GB1453873A - Protective guard mounted on a turbine engine for aircraft - Google Patents

Protective guard mounted on a turbine engine for aircraft

Info

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
Application number
GB444774A
Other languages
English (en)
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.)
Saint Gobain Abrasives Inc
Original Assignee
Norton Co
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 Norton Co filed Critical Norton Co
Publication of GB1453873A publication Critical patent/GB1453873A/en
Expired legal-status Critical Current

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)
GB444774A 1973-02-02 1974-01-31 Protective guard mounted on a turbine engine for aircraft Expired GB1453873A (en)

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 (enrdf_load_stackoverflow)
DE (2) DE2404939A1 (enrdf_load_stackoverflow)
FR (1) FR2216174B1 (enrdf_load_stackoverflow)
GB (1) GB1453873A (enrdf_load_stackoverflow)
IT (1) IT1004855B (enrdf_load_stackoverflow)

Cited By (15)

* Cited by examiner, † Cited by third party
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
FR3145746A1 (fr) * 2023-02-14 2024-08-16 Airbus Operations Ensemble propulsif pour aéronef

Families Citing this family (12)

* Cited by examiner, † Cited by third party
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
DE3712829A1 (de) * 1987-04-15 1988-11-03 Mtu Muenchen Gmbh Berstschutzring fuer turbotriebwerksgehaeuse
DE3862989D1 (de) * 1987-04-15 1991-07-04 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)

* Cited by examiner, † Cited by third party
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 (enrdf_load_stackoverflow) * 1968-07-31 1969-09-19
US3702593A (en) * 1968-10-21 1972-11-14 Norton Co Removal of surface from boron carbide composite armor

Cited By (24)

* Cited by examiner, † Cited by third party
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
EP4332352A1 (fr) 2022-08-30 2024-03-06 Airbus Operations Ensemble propulsif pour aéronef
EP4331993A1 (fr) * 2022-08-30 2024-03-06 Airbus Operations Ensemble propulsif pour aéronef
US12291350B2 (en) 2022-08-30 2025-05-06 Airbus Operations Sas Powerplant for an aircraft
US12398677B2 (en) 2022-08-30 2025-08-26 Airbus Operations Sas Powerplant for an aircraft
FR3145746A1 (fr) * 2023-02-14 2024-08-16 Airbus Operations Ensemble propulsif pour aéronef
EP4417521A1 (fr) * 2023-02-14 2024-08-21 Airbus Operations Ensemble propulsif pour aéronef
US12338775B2 (en) 2023-02-14 2025-06-24 Airbus Operations Sas Propulsion assembly for an aircraft

Also Published As

Publication number Publication date
FR2216174A1 (enrdf_load_stackoverflow) 1974-08-30
DE2404939A1 (de) 1974-08-15
IT1004855B (it) 1976-07-20
DE7403536U (de) 1976-01-22
JPS49111400A (enrdf_load_stackoverflow) 1974-10-23
FR2216174B1 (enrdf_load_stackoverflow) 1978-09-29
JPS5855040B2 (ja) 1983-12-07

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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