IT7926791A0 - Metodo di fabbricazione di un laminato poroso di lamiere. - Google Patents
Metodo di fabbricazione di un laminato poroso di lamiere.Info
- Publication number
- IT7926791A0 IT7926791A0 IT7926791A IT2679179A IT7926791A0 IT 7926791 A0 IT7926791 A0 IT 7926791A0 IT 7926791 A IT7926791 A IT 7926791A IT 2679179 A IT2679179 A IT 2679179A IT 7926791 A0 IT7926791 A0 IT 7926791A0
- Authority
- IT
- Italy
- Prior art keywords
- manufacture
- sheet metal
- porous sheet
- metal laminate
- laminate
- Prior art date
Links
- 238000004519 manufacturing process Methods 0.000 title 1
- 239000002184 metal Substances 0.000 title 1
- 238000000034 method Methods 0.000 title 1
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
- F23R3/00—Continuous combustion chambers using liquid or gaseous fuel
- F23R3/002—Wall structures
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/12—All metal or with adjacent metals
- Y10T428/1234—Honeycomb, or with grain orientation or elongated elements in defined angular relationship in respective components [e.g., parallel, inter- secting, etc.]
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/12—All metal or with adjacent metals
- Y10T428/12361—All metal or with adjacent metals having aperture or cut
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Laminated Bodies (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB7842364 | 1978-10-28 |
Publications (2)
Publication Number | Publication Date |
---|---|
IT7926791A0 true IT7926791A0 (it) | 1979-10-25 |
IT1124649B IT1124649B (it) | 1986-05-07 |
Family
ID=10500671
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
IT26791/79A IT1124649B (it) | 1978-10-28 | 1979-10-25 | Metodo di fabbricazione di un laminato poroso di lamiere |
Country Status (6)
Country | Link |
---|---|
US (1) | US4292376A (it) |
JP (1) | JPS5834210B2 (it) |
DE (1) | DE2942815C2 (it) |
FR (1) | FR2439669A1 (it) |
GB (1) | GB2033071B (it) |
IT (1) | IT1124649B (it) |
Families Citing this family (24)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2192705B (en) * | 1986-07-18 | 1990-06-06 | Rolls Royce Plc | Porous sheet structure for a combustion chamber |
JP2596921B2 (ja) * | 1986-11-28 | 1997-04-02 | 三菱重工業株式会社 | 燃焼器 |
US4773593A (en) * | 1987-05-04 | 1988-09-27 | United Technologies Corporation | Coolable thin metal sheet |
GB2214842A (en) * | 1988-02-11 | 1989-09-13 | Tui Margaret Lawrence | Pre-formed sheet material for small scale manufacture |
GB2227965B (en) * | 1988-10-12 | 1993-02-10 | Rolls Royce Plc | Apparatus for drilling a shaped hole in a workpiece |
US5113648A (en) * | 1990-02-28 | 1992-05-19 | Sundstrand Corporation | Combustor carbon screen |
US5401583A (en) * | 1991-08-02 | 1995-03-28 | Rockwell International Corporation | Gas manifolding for super plastic forming and diffusion bonding of truss core sandwiches |
US5687572A (en) * | 1992-11-02 | 1997-11-18 | Alliedsignal Inc. | Thin wall combustor with backside impingement cooling |
DE4335413A1 (de) * | 1993-10-18 | 1995-04-20 | Abb Management Ag | Verfahren und Vorrichtung zur Kühlung einer Gasturbinenbrennkammer |
US6280140B1 (en) | 1999-11-18 | 2001-08-28 | United Technologies Corporation | Method and apparatus for cooling an airfoil |
GB2356924A (en) | 1999-12-01 | 2001-06-06 | Abb Alstom Power Uk Ltd | Cooling wall structure for combustor |
GB0216362D0 (en) * | 2002-07-13 | 2002-08-21 | Rolls Royce Plc | Stress defender holes |
EP1533113A1 (de) * | 2003-11-14 | 2005-05-25 | Siemens Aktiengesellschaft | Hochtemperatur-Schichtsystem zur Wärmeableitung und Verfahren zu dessen Herstellung |
US7581385B2 (en) * | 2005-11-03 | 2009-09-01 | United Technologies Corporation | Metering sheet and iso-grid arrangement for a non axi-symmetric shaped cooling liner within a gas turbine engine exhaust duct |
US8894363B2 (en) | 2011-02-09 | 2014-11-25 | Siemens Energy, Inc. | Cooling module design and method for cooling components of a gas turbine system |
US9334741B2 (en) * | 2010-04-22 | 2016-05-10 | Siemens Energy, Inc. | Discreetly defined porous wall structure for transpirational cooling |
US9157328B2 (en) | 2010-12-24 | 2015-10-13 | Rolls-Royce North American Technologies, Inc. | Cooled gas turbine engine component |
US10018052B2 (en) | 2012-12-28 | 2018-07-10 | United Technologies Corporation | Gas turbine engine component having engineered vascular structure |
US10036258B2 (en) | 2012-12-28 | 2018-07-31 | United Technologies Corporation | Gas turbine engine component having vascular engineered lattice structure |
EP2977679B1 (en) * | 2014-07-22 | 2019-08-28 | United Technologies Corporation | Combustor wall for a gas turbine engine and method of acoustic dampening |
GB201501817D0 (en) | 2015-02-04 | 2015-03-18 | Rolls Royce Plc | A combustion chamber and a combustion chamber segment |
US10094287B2 (en) | 2015-02-10 | 2018-10-09 | United Technologies Corporation | Gas turbine engine component with vascular cooling scheme |
US10221694B2 (en) | 2016-02-17 | 2019-03-05 | United Technologies Corporation | Gas turbine engine component having vascular engineered lattice structure |
US10774653B2 (en) | 2018-12-11 | 2020-09-15 | Raytheon Technologies Corporation | Composite gas turbine engine component with lattice structure |
Family Cites Families (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2785878A (en) * | 1953-09-16 | 1957-03-19 | Earl W Conrad | Porous walled conduit for fluid cooling |
US3584972A (en) * | 1966-02-09 | 1971-06-15 | Gen Motors Corp | Laminated porous metal |
US3672787A (en) * | 1969-10-31 | 1972-06-27 | Avco Corp | Turbine blade having a cooled laminated skin |
US3864199A (en) * | 1973-07-26 | 1975-02-04 | Gen Motors Corp | Angular discharge porous sheet |
GB1530594A (en) * | 1974-12-13 | 1978-11-01 | Rolls Royce | Perforate laminated material |
US4004056A (en) * | 1975-07-24 | 1977-01-18 | General Motors Corporation | Porous laminated sheet |
CA1070128A (en) * | 1976-04-22 | 1980-01-22 | Samuel S. Osborn | Gas turbine combustion chamber |
GB2061843B (en) * | 1978-12-06 | 1982-10-20 | Lucas Industries Ltd | Apparatus for generating servo pressure signals for aircraft feel simulation |
-
1979
- 1979-09-24 GB GB7933024A patent/GB2033071B/en not_active Expired
- 1979-10-12 US US06/084,128 patent/US4292376A/en not_active Expired - Lifetime
- 1979-10-23 DE DE2942815A patent/DE2942815C2/de not_active Expired
- 1979-10-25 FR FR7926528A patent/FR2439669A1/fr active Granted
- 1979-10-25 IT IT26791/79A patent/IT1124649B/it active
- 1979-10-26 JP JP54138613A patent/JPS5834210B2/ja not_active Expired
Also Published As
Publication number | Publication date |
---|---|
DE2942815C2 (de) | 1982-11-18 |
IT1124649B (it) | 1986-05-07 |
JPS5834210B2 (ja) | 1983-07-25 |
GB2033071B (en) | 1982-07-21 |
GB2033071A (en) | 1980-05-14 |
FR2439669B1 (it) | 1983-07-18 |
JPS5561342A (en) | 1980-05-09 |
US4292376A (en) | 1981-09-29 |
DE2942815A1 (de) | 1980-05-08 |
FR2439669A1 (fr) | 1980-05-23 |
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