IT1248610B - Schermo antiproiettile - Google Patents
Schermo antiproiettileInfo
- Publication number
- IT1248610B IT1248610B ITMI911534A ITMI911534A IT1248610B IT 1248610 B IT1248610 B IT 1248610B IT MI911534 A ITMI911534 A IT MI911534A IT MI911534 A ITMI911534 A IT MI911534A IT 1248610 B IT1248610 B IT 1248610B
- Authority
- IT
- Italy
- Prior art keywords
- fabric
- ballistic
- woven
- ballistic fabric
- braided
- Prior art date
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D21/00—Shutting-down of machines or engines, e.g. in emergency; Regulating, controlling, or safety means not otherwise provided for
- F01D21/04—Shutting-down of machines or engines, e.g. in emergency; Regulating, controlling, or safety means not otherwise provided for responsive to undesired position of rotor relative to stator or to breaking-off of a part of the rotor, e.g. indicating such position
- F01D21/045—Shutting-down of machines or engines, e.g. in emergency; Regulating, controlling, or safety means not otherwise provided for responsive to undesired position of rotor relative to stator or to breaking-off of a part of the rotor, e.g. indicating such position special arrangements in stators or in rotors dealing with breaking-off of part of rotor
-
- D—TEXTILES; PAPER
- D04—BRAIDING; LACE-MAKING; KNITTING; TRIMMINGS; NON-WOVEN FABRICS
- D04C—BRAIDING OR MANUFACTURE OF LACE, INCLUDING BOBBIN-NET OR CARBONISED LACE; BRAIDING MACHINES; BRAID; LACE
- D04C1/00—Braid or lace, e.g. pillow-lace; Processes for the manufacture thereof
- D04C1/02—Braid or lace, e.g. pillow-lace; Processes for the manufacture thereof made from particular materials
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F41—WEAPONS
- F41H—ARMOUR; ARMOURED TURRETS; ARMOURED OR ARMED VEHICLES; MEANS OF ATTACK OR DEFENCE, e.g. CAMOUFLAGE, IN GENERAL
- F41H5/00—Armour; Armour plates
- F41H5/02—Plate construction
-
- D—TEXTILES; PAPER
- D10—INDEXING SCHEME ASSOCIATED WITH SUBLASSES OF SECTION D, RELATING TO TEXTILES
- D10B—INDEXING SCHEME ASSOCIATED WITH SUBLASSES OF SECTION D, RELATING TO TEXTILES
- D10B2403/00—Details of fabric structure established in the fabric forming process
- D10B2403/02—Cross-sectional features
- D10B2403/024—Fabric incorporating additional compounds
- D10B2403/0241—Fabric incorporating additional compounds enhancing mechanical properties
- D10B2403/02411—Fabric incorporating additional compounds enhancing mechanical properties with a single array of unbent yarn, e.g. unidirectional reinforcement fabrics
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2220/00—Application
- F05D2220/30—Application in turbines
- F05D2220/32—Application in turbines in gas turbines
- F05D2220/327—Application in turbines in gas turbines to drive shrouded, high solidity propeller
-
- 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
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/60—Efficient propulsion technologies, e.g. for aircraft
-
- 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
- Y10S—TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10S428/00—Stock material or miscellaneous articles
- Y10S428/902—High modulus filament or fiber
-
- 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
- Y10S—TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10S428/00—Stock material or miscellaneous articles
- Y10S428/911—Penetration resistant layer
-
- 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
- Y10T428/24—Structurally defined web or sheet [e.g., overall dimension, etc.]
- Y10T428/24058—Structurally defined web or sheet [e.g., overall dimension, etc.] including grain, strips, or filamentary elements in respective layers or components in angular relation
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Manufacturing & Machinery (AREA)
- Textile Engineering (AREA)
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
- Laminated Bodies (AREA)
- Braiding, Manufacturing Of Bobbin-Net Or Lace, And Manufacturing Of Nets By Knotting (AREA)
Abstract
E' rivelata una perfezionata struttura di contenimento di pale comprendente uno schermo antiproiettile avente un tessuto balistico intrecciato. Il tessuto intrecciato comprende trefoli balistici disposti secondo un orientamento preferito ed è efficace per aumentare la capacità del tessuto di contenere proiettili e assorbire energia dai medesimi. Il tessuto balistico intrecciato fornisce un sostanziale miglioramento nelle prestazioni rispetto al tessuto balistico ordito convenzionale.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US53924390A | 1990-06-18 | 1990-06-18 |
Publications (3)
Publication Number | Publication Date |
---|---|
ITMI911534A0 ITMI911534A0 (it) | 1991-06-05 |
ITMI911534A1 ITMI911534A1 (it) | 1992-12-05 |
IT1248610B true IT1248610B (it) | 1995-01-19 |
Family
ID=24150401
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
ITMI911534A IT1248610B (it) | 1990-06-18 | 1991-06-05 | Schermo antiproiettile |
Country Status (9)
Country | Link |
---|---|
US (1) | US5437538A (it) |
JP (1) | JPH04231625A (it) |
CN (1) | CN1057507A (it) |
CA (1) | CA2042198A1 (it) |
DE (1) | DE4119858A1 (it) |
FR (1) | FR2663412A1 (it) |
GB (1) | GB2246818A (it) |
IT (1) | IT1248610B (it) |
SE (1) | SE9101844L (it) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5488851A (en) * | 1993-09-03 | 1996-02-06 | Redaelli Tecna Meccanica S.P.A. | Multistage wiredrawing machine provided with pull adjustment |
Families Citing this family (71)
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---|---|---|---|---|
DE4223496A1 (de) * | 1992-07-17 | 1994-01-20 | Asea Brown Boveri | Vorrichtung zum Reduzieren der kinetischen Energie von berstenden Teilen |
DE4412034C2 (de) * | 1994-04-07 | 1996-10-31 | Sommer Metallbau Stahlbau Gmbh | Schutzgitter |
US5516257A (en) * | 1994-04-28 | 1996-05-14 | United Technologies Corporation | Aircraft fan containment structure restraint |
US5431532A (en) * | 1994-05-20 | 1995-07-11 | General Electric Company | Blade containment system |
GB2303596A (en) * | 1995-07-20 | 1997-02-26 | Rolls Royce Plc | Gas turbine engine containment barrier |
GB2317622A (en) * | 1996-09-28 | 1998-04-01 | Wright M & Sons Ltd | Anti-ballistic fabric |
GB2324100A (en) * | 1997-04-07 | 1998-10-14 | Soar Engineering Ltd | Woven protective mesh |
US6053696A (en) * | 1998-05-29 | 2000-04-25 | Pratt & Whitney Canada Inc. | Impact resistant composite shell for gas turbine engine fan case |
US6612217B1 (en) | 1998-06-02 | 2003-09-02 | Sri International | Penetration resistant fabric structures and materials |
US6182531B1 (en) | 1998-06-12 | 2001-02-06 | The Boeing Company | Containment ring for flywheel failure |
US6149380A (en) * | 1999-02-04 | 2000-11-21 | Pratt & Whitney Canada Corp. | Hardwall fan case with structured bumper |
US6206631B1 (en) * | 1999-09-07 | 2001-03-27 | General Electric Company | Turbomachine fan casing with dual-wall blade containment structure |
GB9922619D0 (en) | 1999-09-25 | 1999-11-24 | Rolls Royce Plc | A gas turbine engine blade containment assembly |
US6364603B1 (en) | 1999-11-01 | 2002-04-02 | Robert P. Czachor | Fan case for turbofan engine having a fan decoupler |
US6382905B1 (en) * | 2000-04-28 | 2002-05-07 | General Electric Company | Fan casing liner support |
US6696128B2 (en) | 2002-04-17 | 2004-02-24 | Mcintee Jerome S. | Safety blanket for accident victim |
US6652222B1 (en) | 2002-09-03 | 2003-11-25 | Pratt & Whitney Canada Corp. | Fan case design with metal foam between Kevlar |
US6814541B2 (en) | 2002-10-07 | 2004-11-09 | General Electric Company | Jet aircraft fan case containment design |
US7597040B2 (en) * | 2003-07-30 | 2009-10-06 | The Boeing Company | Composite containment of high energy debris and pressure |
US7008173B2 (en) * | 2003-07-30 | 2006-03-07 | The Boeing Company | High energy containment device and turbine with same |
US7018168B2 (en) * | 2004-04-08 | 2006-03-28 | General Electric Company | Method and apparatus for fabricating gas turbine engines |
GB2416192B (en) * | 2004-07-14 | 2006-09-27 | Rolls Royce Plc | Ducted fan with containment structure |
US7246990B2 (en) * | 2004-12-23 | 2007-07-24 | General Electric Company | Composite fan containment case for turbine engines |
GB2426287B (en) | 2005-05-18 | 2007-05-30 | Rolls Royce Plc | Blade containment structure |
US7517184B2 (en) * | 2006-06-01 | 2009-04-14 | Unied Technologies Corporation | Low deflection fan case cotainment fabric |
DE102006041321A1 (de) * | 2006-09-01 | 2008-03-06 | Rolls-Royce Deutschland Ltd & Co Kg | Gehäuseabschnitt, insbesondere Fangehäuse, für ein Gasturbinentriebwerk |
US7713021B2 (en) * | 2006-12-13 | 2010-05-11 | General Electric Company | Fan containment casings and methods of manufacture |
FR2913053B1 (fr) * | 2007-02-23 | 2009-05-22 | Snecma Sa | Procede de fabrication d'un carter de turbine a gaz en materiau composite et carter ainsi obtenu |
FR2914362B1 (fr) * | 2007-03-30 | 2012-07-27 | Airbus France | Dispositif de deviation et de retention de debris de moteur d'aeronef. |
GB2466608B (en) * | 2007-10-04 | 2012-12-12 | Gkn Aerospace Services Structures Corp | Secondary blade portion containment device |
FR2925118B1 (fr) * | 2007-12-14 | 2009-12-25 | Snecma | Panneau de support d'abradable dans une turbomachine |
GB2459646B (en) * | 2008-04-28 | 2011-03-30 | Rolls Royce Plc | A fan assembly |
US9032706B2 (en) * | 2008-09-26 | 2015-05-19 | Pratt & Whitney Canada Corp. | Composite fan case with integral containment zone |
US8202041B2 (en) * | 2008-10-31 | 2012-06-19 | Pratt & Whitney Canada Corp | Fan case for turbofan engine |
DE102008062363A1 (de) | 2008-12-17 | 2010-06-24 | Rolls-Royce Deutschland Ltd & Co Kg | Fangehäuse für ein Strahltriebwerk |
US8545167B2 (en) * | 2009-08-26 | 2013-10-01 | Pratt & Whitney Canada Corp. | Composite casing for rotating blades |
US20110138769A1 (en) * | 2009-12-11 | 2011-06-16 | United Technologies Corporation | Fan containment case |
US8827629B2 (en) * | 2011-02-10 | 2014-09-09 | United Technologies Corporation | Case with ballistic liner |
US8500390B2 (en) | 2010-05-20 | 2013-08-06 | Pratt & Whitney Canada Corp. | Fan case with rub elements |
US8858156B2 (en) | 2010-08-12 | 2014-10-14 | General Electric Company | Fragment containment assembly and method for adding a fragment containment assembly to a turbine |
GB201103682D0 (en) * | 2011-03-04 | 2011-04-20 | Rolls Royce Plc | A turbomachine casing assembly |
US8443706B2 (en) * | 2011-09-07 | 2013-05-21 | E I Du Pont De Nemours And Company | Triaxial braid fabric architectures for improved soft body armor ballistic impact performance |
CN103089345B (zh) * | 2011-10-31 | 2015-09-09 | 中航商用航空发动机有限责任公司 | 一种用于转动组件的包容装置 |
JP6060481B2 (ja) * | 2011-12-16 | 2017-01-18 | 株式会社Ihi | ファンケース及びその製造方法 |
US9840936B2 (en) * | 2012-02-16 | 2017-12-12 | United Technologies Corporation | Case with ballistic liner |
US20140064938A1 (en) * | 2012-09-06 | 2014-03-06 | General Electric Company | Rub tolerant fan case |
US10287918B2 (en) * | 2013-02-19 | 2019-05-14 | United Technologies Corporation | Composite attachment structure with 3D weave |
US20150345320A1 (en) * | 2013-03-13 | 2015-12-03 | United Technologies Corporation | Fan case with auxetic liner |
DE102013214389A1 (de) * | 2013-07-23 | 2015-01-29 | MTU Aero Engines AG | Gehäusecontainment |
JP2017503950A (ja) * | 2013-12-17 | 2017-02-02 | ゼネラル・エレクトリック・カンパニイ | 複合材ファン入口ブレード格納構造物 |
EP3084178B1 (en) * | 2013-12-20 | 2018-03-28 | United Technologies Corporation | Layered ice liner |
US9714583B2 (en) * | 2014-08-21 | 2017-07-25 | Honeywell International Inc. | Fan containment cases for fan casings in gas turbine engines, fan blade containment systems, and methods for producing the same |
FR3031469B1 (fr) * | 2015-01-14 | 2017-09-22 | Snecma | Carter en materiau composite a matrice organique auto-raidi |
CA2925588A1 (en) | 2015-04-29 | 2016-10-29 | Rolls-Royce Corporation | Brazed blade track for a gas turbine engine |
FR3045448B1 (fr) * | 2015-12-22 | 2018-01-26 | Safran Aircraft Engines | Carter allege en materiau composite et son procede de fabrication |
EP3225843B1 (en) * | 2016-03-30 | 2019-05-08 | Damen Dredging Equipment B.V. | A slurry pump |
US10927703B2 (en) * | 2016-09-16 | 2021-02-23 | General Electric Company | Circumferentially varying thickness composite fan casing |
US10472985B2 (en) * | 2016-12-12 | 2019-11-12 | Honeywell International Inc. | Engine case for fan blade out retention |
US10487684B2 (en) | 2017-03-31 | 2019-11-26 | The Boeing Company | Gas turbine engine fan blade containment systems |
US10550718B2 (en) | 2017-03-31 | 2020-02-04 | The Boeing Company | Gas turbine engine fan blade containment systems |
US10662813B2 (en) | 2017-04-13 | 2020-05-26 | General Electric Company | Turbine engine and containment assembly for use in a turbine engine |
US10677261B2 (en) | 2017-04-13 | 2020-06-09 | General Electric Company | Turbine engine and containment assembly for use in a turbine engine |
US11215069B2 (en) * | 2017-05-16 | 2022-01-04 | General Electric Company | Softwall containment systems |
PL421648A1 (pl) | 2017-05-19 | 2018-12-03 | General Electric Company | Usuwanie owinięcia z kevlaru z obudowy wentylatora |
US20190093512A1 (en) * | 2017-09-01 | 2019-03-28 | Rolls-Royce Corporation | Ceramic matrix composite blade track for a gas turbine engine |
US10711635B2 (en) * | 2017-11-07 | 2020-07-14 | General Electric Company | Fan casing with annular shell |
US11391297B2 (en) | 2017-11-09 | 2022-07-19 | Pratt & Whitney Canada Corp. | Composite fan case with nanoparticles |
FR3074088B1 (fr) * | 2017-11-30 | 2021-02-12 | Safran Aircraft Engines | Carter en materiau composite renforce et son procede de fabrication |
US20200011203A1 (en) * | 2018-07-06 | 2020-01-09 | General Electric Company | Blade containment structure |
CN112412878B (zh) * | 2020-09-30 | 2022-04-12 | 航天材料及工艺研究所 | 一种捕获型抗弹道冲击复合材料风扇机匣及其制造方法 |
US11549391B2 (en) * | 2021-03-22 | 2023-01-10 | General Electric Company | Component formed from hybrid material |
Family Cites Families (20)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2899987A (en) * | 1955-05-19 | 1959-08-18 | Certificate of correction | |
GB868197A (en) * | 1956-09-28 | 1961-05-17 | Rolls Royce | Improvements in or relating to protective arrangements for use with rotating parts |
GB995228A (en) * | 1964-05-08 | 1965-06-16 | Rolls Royce | Bladed structure, for example, for a gas turbine engine compressor |
US3446251A (en) * | 1968-04-23 | 1969-05-27 | Gen Electric | Triaxial fabric |
US4071647A (en) * | 1973-05-08 | 1978-01-31 | The Goodyear Tire & Rubber Company | Rubber goods |
US3874422A (en) * | 1974-03-13 | 1975-04-01 | Doweave Inc | Triaxially woven fabrics of uniform compliancy and porosity |
US3974313A (en) * | 1974-08-22 | 1976-08-10 | The Boeing Company | Projectile energy absorbing protective barrier |
GB1595358A (en) * | 1977-05-17 | 1981-08-12 | Commw Scient Ind Res Org | Impact-resisting composites |
GB2093125B (en) * | 1981-02-14 | 1984-04-18 | Rolls Royce | Gas turbine engine casing |
US4452563A (en) * | 1981-12-21 | 1984-06-05 | United Technologies Corporation | Containment structure |
US4457985A (en) * | 1982-03-19 | 1984-07-03 | Allied Corporation | Ballistic-resistant article |
US4534698A (en) * | 1983-04-25 | 1985-08-13 | General Electric Company | Blade containment structure |
US4438173A (en) * | 1983-07-21 | 1984-03-20 | Barber-Colman Company | Triaxial fabric |
US4547122A (en) * | 1983-10-14 | 1985-10-15 | Aeronautical Research Associates Of Princeton, Inc. | Method of containing fractured turbine blade fragments |
GB2159886B (en) * | 1984-06-07 | 1988-01-27 | Rolls Royce | Fan duct casing |
DE8425173U1 (de) * | 1984-08-25 | 1985-12-19 | Akzo Gmbh, 5600 Wuppertal | Schutzweste od. dgl. gegen ballistische Einwirkungen |
US4621980A (en) * | 1984-09-19 | 1986-11-11 | United Technologies Corporation | Fiber reinforced composite spar for a rotary wing aircraft |
EP0265550A1 (de) * | 1986-10-31 | 1988-05-04 | Erna Roth | Mehrschichtiges schusssicheres Gebilde |
DE3814954A1 (de) * | 1988-05-03 | 1989-11-16 | Mtu Muenchen Gmbh | Berstschutzring fuer ein triebwerksgehaeuse |
DE3830232A1 (de) * | 1988-09-06 | 1990-03-15 | Mtu Muenchen Gmbh | Berstschutzring aus faserwerkstoff |
-
1991
- 1991-05-09 CA CA002042198A patent/CA2042198A1/en not_active Abandoned
- 1991-06-05 IT ITMI911534A patent/IT1248610B/it active IP Right Grant
- 1991-06-12 FR FR9107146A patent/FR2663412A1/fr not_active Withdrawn
- 1991-06-12 JP JP3166165A patent/JPH04231625A/ja active Pending
- 1991-06-14 SE SE9101844A patent/SE9101844L/xx not_active Application Discontinuation
- 1991-06-14 CN CN91104111A patent/CN1057507A/zh active Pending
- 1991-06-17 GB GB9113060A patent/GB2246818A/en not_active Withdrawn
- 1991-06-17 DE DE4119858A patent/DE4119858A1/de not_active Withdrawn
-
1993
- 1993-10-28 US US08/144,098 patent/US5437538A/en not_active Expired - Lifetime
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5488851A (en) * | 1993-09-03 | 1996-02-06 | Redaelli Tecna Meccanica S.P.A. | Multistage wiredrawing machine provided with pull adjustment |
Also Published As
Publication number | Publication date |
---|---|
GB2246818A (en) | 1992-02-12 |
ITMI911534A1 (it) | 1992-12-05 |
JPH04231625A (ja) | 1992-08-20 |
US5437538A (en) | 1995-08-01 |
GB9113060D0 (en) | 1991-08-07 |
DE4119858A1 (de) | 1991-12-19 |
CN1057507A (zh) | 1992-01-01 |
SE9101844D0 (sv) | 1991-06-14 |
ITMI911534A0 (it) | 1991-06-05 |
CA2042198A1 (en) | 1991-12-19 |
SE9101844L (sv) | 1991-12-19 |
FR2663412A1 (fr) | 1991-12-20 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
0001 | Granted |