part A in Fig. 4-2;
图5为本发明金属连接座螺纹杆的位置示意图:其中5-1为从右侧看的立体图,5-2为主视图,5-3为从左侧看的立体图;Fig. 5 is a schematic diagram of the position of the threaded rod of the metal connecting seat of the present invention: 5-1 is a perspective view from the right side, 5-2 is the main view, and 5-3 is a perspective view from the left side;
其中附图标记如下:1-金属连接环,11-连接耳片,12-通孔,2-支撑板,21-铝蜂窝夹层,22-碳纤维蒙皮,3-金属连接座,31-金属连接片,32-金属连接柱,33-螺纹孔,4-螺钉,5-螺纹杆。The reference signs are as follows: 1-metal connection ring, 11-connection lug, 12-through hole, 2-support plate, 21-aluminum honeycomb interlayer, 22-carbon fiber skin, 3-metal connection seat, 31-metal connection piece, 32-metal connecting post, 33-threaded hole, 4-screw, 5-threaded rod.
具体实施方式Detailed ways
如图1、图2所示,一种带有铝蜂窝夹层和碳纤维蒙皮的支撑装置,包括支撑板2,支撑板2包括铝蜂窝夹层21以及固定在铝蜂窝夹层两侧面的碳纤维蒙皮22,还包括一个金属连接环1以及至少三个金属连接座3;金属连接座一般为3个。金属连接环1均匀分布有与金属连接座3数量相应的向外凸出的连接耳片11;连接耳片11上设置有多个通孔12。As shown in Figures 1 and 2, a support device with an aluminum honeycomb sandwich and a carbon fiber skin includes a
如图3所示,金属连接座3包括与连接耳片11形状相应的金属连接片31以及与金属连接片31垂直固连的金属连接柱32,金属连接柱32内设置有多个螺纹孔33。As shown in Figure 3, the
如图4所示,支撑板2的外圆周均匀分布有与金属连接柱32形状相适应的多个缺口;缺口的数量与金属连接座3的数量一致。金属连接柱32分别镶嵌于支撑板2上相应的缺口中,金属连接座3和金属连接环1分别位于支撑板2的两侧;多个螺钉4穿过金属连接环1的通孔12后拧在金属连接柱的相应螺纹孔33内。所述的金属连接片31与支撑板2之间以及金属连接环1与支撑板2之间设置有胶粘层。所述金属连接环1、金属连接座3为钛金属或钛合金。As shown in FIG. 4 , the outer circumference of the
如图5所示,金属连接柱的外侧面设置有端部外露的螺纹杆8。As shown in FIG. 5 , a threaded
Claims (5)
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CN2010105217384A CN101975329B (en) | 2010-10-27 | 2010-10-27 | Support arrangement with aluminium honeycomb intermediate layer and carbon fiber covering |
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CN2010105217384A CN101975329B (en) | 2010-10-27 | 2010-10-27 | Support arrangement with aluminium honeycomb intermediate layer and carbon fiber covering |
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CN101975329A true CN101975329A (en) | 2011-02-16 |
CN101975329B CN101975329B (en) | 2012-07-04 |
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Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN109291518A (en) * | 2018-10-25 | 2019-02-01 | 北京卫星制造厂有限公司 | A kind of the solidified forming tooling and method of honeycomb sandwich construction |
CN109590921A (en) * | 2018-11-08 | 2019-04-09 | 宜兴市融兴铸造有限公司 | Satellite skin drilling and riveting tooling underframe assembly |
CN113165307A (en) * | 2018-12-13 | 2021-07-23 | 三菱电机株式会社 | Honeycomb sandwich panel, optical device and artificial satellite |
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US4241892A (en) * | 1979-08-31 | 1980-12-30 | Boone Box Co. | Appliance skidboard and method of making |
US6264157B1 (en) * | 1997-09-16 | 2001-07-24 | Sonoco Development, Inc. | Appliance base pad |
CN101472687A (en) * | 2006-06-27 | 2009-07-01 | 赫克赛尔公司 | Corrosion resistant honeycomb |
CN101574589A (en) * | 2009-06-05 | 2009-11-11 | 总装备部工程设计研究总院 | Composite material used for large stage prop |
CN201897045U (en) * | 2010-10-27 | 2011-07-13 | 中国科学院西安光学精密机械研究所 | Support arrangement with aluminium honeycomb intermediate layer and carbon fiber covering |
-
2010
- 2010-10-27 CN CN2010105217384A patent/CN101975329B/en not_active Expired - Fee Related
Patent Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
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US4241892A (en) * | 1979-08-31 | 1980-12-30 | Boone Box Co. | Appliance skidboard and method of making |
US6264157B1 (en) * | 1997-09-16 | 2001-07-24 | Sonoco Development, Inc. | Appliance base pad |
CN101472687A (en) * | 2006-06-27 | 2009-07-01 | 赫克赛尔公司 | Corrosion resistant honeycomb |
CN101574589A (en) * | 2009-06-05 | 2009-11-11 | 总装备部工程设计研究总院 | Composite material used for large stage prop |
CN201897045U (en) * | 2010-10-27 | 2011-07-13 | 中国科学院西安光学精密机械研究所 | Support arrangement with aluminium honeycomb intermediate layer and carbon fiber covering |
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN109291518A (en) * | 2018-10-25 | 2019-02-01 | 北京卫星制造厂有限公司 | A kind of the solidified forming tooling and method of honeycomb sandwich construction |
CN109291518B (en) * | 2018-10-25 | 2020-05-12 | 北京卫星制造厂有限公司 | Curing forming tool and method for honeycomb sandwich structure |
CN109590921A (en) * | 2018-11-08 | 2019-04-09 | 宜兴市融兴铸造有限公司 | Satellite skin drilling and riveting tooling underframe assembly |
CN113165307A (en) * | 2018-12-13 | 2021-07-23 | 三菱电机株式会社 | Honeycomb sandwich panel, optical device and artificial satellite |
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