IT1004855B - BARRIER OR PROTECTIVE SCREEN FOR TURBINE ENGINES FOR AIRCRAFT - Google Patents

BARRIER OR PROTECTIVE SCREEN FOR TURBINE ENGINES FOR AIRCRAFT

Info

Publication number
IT1004855B
IT1004855B IT67292/74A IT6729274A IT1004855B IT 1004855 B IT1004855 B IT 1004855B IT 67292/74 A IT67292/74 A IT 67292/74A IT 6729274 A IT6729274 A IT 6729274A IT 1004855 B IT1004855 B IT 1004855B
Authority
IT
Italy
Prior art keywords
aircraft
barrier
turbine engines
protective screen
protective
Prior art date
Application number
IT67292/74A
Other languages
Italian (it)
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
Application granted granted Critical
Publication of IT1004855B publication Critical patent/IT1004855B/en

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)
IT67292/74A 1973-02-02 1974-02-01 BARRIER OR PROTECTIVE SCREEN FOR TURBINE ENGINES FOR AIRCRAFT IT1004855B (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
IT1004855B true IT1004855B (en) 1976-07-20

Family

ID=23283639

Family Applications (1)

Application Number Title Priority Date Filing Date
IT67292/74A IT1004855B (en) 1973-02-02 1974-02-01 BARRIER OR PROTECTIVE SCREEN FOR TURBINE ENGINES FOR AIRCRAFT

Country Status (5)

Country Link
JP (1) JPS5855040B2 (en)
DE (2) DE2404939A1 (en)
FR (1) FR2216174B1 (en)
GB (1) GB1453873A (en)
IT (1) IT1004855B (en)

Families Citing this family (26)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2298759A1 (en) * 1975-01-23 1976-08-20 Mtu Muenchen Gmbh HIGH SPEED ROTOR BURST PROTECTION DEVICE
GB1513338A (en) * 1976-03-26 1978-06-07 Rolls Royce Rotor blade for a gas turbine engine
FR2406074A1 (en) * 1977-10-11 1979-05-11 Snecma SAFETY DEVICE FOR AXIAL ROTATING MACHINE
FR2444800A1 (en) * 1978-12-21 1980-07-18 Rolls Royce Gas turbine protective ring - has reinforced polyamide fibre material layers wrapped on carrier ring
FR2467977A1 (en) * 1979-10-19 1981-04-30 Snecma SAFETY DEVICE IN THE EVENT OF TURBOMACHINE ROTATING ELEMENT BREAK
GB2095749B (en) * 1981-03-25 1984-12-12 Rolls Royce Gas turbine engine having improved resistance for foreign object ingestion damage
US4475864A (en) * 1981-12-21 1984-10-09 United Technologies Corporation Containment structure
US4452565A (en) * 1981-12-21 1984-06-05 United Technologies Corporation Containment structure
US4718818A (en) * 1981-12-21 1988-01-12 United Technologies Corporation Containment structure
GB2128720B (en) * 1982-10-21 1986-04-16 Michael Sacks Protection of structural surfaces
GB2159886B (en) * 1984-06-07 1988-01-27 Rolls Royce Fan duct casing
DE3529979A1 (en) * 1985-08-22 1987-03-05 Mtu Muenchen Gmbh Device for preventing the propagation of titanium fire in turbo engines, especially gas turbines or gas turbine jet engines
DE3712829A1 (en) * 1987-04-15 1988-11-03 Mtu Muenchen Gmbh Bursting protection ring for turbine engine housings
EP0286815B1 (en) * 1987-04-15 1991-05-29 Mtu Motoren- Und Turbinen-Union MàœNchen Gmbh Containment ring for turbo machine casings
JPH04123275U (en) * 1991-04-11 1992-11-06 ユニチカ株式会社 Fabric for preventing cargo from collapsing
GB2265418B (en) * 1992-03-26 1995-03-08 Rolls Royce Plc Gas turbine engine casing
GB2288639B (en) * 1994-04-20 1998-10-21 Rolls Royce Plc Ducted fan gas turbine engine nacelle assembly
GB9605284D0 (en) * 1996-03-13 1996-05-15 Rolls Royce Plc Gas turbine engine casing construction
US5885056A (en) * 1997-03-06 1999-03-23 Rolls-Royce Plc Gas Turbine engine casing construction
US6059524A (en) * 1998-04-20 2000-05-09 United Technologies Corporation Penetration resistant fan casing for a turbine engine
DE102006052498A1 (en) * 2006-11-06 2008-05-08 Rolls-Royce Deutschland Ltd & Co Kg Circlip for the fan housing of a gas turbine engine
FR2914362B1 (en) * 2007-03-30 2012-07-27 Airbus France DEVICE FOR DETECTING AND RETAINING DEBRIS FROM AN AIRCRAFT ENGINE.
JP4823180B2 (en) * 2007-09-12 2011-11-24 株式会社東芝 Radioactive waste granulator
CN101650148B (en) * 2009-09-14 2013-03-06 哈尔滨飞机工业集团有限责任公司 Ceramic/composite material interlayer protecting structure
FR3139119A1 (en) * 2022-08-30 2024-03-01 Airbus Operations PROPULSIVE ASSEMBLY FOR AIRCRAFT
FR3139118A1 (en) * 2022-08-30 2024-03-01 Airbus Operations PROPULSIVE ASSEMBLY FOR AIRCRAFT

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 (en) * 1968-07-31 1969-09-19
US3702593A (en) * 1968-10-21 1972-11-14 Norton Co Removal of surface from boron carbide composite armor

Also Published As

Publication number Publication date
JPS49111400A (en) 1974-10-23
DE2404939A1 (en) 1974-08-15
FR2216174A1 (en) 1974-08-30
FR2216174B1 (en) 1978-09-29
GB1453873A (en) 1976-10-27
JPS5855040B2 (en) 1983-12-07
DE7403536U (en) 1976-01-22

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