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公开(公告)号：US20110256414A1
公开(公告)日：2011-10-20
申请号：US13152371
申请日：2011-06-03
Applicant: Peter Knepper , Klaus J. Eisenmenger
Inventor： Peter Knepper , Klaus J. Eisenmenger
IPC: B32B15/04
CPC classification number: C23C4/02 , C23C4/04 , C23C4/08 , C23C4/12 , C23C4/129 , Y10T428/249921 , Y10T428/31678
Abstract: In a method for coating a fibre composite component for an aircraft or spacecraft, a surface layer of the fibre composite component, which surface layer has spacing from the fibres introduced in the fibre composite component for the protection thereof, is pretreated, at least in portions to form a primer coat; at least one functional coat is then applied to the formed primer coat. A corresponding fibre composite component comprises at least one functional coat which is applied to a primer coat.
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2.发明申请METHOD FOR COATING A FIBER COMPOSITE COMPONENT FOR AN AIRCRAFT OR SPACECRAFT AND FIBER COMPOSITE COMPONENT PRODUCED BY SAID METHOD 审中-公开用于涂覆用于由方法生产的飞行器或空格和纤维复合组分的纤维复合组分的方法公开(公告)号：US20110091709A1
公开(公告)日：2011-04-21
申请号：US12910270
申请日：2010-10-22
Applicant: Peter Knepper , Klaus J. Eisenmenger
Inventor： Peter Knepper , Klaus J. Eisenmenger
CPC classification number: C23C4/02 , C23C4/04 , C23C4/08 , C23C4/12 , C23C4/129 , Y10T428/249921 , Y10T428/31678
Abstract: In a method for coating a fibre composite component for an aircraft or spacecraft, a surface layer of the fibre composite component, which surface layer has spacing from the fibres introduced in the fibre composite component for the protection thereof, is pretreated, at least in portions to form a primer coat; at least one functional coat is then applied to the formed primer coat. A corresponding fibre composite component comprises at least one functional coat which is applied to a primer coat.
Abstract translation: 在用于飞行器或航天器的纤维复合材料部件的涂覆方法中，将纤维复合材料部件的表面层与纤维复合材料部件中引入的纤维间隔开来进行保护的表层，至少部分地进行预处理 形成底漆; 然后将至少一种功能性涂层施加到所形成的底涂层。 相应的纤维复合材料组分包含至少一种施加于底漆的功能性涂层。
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Patent Agency Ranking
公开(公告)号：US20100038409A1
公开(公告)日：2010-02-18
申请号：US12112870
申请日：2008-04-30
Applicant: Johannes WILDEN , Jean Pierre BERGMANN , Simon JAHN , Tamara Vugrin , Peter Knepper
Inventor： Johannes WILDEN , Jean Pierre BERGMANN , Simon JAHN , Tamara Vugrin , Peter Knepper
IPC: B23K31/02
CPC classification number: B23K1/0006
Abstract: A method is provided for connecting components particularly in the field of aerospace wherein a first component is connected to a second component, comprising the following steps: arranging at least one nano- or microstructured material between the first and the second component, initiating an exothermic reaction of the nano- or microstructured material for connecting both components with each other.
Abstract translation: 提供一种用于连接部件的方法，特别是在航空航天领域，其中第一部件连接到第二部件，其包括以下步骤：在第一和第二部件之间布置至少一种纳米或微结构材料，引发放热反应 用于将两个部件彼此连接的纳米或微结构材料。
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公开(公告)号：US09764351B2
公开(公告)日：2017-09-19
申请号：US11906278
申请日：2007-10-01
Applicant: Rainer Kocik , Peter Knepper , Thomas Warda
Inventor： Rainer Kocik , Peter Knepper , Thomas Warda
Abstract: A method is provided for coating a substrate, in particular a fiber reinforced plastic component, a protective layer being applied, with preference by means of thermal spraying, to a non-cured resin film applied to a release film, and subsequently, after removal of the release film, the resin film being applied to the substrate and cured.
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公开(公告)号：US5618357A
公开(公告)日：1997-04-08
申请号：US493672
申请日：1995-06-22
Applicant: Peter Knepper , Olaf Scheffler
Inventor： Peter Knepper , Olaf Scheffler
CPC classification number: B23K35/286
Abstract: A solder material that is especially suitable for the fluxless hard soldering of aluminum-based components consists of an aluminum-based alloy that especially contains about 10 to 50 wt. % of germanium, about 1 to 12 wt. % of silicon, about 0.1 to 3 wt. % of magnesium, and about 0.1 to 3 wt. % of indium. The solder material is useful at soldering temperatures in the range from 424.degree. to about 600.degree. C., and is therefore especially suitable for the fluxless hard soldering of components made of precipitation-hardened high-strength aluminum-based materials.
Abstract translation: 特别适用于铝基部件的无助焊硬焊接的焊料材料由铝基合金组成，其特别地包含约10至50wt。 约1〜12wt。 硅的百分比，约0.1至3wt。 ％的镁和约0.1至3wt。 ％的铟。 焊料材料在424〜600℃的焊接温度下是有用的，因此特别适用于由沉淀硬化的高强度铝基材料制成的部件的无焊剂硬焊接。
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公开(公告)号：US07975902B2
公开(公告)日：2011-07-12
申请号：US12112870
申请日：2008-04-30
Applicant: Johannes Wilden , Jean Pierre Bergmann , Simon Jahn , Tamara Vugrin , Peter Knepper
Inventor： Johannes Wilden , Jean Pierre Bergmann , Simon Jahn , Tamara Vugrin , Peter Knepper
IPC: B23K31/02
CPC classification number: B23K1/0006
Abstract: A method is provided for connecting components particularly in the field of aerospace wherein a first component is connected to a second component, comprising the following steps: arranging at least one nano- or microstructured material between the first and the second component, initiating an exothermic reaction of the nano- or microstructured material for connecting both components with each other.
Abstract translation: 提供一种用于连接部件的方法，特别是在航空航天领域，其中第一部件连接到第二部件，其包括以下步骤：在第一和第二部件之间布置至少一种纳米或微结构材料，引发放热反应 用于将两个部件彼此连接的纳米或微结构材料。
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公开(公告)号：US20080145555A1
公开(公告)日：2008-06-19
申请号：US11906278
申请日：2007-10-01
Applicant: Rainer Kocik , Peter Knepper , Thomas Warda
Inventor： Rainer Kocik , Peter Knepper , Thomas Warda
IPC: B05D1/08
Abstract: The present invention provides a method for coating a substrate, in particular a fiber reinforced plastic component, a protective layer being applied, with preference by means of thermal spraying, to a non-cured resin film applied to a release film, and subsequently, after removal of the release film, the resin film being applied to the substrate and cured.
Abstract translation: 本发明提供了一种通过热喷涂优选地将基材，特别是纤维增强塑料组分，保护层涂覆到施加到脱模膜的未固化树脂膜上，随后在 去除脱模膜，将树脂膜施加到基材上并固化。
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