ES2156720A1 - Estructura metalica aplicable a carcasas externas de aeromotores. - Google Patents

Estructura metalica aplicable a carcasas externas de aeromotores.

Info

Publication number
ES2156720A1
ES2156720A1 ES009900660A ES9900660A ES2156720A1 ES 2156720 A1 ES2156720 A1 ES 2156720A1 ES 009900660 A ES009900660 A ES 009900660A ES 9900660 A ES9900660 A ES 9900660A ES 2156720 A1 ES2156720 A1 ES 2156720A1
Authority
ES
Spain
Prior art keywords
external
metal structure
casings
aeromotor
structure applicable
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
ES009900660A
Other languages
English (en)
Other versions
ES2156720B1 (es
Inventor
Garcia San Pedro Santiago Reig
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.)
MECANIZACIONES AERONAUTICAS S
Original Assignee
MECANIZACIONES AERONAUTICAS S
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 MECANIZACIONES AERONAUTICAS S filed Critical MECANIZACIONES AERONAUTICAS S
Priority to ES9900660A priority Critical patent/ES2156720B1/es
Publication of ES2156720A1 publication Critical patent/ES2156720A1/es
Application granted granted Critical
Publication of ES2156720B1 publication Critical patent/ES2156720B1/es
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

Links

Landscapes

  • Laminated Bodies (AREA)
  • Pressure Welding/Diffusion-Bonding (AREA)
  • Motor Or Generator Frames (AREA)

Abstract

Estructura metálica aplicable a carcasas externas de aeromotores constituida a partir de una estructura bicónica (3) situada entre dos chapas planas (1) y (2), en la que la estructura bicónica (3) esta fabricada por conformado superplástico de una chapa de Ti6A14V o similar, estando constituida por una pluralidad de troncos de cono cuyo vértice se sitúa en una dirección perpendicular al plano definido por las dos dimensiones mayores de la estructura y alternativamente situados en direcciones opuestas. Opcionalmente, la estructura bicónica (3) puede ser sustituida por una estructura piramidal (3'').
ES9900660A 1999-03-31 1999-03-31 Estructura metalica aplicable a carcasas externas de aeromotores. Expired - Fee Related ES2156720B1 (es)

Priority Applications (1)

Application Number Priority Date Filing Date Title
ES9900660A ES2156720B1 (es) 1999-03-31 1999-03-31 Estructura metalica aplicable a carcasas externas de aeromotores.

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
ES9900660A ES2156720B1 (es) 1999-03-31 1999-03-31 Estructura metalica aplicable a carcasas externas de aeromotores.

Publications (2)

Publication Number Publication Date
ES2156720A1 true ES2156720A1 (es) 2001-07-01
ES2156720B1 ES2156720B1 (es) 2002-01-16

Family

ID=8307867

Family Applications (1)

Application Number Title Priority Date Filing Date
ES9900660A Expired - Fee Related ES2156720B1 (es) 1999-03-31 1999-03-31 Estructura metalica aplicable a carcasas externas de aeromotores.

Country Status (1)

Country Link
ES (1) ES2156720B1 (es)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP2500118A4 (en) * 2009-11-13 2015-06-24 Sumitomo Light Metal Ind MATERIAL PLATE HAVING CONCRETE / CONVEX SECTIONS AND LAMINATE STRUCTURE AND PANEL FOR VEHICLE USING SAID PLATE OF MATERIAL
US20150233118A1 (en) * 2012-08-24 2015-08-20 Alexis Chermant Sheet for Structural Material Core, Core and Structural Material Comprising Such a Sheet

Citations (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2481046A (en) * 1947-11-13 1949-09-06 Western Engineering Associates Panel structure
US3011602A (en) * 1959-07-13 1961-12-05 Lockheed Aircraft Corp Panel construction
US3876492A (en) * 1973-05-21 1975-04-08 Lawrence A Schott Reinforced cellular panel construction
US3927817A (en) * 1974-10-03 1975-12-23 Rockwell International Corp Method for making metallic sandwich structures
US3938963A (en) * 1973-10-01 1976-02-17 Hale Jesse R Sandwich core panel having cured face sheets and a core formed with projecting modes
US4292375A (en) * 1979-05-30 1981-09-29 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Superplastically formed diffusion bonded metallic structure
US5242735A (en) * 1991-10-17 1993-09-07 Karl Blankenburg Structural module
US5486086A (en) * 1994-01-04 1996-01-23 General Electric Company Blade containment system
US5850722A (en) * 1996-09-27 1998-12-22 Mcdonnell Douglas Corporation Lightweight superplastically formed, diffusion bonded panel structure and process of manufacture

Patent Citations (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2481046A (en) * 1947-11-13 1949-09-06 Western Engineering Associates Panel structure
US3011602A (en) * 1959-07-13 1961-12-05 Lockheed Aircraft Corp Panel construction
US3876492A (en) * 1973-05-21 1975-04-08 Lawrence A Schott Reinforced cellular panel construction
US3938963A (en) * 1973-10-01 1976-02-17 Hale Jesse R Sandwich core panel having cured face sheets and a core formed with projecting modes
US3927817A (en) * 1974-10-03 1975-12-23 Rockwell International Corp Method for making metallic sandwich structures
US4292375A (en) * 1979-05-30 1981-09-29 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Superplastically formed diffusion bonded metallic structure
US5242735A (en) * 1991-10-17 1993-09-07 Karl Blankenburg Structural module
US5486086A (en) * 1994-01-04 1996-01-23 General Electric Company Blade containment system
US5850722A (en) * 1996-09-27 1998-12-22 Mcdonnell Douglas Corporation Lightweight superplastically formed, diffusion bonded panel structure and process of manufacture

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP2500118A4 (en) * 2009-11-13 2015-06-24 Sumitomo Light Metal Ind MATERIAL PLATE HAVING CONCRETE / CONVEX SECTIONS AND LAMINATE STRUCTURE AND PANEL FOR VEHICLE USING SAID PLATE OF MATERIAL
US9108239B2 (en) 2009-11-13 2015-08-18 Sumitomo Light Metal Industries, Ltd. Sheet material having concave-convex section, and laminated structure and vehicle panel using the same
US20150233118A1 (en) * 2012-08-24 2015-08-20 Alexis Chermant Sheet for Structural Material Core, Core and Structural Material Comprising Such a Sheet

Also Published As

Publication number Publication date
ES2156720B1 (es) 2002-01-16

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