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METHOD FOR PRODUCING COMPOSITE CASE IN THE FIELD OF AVIATION AND SPACE INDUSTRY

机译:航空航天工业领域中复合壳体的生产方法

摘要

1. A method for the production of composite skin (10) for the aviation and space industry, comprising the following steps:! removing excess material (33) from the butt plate (12) to obtain a butt plate (22) at one end (20) of the said butt plate; ! the connection of the other end (19) of the butt plate (12) with the substance-substance sheathing plate (11); ! and fastening the next sheathing plate (13) with the butt plate (22) to obtain a composite sheathing (10). ! 2. The method according to claim 1, characterized in that the substance-substance bond between the other end (19) of the butt plate (12) and the sheathing plate (11) is carried out by friction stir welding, laser welding and / or electron beam welding. ! 3. The method according to claim 1, characterized in that the method of implementing the connection "substance-substance" is performed as a method of performing a butt joint (14). ! 4. The method according to claim 1, characterized in that the butt plate (22) is attached to the next plate (13) sheathing using rivets (23, 24, 25). ! 5. The method according to claim 1, characterized in that the step of removing excess material (33) includes removing excess material (32) at the other end (19) of the butt plate (12) to obtain a butt plate (12) having essentially Z- figurative cross section (15). ! 6. The method according to claim 1, characterized in that the excess material (33) and / or the following excess material (32) is removed mechanically or chemically. ! 7. Composite sheathing for the aerospace industry, comprising: a butt plate (12) that has a butt plate (22) at one end thereof (20), a sheath plate (11) that is connected to the other end (19) of this butt plate (12) a substance-to-substance bond, and the next plate (13) sheathed
机译:1.一种用于航空和航天工业的复合蒙皮(10)的生产方法,其包括以下步骤:!从对接板(12)中去除多余的材料(33),以在所述对接板的一端(20)处获得对接板(22); !对接板(12)的另一端(19)与物质覆盖板(11)的连接; !将下一个护套板(13)与对接板(22)固定在一起,得到复合护套(10)。 ! 2.根据权利要求1所述的方法,其特征在于,所述对接板(12)的另一端(19)和所述护套板(11)之间的物质-物质结合是通过搅拌摩擦焊接,激光焊接和/或进行的。或电子束焊接。 ! 3.根据权利要求1或2所述的方法,其特征在于,实现所述连接“物质-物质”的方法作为进行对接(14)的方法来进行。 ! 4.根据权利要求1至3中任一项所述的方法,其特征在于,所述对接板(22)利用铆钉(23、24、25)附接至下一个板(13)的护套。 ! 5.根据权利要求1所述的方法,其特征在于,去除多余材料(33)的步骤包括去除所述对接板(12)的另一端(19)处的多余材料(32)以获得对接板(12)。具有基本上Z形的横截面(15)。 ! 6.根据权利要求1至5中任一项所述的方法,其特征在于,所述多余的材料(33)和/或随后的多余的材料(32)被机械地或化学地去除。 ! 7.一种用于航空航天工业的复合护套,包括:对接板(12),其一端(20)具有对接板(22);护套板(11),其连接至所述护套的另一端(19)。该对接板(12)具有物质对物质的结合,而下一个板(13)带有护套

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