CN110375073A - 一种机匣端面密封结构 - Google Patents
一种机匣端面密封结构 Download PDFInfo
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- CN110375073A CN110375073A CN201910627973.0A CN201910627973A CN110375073A CN 110375073 A CN110375073 A CN 110375073A CN 201910627973 A CN201910627973 A CN 201910627973A CN 110375073 A CN110375073 A CN 110375073A
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- 108090000565 Capsid Proteins Proteins 0.000 claims abstract description 8
- 238000004073 vulcanization Methods 0.000 claims abstract description 6
- 238000003032 molecular docking Methods 0.000 claims abstract description 4
- 239000000463 material Substances 0.000 claims description 8
- 229910000838 Al alloy Inorganic materials 0.000 claims description 3
- 239000003292 glue Substances 0.000 claims description 3
- YCKRFDGAMUMZLT-UHFFFAOYSA-N Fluorine atom Chemical compound [F] YCKRFDGAMUMZLT-UHFFFAOYSA-N 0.000 claims 1
- 239000004411 aluminium Substances 0.000 claims 1
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical group [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 claims 1
- 229910052782 aluminium Inorganic materials 0.000 claims 1
- 229910052731 fluorine Inorganic materials 0.000 claims 1
- 239000011737 fluorine Substances 0.000 claims 1
- 229910052751 metal Inorganic materials 0.000 claims 1
- 239000002184 metal Substances 0.000 claims 1
- 238000012856 packing Methods 0.000 claims 1
- 238000007789 sealing Methods 0.000 abstract description 12
- 238000005457 optimization Methods 0.000 abstract description 2
- 238000000034 method Methods 0.000 description 4
- 238000010586 diagram Methods 0.000 description 2
- 239000003921 oil Substances 0.000 description 2
- FYYHWMGAXLPEAU-UHFFFAOYSA-N Magnesium Chemical compound [Mg] FYYHWMGAXLPEAU-UHFFFAOYSA-N 0.000 description 1
- 239000000956 alloy Substances 0.000 description 1
- 239000010425 asbestos Substances 0.000 description 1
- 238000005266 casting Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- PCHJSUWPFVWCPO-UHFFFAOYSA-N gold Chemical compound [Au] PCHJSUWPFVWCPO-UHFFFAOYSA-N 0.000 description 1
- 239000010931 gold Substances 0.000 description 1
- 229910052737 gold Inorganic materials 0.000 description 1
- 239000010687 lubricating oil Substances 0.000 description 1
- 229910052749 magnesium Inorganic materials 0.000 description 1
- 239000011777 magnesium Substances 0.000 description 1
- 230000013011 mating Effects 0.000 description 1
- 239000000203 mixture Substances 0.000 description 1
- 238000003825 pressing Methods 0.000 description 1
- 229910052895 riebeckite Inorganic materials 0.000 description 1
- 239000000565 sealant Substances 0.000 description 1
- 230000003746 surface roughness Effects 0.000 description 1
Classifications
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16H—GEARING
- F16H57/00—General details of gearing
- F16H57/02—Gearboxes; Mounting gearing therein
- F16H57/029—Gearboxes; Mounting gearing therein characterised by means for sealing the gearboxes, e.g. to improve airtightness
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16J—PISTONS; CYLINDERS; SEALINGS
- F16J15/00—Sealings
- F16J15/02—Sealings between relatively-stationary surfaces
- F16J15/06—Sealings between relatively-stationary surfaces with solid packing compressed between sealing surfaces
- F16J15/10—Sealings between relatively-stationary surfaces with solid packing compressed between sealing surfaces with non-metallic packing
- F16J15/102—Sealings between relatively-stationary surfaces with solid packing compressed between sealing surfaces with non-metallic packing characterised by material
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16J—PISTONS; CYLINDERS; SEALINGS
- F16J15/00—Sealings
- F16J15/02—Sealings between relatively-stationary surfaces
- F16J15/06—Sealings between relatively-stationary surfaces with solid packing compressed between sealing surfaces
- F16J15/10—Sealings between relatively-stationary surfaces with solid packing compressed between sealing surfaces with non-metallic packing
- F16J15/104—Sealings between relatively-stationary surfaces with solid packing compressed between sealing surfaces with non-metallic packing characterised by structure
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16J—PISTONS; CYLINDERS; SEALINGS
- F16J15/00—Sealings
- F16J15/02—Sealings between relatively-stationary surfaces
- F16J15/06—Sealings between relatively-stationary surfaces with solid packing compressed between sealing surfaces
- F16J15/10—Sealings between relatively-stationary surfaces with solid packing compressed between sealing surfaces with non-metallic packing
- F16J15/12—Sealings between relatively-stationary surfaces with solid packing compressed between sealing surfaces with non-metallic packing with metal reinforcement or covering
- F16J15/121—Sealings between relatively-stationary surfaces with solid packing compressed between sealing surfaces with non-metallic packing with metal reinforcement or covering with metal reinforcement
- F16J15/122—Sealings between relatively-stationary surfaces with solid packing compressed between sealing surfaces with non-metallic packing with metal reinforcement or covering with metal reinforcement generally parallel to the surfaces
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- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Gasket Seals (AREA)
Abstract
本技术方案涉及机匣端面的密封,特别涉及一种包括金属密封垫的端面密封结构。所述的结构包括前壳体(1)、后壳体(2)和金属密封垫(3),金属密封垫(3)被压紧在前壳体(1)和后壳体(2)的对接端面上;所述金属密封垫(3)的两侧端面上开有凹槽;所述凹槽内开有贯通两侧凹槽的通孔(32);所述凹槽和通孔(32)内硫化有橡胶。该设计,通过增加了金属密封垫提高了密封寿命和装配效率。同时优化的密封垫结构,结构形式简单,密封可靠性高。
Description
技术领域
本技术方案涉及机匣端面的密封,特别涉及一种包括金属密封垫的端面密封结构。
背景技术
在传统附件传动系统结构中,机匣壳体端面密封是常见的密封结构,机匣壳体端面密封性能至关重要。机匣壳体端面密封一般为耐油石棉橡胶垫上涂抹“乐泰587”密封胶后,装配于机匣壳体结合面上的方式,耐油石棉橡胶垫弹性差,压紧力不均匀,可能会导致附件机匣偏斜,从而引起齿轮偏斜等问题,而且石棉密封垫更换频繁,报废率高。因此密封可靠性稍差,使用成本高。
发明内容
本发明解决的技术问题:提供一种密封可靠性高、寿命长的机匣端面密封结构。
本发明的技术方案:一种机匣端面密封结构,所述的结构包括前壳体、后壳体和金属密封垫,金属密封垫被压紧在前壳体和后壳体的对接端面上;所述金属密封垫的两侧端面上开有凹槽;所述凹槽内开有贯通两侧凹槽的通孔;所述凹槽和通孔内硫化有橡胶。该设计,通过增加了金属密封垫提高了密封寿命和装配效率。同时优化的密封垫结构,结构形式简单,密封可靠性高。
优选地,金属密封垫上的结合面上全部设置有凹槽。该设计保证了所有端面接触部位都能实现密封。
优选地,所述的金属密封垫为铝合金材料,该设计便于加工,材料成本低。
优选地,所述的金属密封垫厚度为2-4mm。该设计一方面充分考虑了密封的可靠性,另一方面最大限度减低了结构的质量。
优选地,所述的橡胶材料为氟橡胶,该设计密封效果好,材料成本低。
附图说明
图1为机匣端面装配结构示意图;
图2为金属密封垫骨架结构示意图。
具体实施方式
如图1所示,所述的结构包括前壳体1、后壳体2和金属密封垫3,金属密封垫3被压紧在前壳体1和后壳体2的对接端面上。如图2所示,所述的金属密封垫3由金属骨架33和橡胶组成,该结构利用一种将橡胶硫化到金属骨架33胶圈槽31的设计方法。金属骨架33材料选择质量轻、易加工的铝合金2A12,骨架厚度为3mm,公差为±0.03,骨架正反两面分别为深度1mm的胶圈槽。同时金属骨架33的胶圈槽31上分布着59处φ1.8通孔32,硫化的橡胶通过这些孔,将正反两面的硫化胶圈固定到金属骨架上。橡胶材料为氟橡胶FX-4。与金属密封垫相配零件为前、后两个壳体,壳体材料均为铸镁(ZM6),前、后壳体与金属密封垫接触的端面的表面粗糙度为1.6um。该金属密封垫工作密封介质为滑油4106;工作温度范围为-55℃~+120℃;工作压力为50kPa,密封检查压力0.1~0.15MPa。该结构不需要在机匣壳体上加工胶圈槽,提高机匣加工工艺性。
Claims (6)
1.一种机匣端面密封结构,其特征为:所述的结构包括前壳体(1)、后壳体(2)和金属密封垫(3),金属密封垫(3)被压紧在前壳体(1)和后壳体(2)的对接端面上;
所述金属密封垫(3)的两侧端面上开有凹槽;
所述凹槽内开有贯通两侧凹槽的通孔(32);
所述凹槽和通孔(32)内硫化有橡胶。
2.根据权利要求1所述的一种机匣端面密封结构,其特征为:金属密封垫上的结合面上全部设置有凹槽。
3.根据权利要求1所述的一种机匣端面密封结构,其特征为:所述的金属密封垫为铝合金材料。
4.根据权利要求3所述的一种机匣端面密封结构,其特征为:铝合金型号为2A12,骨架厚度为3mm。
5.根据权利要求1所述的一种机匣端面密封结构,其特征为:所述的金属密封垫厚度为2-4mm。
6.根据权利要求1所述的一种机匣端面密封结构,其特征为:所述的橡胶材料为氟橡胶。
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Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN203051760U (zh) * | 2012-11-21 | 2013-07-10 | 哈尔滨东安发动机(集团)有限公司 | 密封垫片 |
CN204127530U (zh) * | 2014-10-28 | 2015-01-28 | 中国航空工业集团公司西安飞机设计研究所 | 一种法兰密封装置 |
CN205503981U (zh) * | 2016-04-12 | 2016-08-24 | 哈尔滨东安发动机(集团)有限公司 | 一种组合式密封垫片 |
CN206310128U (zh) * | 2016-12-26 | 2017-07-07 | 沈阳第四橡胶(厂)有限公司 | 一种带金属骨架的橡胶密封垫 |
CN210531603U (zh) * | 2019-07-09 | 2020-05-15 | 中国航发哈尔滨东安发动机有限公司 | 一种机匣端面密封结构 |
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2019
- 2019-07-11 CN CN201910627973.0A patent/CN110375073A/zh active Pending
Patent Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN203051760U (zh) * | 2012-11-21 | 2013-07-10 | 哈尔滨东安发动机(集团)有限公司 | 密封垫片 |
CN204127530U (zh) * | 2014-10-28 | 2015-01-28 | 中国航空工业集团公司西安飞机设计研究所 | 一种法兰密封装置 |
CN205503981U (zh) * | 2016-04-12 | 2016-08-24 | 哈尔滨东安发动机(集团)有限公司 | 一种组合式密封垫片 |
CN206310128U (zh) * | 2016-12-26 | 2017-07-07 | 沈阳第四橡胶(厂)有限公司 | 一种带金属骨架的橡胶密封垫 |
CN210531603U (zh) * | 2019-07-09 | 2020-05-15 | 中国航发哈尔滨东安发动机有限公司 | 一种机匣端面密封结构 |
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