ES2131479A1 - Util y proceso de ensamblaje para soldadura laser. - Google Patents

Util y proceso de ensamblaje para soldadura laser.

Info

Publication number
ES2131479A1
ES2131479A1 ES09702341A ES9702341A ES2131479A1 ES 2131479 A1 ES2131479 A1 ES 2131479A1 ES 09702341 A ES09702341 A ES 09702341A ES 9702341 A ES9702341 A ES 9702341A ES 2131479 A1 ES2131479 A1 ES 2131479A1
Authority
ES
Spain
Prior art keywords
laser welding
assembly tool
elements
tool
assembly
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Granted
Application number
ES09702341A
Other languages
English (en)
Other versions
ES2131479B1 (es
Inventor
Martinez Manuel Torres
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Individual
Original Assignee
Individual
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Individual filed Critical Individual
Priority to ES009702341A priority Critical patent/ES2131479B1/es
Publication of ES2131479A1 publication Critical patent/ES2131479A1/es
Application granted granted Critical
Publication of ES2131479B1 publication Critical patent/ES2131479B1/es
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23K—SOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
    • B23K26/00—Working by laser beam, e.g. welding, cutting or boring
    • B23K26/08—Devices involving relative movement between laser beam and workpiece
    • B23K26/10—Devices involving relative movement between laser beam and workpiece using a fixed support, i.e. involving moving the laser beam
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23K—SOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
    • B23K37/00—Auxiliary devices or processes, not specially adapted to a procedure covered by only one of the preceding main groups
    • B23K37/04—Auxiliary devices or processes, not specially adapted to a procedure covered by only one of the preceding main groups for holding or positioning work
    • B23K37/0426—Fixtures for other work
    • B23K37/0435—Clamps
    • B23K37/0443—Jigs
    • 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
    • B64C1/06—Frames; Stringers; Longerons ; Fuselage sections
    • 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
    • B64C1/06—Frames; Stringers; Longerons ; Fuselage sections
    • B64C1/12—Construction or attachment of skin panels

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Physics & Mathematics (AREA)
  • Optics & Photonics (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Plasma & Fusion (AREA)
  • Laser Beam Processing (AREA)

Abstract

til y proceso de ensamblaje para soldadura láser, comprendiendo el útil unos elementos (1) en forma de perfiles huecos con una ranura longitudinal abierta en el borde superior, en disposición de dichos elementos (1) según una distribución entrecruzada sobre una base sustentadora (3), mientras que en el interior dé los mismos se incluyen unos correspondientes elementos-émbolos (4), los cuales son susceptibles de asomamiento y remetido por acción neumática, determinando un conjunto flotante para la sujeción de las piezas a soldar.
ES009702341A 1997-11-10 1997-11-10 Util y proceso de ensamblaje para soldadura laser. Expired - Lifetime ES2131479B1 (es)

Priority Applications (1)

Application Number Priority Date Filing Date Title
ES009702341A ES2131479B1 (es) 1997-11-10 1997-11-10 Util y proceso de ensamblaje para soldadura laser.

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
ES009702341A ES2131479B1 (es) 1997-11-10 1997-11-10 Util y proceso de ensamblaje para soldadura laser.

Publications (2)

Publication Number Publication Date
ES2131479A1 true ES2131479A1 (es) 1999-07-16
ES2131479B1 ES2131479B1 (es) 2000-03-01

Family

ID=8301132

Family Applications (1)

Application Number Title Priority Date Filing Date
ES009702341A Expired - Lifetime ES2131479B1 (es) 1997-11-10 1997-11-10 Util y proceso de ensamblaje para soldadura laser.

Country Status (1)

Country Link
ES (1) ES2131479B1 (es)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0995673A3 (de) * 1998-09-25 2003-06-04 Airbus Deutschland GmbH Schalenbauteil für ein Flugzeug und Verfahren zur Herstellung

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN101407008B (zh) * 2008-11-21 2011-01-19 四川成飞集成科技股份有限公司 精确定位三维激光切割零件的坐标平台
CN102774491B (zh) * 2012-07-30 2016-12-07 北京智创联合科技有限公司 一种空心夹层结构及其制造方法

Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2074117A (en) * 1980-04-21 1981-10-28 Lear Fan Corp Composite structure for joining intersecting structural members of an airframe
US4310132A (en) * 1978-02-16 1982-01-12 Nasa Fuselage structure using advanced technology fiber reinforced composites
US4633632A (en) * 1983-11-17 1987-01-06 Messerschmitt-Boelkow-Blohm Gesellschaft Mit Beschraenkter Haftung Structural component having a curved wall and apparatus for making such structural component
US4921568A (en) * 1988-05-31 1990-05-01 Rockwell International Corporation Moving head high frequency resistance welding system
US5242523A (en) * 1992-05-14 1993-09-07 The Boeing Company Caul and method for bonding and curing intricate composite structures
US5518208A (en) * 1993-12-28 1996-05-21 The Boeing Company Optimum aircraft body frame to body skin shear tie installation pattern for body skin/stringer circumferential splices
ES2092869T3 (es) * 1993-05-25 1996-12-01 Snecma Procedimiento de soldadura laser de una ensambladura de dos piezas metalicas.

Patent Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4310132A (en) * 1978-02-16 1982-01-12 Nasa Fuselage structure using advanced technology fiber reinforced composites
GB2074117A (en) * 1980-04-21 1981-10-28 Lear Fan Corp Composite structure for joining intersecting structural members of an airframe
US4633632A (en) * 1983-11-17 1987-01-06 Messerschmitt-Boelkow-Blohm Gesellschaft Mit Beschraenkter Haftung Structural component having a curved wall and apparatus for making such structural component
US4921568A (en) * 1988-05-31 1990-05-01 Rockwell International Corporation Moving head high frequency resistance welding system
US5242523A (en) * 1992-05-14 1993-09-07 The Boeing Company Caul and method for bonding and curing intricate composite structures
ES2092869T3 (es) * 1993-05-25 1996-12-01 Snecma Procedimiento de soldadura laser de una ensambladura de dos piezas metalicas.
US5518208A (en) * 1993-12-28 1996-05-21 The Boeing Company Optimum aircraft body frame to body skin shear tie installation pattern for body skin/stringer circumferential splices

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0995673A3 (de) * 1998-09-25 2003-06-04 Airbus Deutschland GmbH Schalenbauteil für ein Flugzeug und Verfahren zur Herstellung

Also Published As

Publication number Publication date
ES2131479B1 (es) 2000-03-01

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