公开(公告)号：US3378914A

公开(公告)日：1968-04-23

申请号：US57377466

申请日：1966-08-08

Applicant: GEN ELECTRIC

Inventor： JOHN MILLER CLARENCE

IPC: B23K1/19 ,  B23K35/28 ,  B23K35/38

CPC classification number: B23K35/38 ,  B23K1/19 ,  B23K35/284 ,  B23K35/286 ,  B23K2201/02 ,  B23K2201/14 ,  Y10S428/938 ,  Y10S428/939 ,  Y10T428/12764

Abstract: Members of Al or Al alloy are brazed together by providing at the juncture a brazing material having a melting point between 550 DEG C. and the melting point of the member having the lowest melting point and comprising at most 15% Si, at least 0.4% Mg, o-25% Cu, the balance Al, producing a non-oxidizing atmosphere at the juncture and heating to the brazing temperature. Some or all of the components of the brazing material may be included in the members to be joined and additional components may be as sheet, powder or wire.

公开(公告)号：US3350078A

公开(公告)日：1967-10-31

申请号：US57941266

申请日：1966-09-14

Applicant: NORTH AMERICAN AVIATION INC

Inventor： SHULTZ ALVY P ,  O'NEILL MICHAEL S ,  KERNS WILSON D

IPC: B23K1/00

CPC classification number: B23K1/0014 ,  B23K3/087 ,  B23K2201/02

公开(公告)号：US3106015A

公开(公告)日：1963-10-08

申请号：US10234461

申请日：1961-03-13

Applicant: ROHR CORP

Inventor： HERBERT JR THOMAS A

IPC: B21D47/00 ,  B23K1/00

CPC classification number: B21D47/00 ,  B23K1/0014 ,  B23K2201/02 ,  Y10T29/49879

公开(公告)号：US3093104A

公开(公告)日：1963-06-11

申请号：US74512958

申请日：1958-06-27

Applicant: STEPHEN BUKATA

Inventor： STEPHEN BUKATA

IPC: B23K1/00 ,  B23K1/008 ,  C21D1/74 ,  F27B5/04

CPC classification number: C21D1/74 ,  B23K1/0014 ,  B23K1/008 ,  B23K2201/02 ,  F27B5/04 ,  Y10T29/49879

公开(公告)号：US3033973A

公开(公告)日：1962-05-08

申请号：US8209761

申请日：1961-01-11

Applicant: ROHR AIRCRAFT CORP

Inventor： HERBERT JR THOMAS A

IPC: B23K1/00

CPC classification number: B23K1/0014 ,  B23K2201/02 ,  Y10T29/49879

公开(公告)号：US5635306A

公开(公告)日：1997-06-03

申请号：US485884

申请日：1995-06-07

Applicant: Katsuhiro Minamida ,  Masashi Oikawa ,  Atsushi Sugihashi ,  Akira Ishibashi ,  Mamoru Takeda

Inventor： Katsuhiro Minamida ,  Masashi Oikawa ,  Atsushi Sugihashi ,  Akira Ishibashi ,  Mamoru Takeda

IPC: B21D47/00 ,  B23K26/20 ,  B32B3/12 ,  E04C2/34 ,  B32B3/02 ,  B32B3/28 ,  B23K26/00

CPC classification number: E04C2/3405 ,  B21D47/00 ,  B23K26/22 ,  B23K26/242 ,  B23K26/244 ,  B23K26/26 ,  B32B3/12 ,  B23K2201/02 ,  E04C2002/3455 ,  E04C2002/3494 ,  Y10T29/49629 ,  Y10T428/1234

Abstract: The present invention is a honeycomb panel comprising metal face sheets respectively disposed on upper and lower faces of said honeycomb core characterized in that said honeycomb panel has a metal side plate disposed on at least one side face thereof, for mutually connecting honeycomb panels to each other, and a process for producing a honeycomb panel, said process characterized by comprising the steps of: welding a corrugated honeycomb core at an end face of its corrugation to a side plate along the end face of said corrugation; welding the honeycomb core at top portions of its corrugation to an upper face sheet from the side of the honeycomb core by means of an energy beam; welding bottom portions of the corrugation of the honeycomb core to a lower face sheet from the side of the face sheet by means of an energy beam; and welding the face sheets to the side plate before or after welding the honeycomb core to the face sheets.

Abstract translation: 本发明是一种蜂窝板，其包括分别设置在所述蜂窝芯的上表面和下表面上的金属面板，其特征在于，所述蜂窝板具有设置在其至少一个侧面上的金属侧板，用于将蜂窝板彼此相互连接 以及蜂窝板的制造方法，其特征在于，包括以下步骤：沿着所述波纹的端面将波纹状蜂窝芯在其波纹端面焊接到侧板上; 通过能量束从蜂窝芯的侧面将蜂窝状芯在其波纹的顶部处焊接到上表面片; 通过能量束将蜂窝芯的波纹的底部部分从面板的侧面焊接到下表面片; 并且在将蜂窝芯焊接到面板之前或之后将面板焊接到侧板。

公开(公告)号：US5609288A

公开(公告)日：1997-03-11

申请号：US476671

申请日：1995-06-06

Applicant: Jeffrey D. Johnson

Inventor： Jeffrey D. Johnson

IPC: B21D47/00 ,  B23K26/00 ,  B23K26/08 ,  B23K26/20 ,  B23K101/02

CPC classification number: B21D47/00 ,  B23K26/08 ,  B23K26/0869 ,  B23K26/244 ,  B23K26/26 ,  B23K2201/02 ,  B23K2203/05 ,  B23K2203/166 ,  Y10T428/1234 ,  Y10T428/12347 ,  Y10T428/1241

Abstract: "A method for fabricating a sheet assemblage ultimately extensible into a honeycomb core structure, including the steps of locating upper and lower metallic foil sheets with their confronting surfaces in uniform continuous engagement with each other and forming successive, staggered laser welded patterns as successive sheets are added to the assemblage."

Abstract translation: “一种用于制造最终可延伸到蜂窝芯结构中的片组合件的方法，包括以下步骤：将上金属箔片和下金属箔片的相对表面彼此均匀地连续地定位并形成连续的交错的激光焊接图案作为连续的片材 添加到组合中。

公开(公告)号：US5501391A

公开(公告)日：1996-03-26

申请号：US393856

申请日：1995-02-24

Applicant: Ludwig Wieres

Inventor： Ludwig Wieres

IPC: B05D1/28 ,  B23K1/00 ,  B23K1/20 ,  B23K3/00 ,  B23K3/06 ,  B23K10/02 ,  B23K35/30 ,  B23K101/02 ,  C09J129/00 ,  C09J129/10 ,  F01N3/28 ,  B23K31/02

CPC classification number: F01N3/2842 ,  B23K1/0014 ,  B23K1/20 ,  B23K10/02 ,  B23K2201/02 ,  F01N2450/02 ,  F01N2450/22

Abstract: A method for applying brazing material to a metal structure includes applying a sticky material maintaining adhesiveness up to temperatures of at least 180.degree. C. and preferably above 200.degree. C., to at least a subregion of the structure. Then brazing powder is applied which continues to adhere to the sticky material. After the application of the brazing powder but before an actual brazing process, the structure is heat treated without the brazing powder falling out during the heat treatment or during ensuing handling steps. The heat treatment may be a heat-degreasing of the structural parts that do not have or do not yet have brazing material applied to them.

Abstract translation: 将钎焊材料施加到金属结构的方法包括将至少180℃，优选高于200℃的粘合性的粘性材料施加到结构的至少一个次级区域。 然后施加持续粘附到粘性材料上的钎焊粉末。 在施加钎焊粉末之后但在实际的钎焊过程之前，该结构被热处理，而在热处理期间或在随后的处理步骤期间钎焊粉末不会脱落。 热处理可以是不具有或还没有施加钎焊材料的结构部件的热脱脂。

公开(公告)号：US5380153A

公开(公告)日：1995-01-10

申请号：US063039

申请日：1993-05-18

Applicant: James R. Campbell

Inventor： James R. Campbell

IPC: B23K1/00 ,  B23K1/20 ,  C23C4/18 ,  F04D29/08

CPC classification number: B23K1/0014 ,  B23K1/20 ,  C23C4/18 ,  B23K2201/02

Abstract: A honeycomb seal construction which includes said seal and a mounting ring therefor, said seal having honeycomb cells and being in a press-fit relationship with said mounting ring, there being a brazed joint between the seal and said ring defined by brazing material deposited in said cells at the OD of said seal.

Abstract translation: 一种蜂窝密封结构，其包括所述密封件及其安装环，所述密封件具有蜂窝单元并且与所述安装环压配关系，所述密封件和所述环之间的钎焊接头由沉积在所述密封件中的钎焊材料限定 细胞在所述密封的OD处。

公开(公告)号：US4850093A

公开(公告)日：1989-07-25

申请号：US186676

申请日：1988-04-21

Applicant: Charles A. Parente

Inventor： Charles A. Parente

IPC: B21D47/00 ,  B23K26/38 ,  E04C2/36 ,  G10K11/172

CPC classification number: E04C2/365 ,  B21D47/00 ,  B23K26/382 ,  B23K26/40 ,  G10K11/172 ,  B23K2201/02 ,  B23K2203/08 ,  B23K2203/10 ,  B23K2203/14 ,  B23K2203/16 ,  B23K2203/18 ,  B23K2203/40 ,  B23K2203/50 ,  B64D2033/0206 ,  Y10T29/49826 ,  Y10T29/49996

Abstract: A titanium face plate is perforated by laser drilling holes therethrough. A cellular core is positioned between a sound reflecting solid back plate and the face plate.

Abstract translation: 钛面板穿过激光钻孔。 蜂窝芯位于声音反射固体背板和面板之间。