CN108754265A - 一种耐腐蚀无人机壳体材料 - Google Patents

一种耐腐蚀无人机壳体材料 Download PDF

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Publication number
CN108754265A
CN108754265A CN201810560401.0A CN201810560401A CN108754265A CN 108754265 A CN108754265 A CN 108754265A CN 201810560401 A CN201810560401 A CN 201810560401A CN 108754265 A CN108754265 A CN 108754265A
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China
Prior art keywords
corrosion
unmanned plane
resistant
case material
plane case
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CN201810560401.0A
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Inventor
桂骏
桂峰
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Wuhu Journey Electronic Technology Co Ltd
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Wuhu Journey Electronic Technology Co Ltd
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Priority to CN201810560401.0A priority Critical patent/CN108754265A/zh
Publication of CN108754265A publication Critical patent/CN108754265A/zh
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    • C—CHEMISTRY; METALLURGY
    • C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22C—ALLOYS
    • C22C23/00—Alloys based on magnesium
    • C22C23/02—Alloys based on magnesium with aluminium as the next major constituent
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
    • C—CHEMISTRY; METALLURGY
    • C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22C—ALLOYS
    • C22C21/00—Alloys based on aluminium
    • C22C21/06—Alloys based on aluminium with magnesium as the next major constituent
    • C22C21/08—Alloys based on aluminium with magnesium as the next major constituent with silicon
    • C—CHEMISTRY; METALLURGY
    • C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22C—ALLOYS
    • C22C30/00—Alloys containing less than 50% by weight of each constituent
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
    • B64C2001/0054—Fuselage structures substantially made from particular materials
    • B64C2001/0081—Fuselage structures substantially made from particular materials from metallic materials

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  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Materials Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Powder Metallurgy (AREA)
  • Ceramic Products (AREA)

Abstract

本发明公开了一种耐腐蚀无人机壳体材料，包括以下组份和各组分所占重量百分比为：Ti1.5％‑8.5％、Ta0.5％‑1.5％、Nd0.2％‑0.7％、Si2％‑8％、Al30％‑45％、Ba1％‑3％、In0.1％‑0.8％，余量为Mg。该种耐腐蚀无人机壳体材料能够适应各种温度变化，耐高温和低温，具有较好的抗疲劳性和机械性。

Description

一种耐腐蚀无人机壳体材料
技术领域
本发明涉及无人机技术领域，更具体地说，特别涉及一种耐腐蚀无人机壳体材料。
背景技术
复合材料是一种混合物。在很多领域都发挥了很大的作用，代替了很多传统的材料。复合材料按其组成分为金属与金属复合材料、非金属与金属复合材料、非金属与非金属复合材料。纵观国外无人机(包括中、高空无人侦察机、无人作战飞机等)，无一例外地大量使用了复合材料结构，有些甚至是全复合材料结构，但是这些材料耐腐蚀性能较差。因此，我们提出一种耐腐蚀无人机壳体材料。
发明内容
本发明要解决的技术问题是克服现有技术的缺陷，提供一种耐腐蚀无人机壳体材料。
为了解决上述技术问题，本发明提供了如下的技术方案：
一种耐腐蚀无人机壳体材料，包括以下组份和各组分所占重量百分比为：Ti1.5％-8.5％、Ta0.5％-1.5％、Nd0.2％-0.7％、Si2％-8％、Al30％-45％、Ba1％-3％、In0.1％-0.8％，余量为Mg。
与现有技术相比，本发明的优点在于：该种耐腐蚀无人机壳体材料能够适应各种温度变化，耐高温和低温，具有较好的抗疲劳性和机械性。
具体实施方式
下面对本发明的优选实施例进行详细阐述，以使本发明的优点和特征能更易于被本领域技术人员理解，从而对本发明的保护范围做出更为清楚明确的界定。
实施例1
一种耐腐蚀无人机壳体材料，包括以下组份和各组分所占重量百分比为：Ti1.5％-8.5％、Ta0.5％-1.5％、Nd0.2％-0.7％、Si2％-8％、Al30％-45％、Ba1％-3％、In0.1％-0.8％，余量为Mg。
实施例2
一种耐腐蚀无人机壳体材料，包括以下组份和各组分所占重量百分比为：Ti3％-5％、Ta0.5％-0.8％、Nd0.3％-0.5％、Si4％-6％、Al35％-45％、Ba2％-3％、In0.4％-0.6％，余量为Mg。
该种耐腐蚀无人机壳体材料能够适应各种温度变化，耐高温和低温，具有较好的抗疲劳性和机械性。
虽然描述了本发明的实施方式，但是专利所有者可以在所附权利要求的范围之内做出各种变形或修改，只要不超过本发明的权利要求所描述的保护范围，都应当在本发明的保护范围之内。

Claims (1)

1.一种耐腐蚀无人机壳体材料，其特征在于：包括以下组份和各组分所占重量百分比为：Ti1.5％-8.5％、Ta0.5％-1.5％、Nd0.2％-0.7％、Si2％-8％、Al30％-45％、Ba1％-3％、In0.1％-0.8％，余量为Mg。
CN201810560401.0A 2018-06-04 2018-06-04 一种耐腐蚀无人机壳体材料 Withdrawn CN108754265A (zh)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201810560401.0A CN108754265A (zh) 2018-06-04 2018-06-04 一种耐腐蚀无人机壳体材料

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201810560401.0A CN108754265A (zh) 2018-06-04 2018-06-04 一种耐腐蚀无人机壳体材料

Publications (1)

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CN108754265A true CN108754265A (zh) 2018-11-06

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CN (1) CN108754265A (zh)

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN105441772A (zh) * 2015-12-30 2016-03-30 太仓卡斯特姆新材料有限公司 隔热复合金属材料
CN105441803A (zh) * 2015-12-30 2016-03-30 太仓卡斯特姆新材料有限公司 耐腐蚀复合金属材料
CN105525206A (zh) * 2015-12-30 2016-04-27 太仓卡斯特姆新材料有限公司 抗疲劳复合金属材料
CN106119643A (zh) * 2016-07-01 2016-11-16 无锡市华东电力设备有限公司 隔热复合金属材料

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN105441772A (zh) * 2015-12-30 2016-03-30 太仓卡斯特姆新材料有限公司 隔热复合金属材料
CN105441803A (zh) * 2015-12-30 2016-03-30 太仓卡斯特姆新材料有限公司 耐腐蚀复合金属材料
CN105525206A (zh) * 2015-12-30 2016-04-27 太仓卡斯特姆新材料有限公司 抗疲劳复合金属材料
CN106119643A (zh) * 2016-07-01 2016-11-16 无锡市华东电力设备有限公司 隔热复合金属材料

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