GB1453873A - Protective guard mounted on a turbine engine for aircraft - Google Patents
Protective guard mounted on a turbine engine for aircraftInfo
- Publication number
- GB1453873A GB1453873A GB444774A GB444774A GB1453873A GB 1453873 A GB1453873 A GB 1453873A GB 444774 A GB444774 A GB 444774A GB 444774 A GB444774 A GB 444774A GB 1453873 A GB1453873 A GB 1453873A
- Authority
- GB
- United Kingdom
- Prior art keywords
- panel
- turbine engine
- organic polymer
- inch
- impact panel
- 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.)
- Expired
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B9/00—Layered products comprising a layer of a particular substance not covered by groups B32B11/00 - B32B29/00
- B32B9/04—Layered products comprising a layer of a particular substance not covered by groups B32B11/00 - B32B29/00 comprising such particular substance as the main or only constituent of a layer, which is next to another layer of the same or of a different material
- B32B9/047—Layered products comprising a layer of a particular substance not covered by groups B32B11/00 - B32B29/00 comprising such particular substance as the main or only constituent of a layer, which is next to another layer of the same or of a different material made of fibres or filaments
-
- 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
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B5/00—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts
- B32B5/22—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by the presence of two or more layers which are next to each other and are fibrous, filamentary, formed of particles or foamed
- B32B5/24—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by the presence of two or more layers which are next to each other and are fibrous, filamentary, formed of particles or foamed one layer being a fibrous or filamentary layer
- B32B5/26—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by the presence of two or more layers which are next to each other and are fibrous, filamentary, formed of particles or foamed one layer being a fibrous or filamentary layer another layer next to it also being fibrous or filamentary
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B7/00—Layered products characterised by the relation between layers; Layered products characterised by the relative orientation of features between layers, or by the relative values of a measurable parameter between layers, i.e. products comprising layers having different physical, chemical or physicochemical properties; Layered products characterised by the interconnection of layers
- B32B7/04—Interconnection of layers
- B32B7/12—Interconnection of layers using interposed adhesives or interposed materials with bonding properties
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B9/00—Layered products comprising a layer of a particular substance not covered by groups B32B11/00 - B32B29/00
- B32B9/005—Layered products comprising a layer of a particular substance not covered by groups B32B11/00 - B32B29/00 comprising one layer of ceramic material, e.g. porcelain, ceramic tile
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B2309/00—Parameters for the laminating or treatment process; Apparatus details
- B32B2309/08—Dimensions, e.g. volume
- B32B2309/10—Dimensions, e.g. volume linear, e.g. length, distance, width
- B32B2309/105—Thickness
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B2315/00—Other materials containing non-metallic inorganic compounds not provided for in groups B32B2311/00 - B32B2313/04
- B32B2315/08—Glass
- B32B2315/085—Glass fiber cloth or fabric
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B2571/00—Protective equipment
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B2605/00—Vehicles
- B32B2605/18—Aircraft
-
- 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
- F05D2220/50—Application for auxiliary power units (APU's)
-
- 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
Landscapes
- Engineering & Computer Science (AREA)
- Ceramic Engineering (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Laminated Bodies (AREA)
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US32904673A | 1973-02-02 | 1973-02-02 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB1453873A true GB1453873A (en) | 1976-10-27 |
Family
ID=23283639
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB444774A Expired GB1453873A (en) | 1973-02-02 | 1974-01-31 | Protective guard mounted on a turbine engine for aircraft |
Country Status (5)
Country | Link |
---|---|
JP (1) | JPS5855040B2 (ja) |
DE (2) | DE2404939A1 (ja) |
FR (1) | FR2216174B1 (ja) |
GB (1) | GB1453873A (ja) |
IT (1) | IT1004855B (ja) |
Cited By (15)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2444800A1 (fr) * | 1978-12-21 | 1980-07-18 | Rolls Royce | Anneau de retenue pour moteur a turbine a gaz |
FR2502696A1 (fr) * | 1981-03-25 | 1982-10-01 | Rolls Royce | Moteur a turbine a gaz presentant une immunite accrue aux dommages causes par l'ingestion de corps etrangers |
GB2128720A (en) * | 1982-10-21 | 1984-05-02 | Michael Sacks | Protection of structural surfaces |
US4452565A (en) * | 1981-12-21 | 1984-06-05 | United Technologies Corporation | Containment structure |
US4475864A (en) * | 1981-12-21 | 1984-10-09 | United Technologies Corporation | Containment structure |
DE3529979A1 (de) * | 1985-08-22 | 1987-03-05 | Mtu Muenchen Gmbh | Einrichtung zur verhinderung der ausbreitung von titanfeuer bei turbomaschinen, insbesondere gasturbinen- bzw. gasturbinenstrahltriebwerken |
US4718818A (en) * | 1981-12-21 | 1988-01-12 | United Technologies Corporation | Containment structure |
GB2265418A (en) * | 1992-03-26 | 1993-09-29 | Rolls Royce Plc | Gas turbine engine casing blade containment. |
GB2288639A (en) * | 1994-04-20 | 1995-10-25 | Rolls Royce Plc | Blade containment in a ducted fan gas turbine engine nacelle assembly |
US5885056A (en) * | 1997-03-06 | 1999-03-23 | Rolls-Royce Plc | Gas Turbine engine casing construction |
EP0952310A3 (en) * | 1998-04-20 | 2000-07-19 | United Technologies Corporation | Penetration resistant fan casing for a turbine engine |
CN101650148B (zh) * | 2009-09-14 | 2013-03-06 | 哈尔滨飞机工业集团有限责任公司 | 一种陶瓷/复合材料夹层防护结构 |
FR3139118A1 (fr) * | 2022-08-30 | 2024-03-01 | Airbus Operations | Ensemble propulsif pour aéronef |
FR3139119A1 (fr) * | 2022-08-30 | 2024-03-01 | Airbus Operations | Ensemble propulsif pour aéronef |
EP4417521A1 (fr) * | 2023-02-14 | 2024-08-21 | Airbus Operations | Ensemble propulsif pour aéronef |
Families Citing this family (12)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2298759A1 (fr) * | 1975-01-23 | 1976-08-20 | Mtu Muenchen Gmbh | Dispositif de protection contre l'eclatement de rotors a haute vitesse |
GB1513338A (en) * | 1976-03-26 | 1978-06-07 | Rolls Royce | Rotor blade for a gas turbine engine |
FR2406074A1 (fr) * | 1977-10-11 | 1979-05-11 | Snecma | Dispositif de securite pour machine tournante axiale |
FR2467977A1 (fr) * | 1979-10-19 | 1981-04-30 | Snecma | Dispositif de securite en cas de rupture d'element rotatif de turbomachine |
GB2159886B (en) * | 1984-06-07 | 1988-01-27 | Rolls Royce | Fan duct casing |
DE3862989D1 (de) * | 1987-04-15 | 1991-07-04 | Mtu Muenchen Gmbh | Berstschutzring fuer turbotriebwerksgehaeuse. |
DE3712829A1 (de) * | 1987-04-15 | 1988-11-03 | Mtu Muenchen Gmbh | Berstschutzring fuer turbotriebwerksgehaeuse |
JPH04123275U (ja) * | 1991-04-11 | 1992-11-06 | ユニチカ株式会社 | 荷崩れ防止用織物 |
GB9605284D0 (en) * | 1996-03-13 | 1996-05-15 | Rolls Royce Plc | Gas turbine engine casing construction |
DE102006052498A1 (de) * | 2006-11-06 | 2008-05-08 | Rolls-Royce Deutschland Ltd & Co Kg | Sicherungsring für das Fangehäuse eines Gasturbinentriebwerks |
FR2914362B1 (fr) * | 2007-03-30 | 2012-07-27 | Airbus France | Dispositif de deviation et de retention de debris de moteur d'aeronef. |
JP4823180B2 (ja) * | 2007-09-12 | 2011-11-24 | 株式会社東芝 | 放射性廃棄物の造粒装置 |
Family Cites Families (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB1067506A (en) * | 1963-05-27 | 1967-05-03 | Dow Corning | Ceramic articles |
FR1605066A (en) * | 1966-09-07 | 1973-01-12 | Non metallic armour - made of interlaced polyamide fibres and glass fibre mesh all bound by a resin | |
GB1291821A (en) * | 1966-09-20 | 1972-10-04 | Aerojet General Co | Armour for providing protection against high energy particles |
FR1581760A (ja) * | 1968-07-31 | 1969-09-19 | ||
US3702593A (en) * | 1968-10-21 | 1972-11-14 | Norton Co | Removal of surface from boron carbide composite armor |
-
1974
- 1974-01-30 FR FR7403025A patent/FR2216174B1/fr not_active Expired
- 1974-01-31 GB GB444774A patent/GB1453873A/en not_active Expired
- 1974-01-31 JP JP49013247A patent/JPS5855040B2/ja not_active Expired
- 1974-02-01 DE DE2404939A patent/DE2404939A1/de active Pending
- 1974-02-01 DE DE7403536U patent/DE7403536U/de not_active Expired
- 1974-02-01 IT IT67292/74A patent/IT1004855B/it active
Cited By (20)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2444800A1 (fr) * | 1978-12-21 | 1980-07-18 | Rolls Royce | Anneau de retenue pour moteur a turbine a gaz |
FR2502696A1 (fr) * | 1981-03-25 | 1982-10-01 | Rolls Royce | Moteur a turbine a gaz presentant une immunite accrue aux dommages causes par l'ingestion de corps etrangers |
US4452565A (en) * | 1981-12-21 | 1984-06-05 | United Technologies Corporation | Containment structure |
US4475864A (en) * | 1981-12-21 | 1984-10-09 | United Technologies Corporation | Containment structure |
US4718818A (en) * | 1981-12-21 | 1988-01-12 | United Technologies Corporation | Containment structure |
GB2128720A (en) * | 1982-10-21 | 1984-05-02 | Michael Sacks | Protection of structural surfaces |
DE3529979A1 (de) * | 1985-08-22 | 1987-03-05 | Mtu Muenchen Gmbh | Einrichtung zur verhinderung der ausbreitung von titanfeuer bei turbomaschinen, insbesondere gasturbinen- bzw. gasturbinenstrahltriebwerken |
GB2265418A (en) * | 1992-03-26 | 1993-09-29 | Rolls Royce Plc | Gas turbine engine casing blade containment. |
US5273393A (en) * | 1992-03-26 | 1993-12-28 | Rolls-Royce Plc | Gas turbine engine casing |
GB2265418B (en) * | 1992-03-26 | 1995-03-08 | Rolls Royce Plc | Gas turbine engine casing |
GB2288639A (en) * | 1994-04-20 | 1995-10-25 | Rolls Royce Plc | Blade containment in a ducted fan gas turbine engine nacelle assembly |
GB2288639B (en) * | 1994-04-20 | 1998-10-21 | Rolls Royce Plc | Ducted fan gas turbine engine nacelle assembly |
US5885056A (en) * | 1997-03-06 | 1999-03-23 | Rolls-Royce Plc | Gas Turbine engine casing construction |
EP0952310A3 (en) * | 1998-04-20 | 2000-07-19 | United Technologies Corporation | Penetration resistant fan casing for a turbine engine |
CN101650148B (zh) * | 2009-09-14 | 2013-03-06 | 哈尔滨飞机工业集团有限责任公司 | 一种陶瓷/复合材料夹层防护结构 |
FR3139118A1 (fr) * | 2022-08-30 | 2024-03-01 | Airbus Operations | Ensemble propulsif pour aéronef |
FR3139119A1 (fr) * | 2022-08-30 | 2024-03-01 | Airbus Operations | Ensemble propulsif pour aéronef |
EP4331993A1 (fr) * | 2022-08-30 | 2024-03-06 | Airbus Operations | Ensemble propulsif pour aéronef |
EP4332352A1 (fr) | 2022-08-30 | 2024-03-06 | Airbus Operations | Ensemble propulsif pour aéronef |
EP4417521A1 (fr) * | 2023-02-14 | 2024-08-21 | Airbus Operations | Ensemble propulsif pour aéronef |
Also Published As
Publication number | Publication date |
---|---|
JPS5855040B2 (ja) | 1983-12-07 |
DE2404939A1 (de) | 1974-08-15 |
DE7403536U (de) | 1976-01-22 |
FR2216174B1 (ja) | 1978-09-29 |
JPS49111400A (ja) | 1974-10-23 |
FR2216174A1 (ja) | 1974-08-30 |
IT1004855B (it) | 1976-07-20 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
PS | Patent sealed [section 19, patents act 1949] | ||
PCNP | Patent ceased through non-payment of renewal fee |