EP2015935A1 - Pressure-resistant body that is supplied with fluid - Google Patents

Pressure-resistant body that is supplied with fluid

Info

Publication number
EP2015935A1
EP2015935A1 EP07728989A EP07728989A EP2015935A1 EP 2015935 A1 EP2015935 A1 EP 2015935A1 EP 07728989 A EP07728989 A EP 07728989A EP 07728989 A EP07728989 A EP 07728989A EP 2015935 A1 EP2015935 A1 EP 2015935A1
Authority
EP
European Patent Office
Prior art keywords
fibers
layer
body according
pressure
fiber
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.)
Withdrawn
Application number
EP07728989A
Other languages
German (de)
French (fr)
Inventor
Karl Maile
Karl Berreth
Abram Lyutovich
Roland Weiss
Thorsten Scheibel
Marco Ebert
Martin Henrich
Andreas Lauer
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.)
Schunk Kohlenstofftechnik GmbH
Original Assignee
Schunk Kohlenstofftechnik GmbH
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 Schunk Kohlenstofftechnik GmbH filed Critical Schunk Kohlenstofftechnik GmbH
Publication of EP2015935A1 publication Critical patent/EP2015935A1/en
Withdrawn legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16JPISTONS; CYLINDERS; SEALINGS
    • F16J12/00Pressure vessels in general
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C1/00Pressure vessels, e.g. gas cylinder, gas tank, replaceable cartridge
    • F17C1/02Pressure vessels, e.g. gas cylinder, gas tank, replaceable cartridge involving reinforcing arrangements
    • F17C1/04Protecting sheathings
    • F17C1/06Protecting sheathings built-up from wound-on bands or filamentary material, e.g. wires
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B1/00Layered products having a non-planar shape
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B15/00Layered products comprising a layer of metal
    • B32B15/04Layered products comprising a layer of metal comprising metal as the main or only constituent of a layer, which is next to another layer of the same or of a different material
    • B32B15/08Layered products comprising a layer of metal comprising metal as the main or only constituent of a layer, which is next to another layer of the same or of a different material of synthetic resin
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B15/00Layered products comprising a layer of metal
    • B32B15/14Layered products comprising a layer of metal next to a fibrous or filamentary layer
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B15/00Layered products comprising a layer of metal
    • B32B15/18Layered products comprising a layer of metal comprising iron or steel
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B18/00Layered products essentially comprising ceramics, e.g. refractory products
    • CCHEMISTRY; METALLURGY
    • C04CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
    • C04BLIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
    • C04B2235/00Aspects relating to ceramic starting mixtures or sintered ceramic products
    • C04B2235/02Composition of constituents of the starting material or of secondary phases of the final product
    • C04B2235/50Constituents or additives of the starting mixture chosen for their shape or used because of their shape or their physical appearance
    • C04B2235/52Constituents or additives characterised by their shapes
    • C04B2235/5208Fibers
    • C04B2235/5216Inorganic
    • C04B2235/522Oxidic
    • C04B2235/5224Alumina or aluminates
    • CCHEMISTRY; METALLURGY
    • C04CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
    • C04BLIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
    • C04B2235/00Aspects relating to ceramic starting mixtures or sintered ceramic products
    • C04B2235/02Composition of constituents of the starting material or of secondary phases of the final product
    • C04B2235/50Constituents or additives of the starting mixture chosen for their shape or used because of their shape or their physical appearance
    • C04B2235/52Constituents or additives characterised by their shapes
    • C04B2235/5208Fibers
    • C04B2235/5216Inorganic
    • C04B2235/522Oxidic
    • C04B2235/5228Silica and alumina, including aluminosilicates, e.g. mullite
    • CCHEMISTRY; METALLURGY
    • C04CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
    • C04BLIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
    • C04B2235/00Aspects relating to ceramic starting mixtures or sintered ceramic products
    • C04B2235/02Composition of constituents of the starting material or of secondary phases of the final product
    • C04B2235/50Constituents or additives of the starting mixture chosen for their shape or used because of their shape or their physical appearance
    • C04B2235/52Constituents or additives characterised by their shapes
    • C04B2235/5208Fibers
    • C04B2235/5216Inorganic
    • C04B2235/522Oxidic
    • C04B2235/5236Zirconia
    • CCHEMISTRY; METALLURGY
    • C04CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
    • C04BLIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
    • C04B2235/00Aspects relating to ceramic starting mixtures or sintered ceramic products
    • C04B2235/02Composition of constituents of the starting material or of secondary phases of the final product
    • C04B2235/50Constituents or additives of the starting mixture chosen for their shape or used because of their shape or their physical appearance
    • C04B2235/52Constituents or additives characterised by their shapes
    • C04B2235/5208Fibers
    • C04B2235/5216Inorganic
    • C04B2235/524Non-oxidic, e.g. borides, carbides, silicides or nitrides
    • C04B2235/5244Silicon carbide
    • CCHEMISTRY; METALLURGY
    • C04CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
    • C04BLIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
    • C04B2235/00Aspects relating to ceramic starting mixtures or sintered ceramic products
    • C04B2235/02Composition of constituents of the starting material or of secondary phases of the final product
    • C04B2235/50Constituents or additives of the starting mixture chosen for their shape or used because of their shape or their physical appearance
    • C04B2235/52Constituents or additives characterised by their shapes
    • C04B2235/5208Fibers
    • C04B2235/5216Inorganic
    • C04B2235/524Non-oxidic, e.g. borides, carbides, silicides or nitrides
    • C04B2235/5248Carbon, e.g. graphite
    • CCHEMISTRY; METALLURGY
    • C04CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
    • C04BLIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
    • C04B2235/00Aspects relating to ceramic starting mixtures or sintered ceramic products
    • C04B2235/02Composition of constituents of the starting material or of secondary phases of the final product
    • C04B2235/50Constituents or additives of the starting mixture chosen for their shape or used because of their shape or their physical appearance
    • C04B2235/52Constituents or additives characterised by their shapes
    • C04B2235/5208Fibers
    • C04B2235/5268Orientation of the fibers
    • CCHEMISTRY; METALLURGY
    • C04CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
    • C04BLIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
    • C04B2237/00Aspects relating to ceramic laminates or to joining of ceramic articles with other articles by heating
    • C04B2237/30Composition of layers of ceramic laminates or of ceramic or metallic articles to be joined by heating, e.g. Si substrates
    • C04B2237/32Ceramic
    • C04B2237/34Oxidic
    • C04B2237/341Silica or silicates
    • CCHEMISTRY; METALLURGY
    • C04CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
    • C04BLIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
    • C04B2237/00Aspects relating to ceramic laminates or to joining of ceramic articles with other articles by heating
    • C04B2237/30Composition of layers of ceramic laminates or of ceramic or metallic articles to be joined by heating, e.g. Si substrates
    • C04B2237/32Ceramic
    • C04B2237/34Oxidic
    • C04B2237/343Alumina or aluminates
    • CCHEMISTRY; METALLURGY
    • C04CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
    • C04BLIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
    • C04B2237/00Aspects relating to ceramic laminates or to joining of ceramic articles with other articles by heating
    • C04B2237/30Composition of layers of ceramic laminates or of ceramic or metallic articles to be joined by heating, e.g. Si substrates
    • C04B2237/32Ceramic
    • C04B2237/36Non-oxidic
    • C04B2237/365Silicon carbide
    • CCHEMISTRY; METALLURGY
    • C04CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
    • C04BLIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
    • C04B2237/00Aspects relating to ceramic laminates or to joining of ceramic articles with other articles by heating
    • C04B2237/30Composition of layers of ceramic laminates or of ceramic or metallic articles to be joined by heating, e.g. Si substrates
    • C04B2237/32Ceramic
    • C04B2237/38Fiber or whisker reinforced
    • CCHEMISTRY; METALLURGY
    • C04CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
    • C04BLIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
    • C04B2237/00Aspects relating to ceramic laminates or to joining of ceramic articles with other articles by heating
    • C04B2237/30Composition of layers of ceramic laminates or of ceramic or metallic articles to be joined by heating, e.g. Si substrates
    • C04B2237/32Ceramic
    • C04B2237/38Fiber or whisker reinforced
    • C04B2237/385Carbon or carbon composite
    • CCHEMISTRY; METALLURGY
    • C04CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
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    • C04B2237/00Aspects relating to ceramic laminates or to joining of ceramic articles with other articles by heating
    • C04B2237/50Processing aspects relating to ceramic laminates or to the joining of ceramic articles with other articles by heating
    • C04B2237/70Forming laminates or joined articles comprising layers of a specific, unusual thickness
    • C04B2237/704Forming laminates or joined articles comprising layers of a specific, unusual thickness of one or more of the ceramic layers or articles
    • CCHEMISTRY; METALLURGY
    • C04CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
    • C04BLIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
    • C04B2237/00Aspects relating to ceramic laminates or to joining of ceramic articles with other articles by heating
    • C04B2237/50Processing aspects relating to ceramic laminates or to the joining of ceramic articles with other articles by heating
    • C04B2237/76Forming laminates or joined articles comprising at least one member in the form other than a sheet or disc, e.g. two tubes or a tube and a sheet or disc
    • C04B2237/765Forming laminates or joined articles comprising at least one member in the form other than a sheet or disc, e.g. two tubes or a tube and a sheet or disc at least one member being a tube
    • CCHEMISTRY; METALLURGY
    • C04CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
    • C04BLIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
    • C04B2237/00Aspects relating to ceramic laminates or to joining of ceramic articles with other articles by heating
    • C04B2237/50Processing aspects relating to ceramic laminates or to the joining of ceramic articles with other articles by heating
    • C04B2237/84Joining of a first substrate with a second substrate at least partially inside the first substrate, where the bonding area is at the inside of the first substrate, e.g. one tube inside another tube
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C2209/00Vessel construction, in particular methods of manufacturing
    • F17C2209/21Shaping processes
    • F17C2209/2154Winding

Definitions

  • the invention relates to a pressure-resistant fluidbeaufschlagbaren or -ten body such as pressure tube or pressure vessel.
  • the used bodies of the aforementioned steels withstand pressures of up to 300 bar. Higher temperatures and pressures are not feasible, because of the required resistance to the material creep behavior, not feasible for safety and economy.
  • the present invention has the object, a pressure-resistant fluidbeetzschlagbaren or -ten body such as pressure tube or pressure vessel in such a way that an increase in the process temperatures compared to bodies, which consist of steels, is achieved. Also, the body should be acted upon with pressures that are greater than those previously used are usually used.
  • a pressure-resistant fluidbeetzschlagbaren or -ten body such as pressure tube or pressure vessel consisting of a base body made of steel, a body surrounding the outside first layer of ceramic fiber composite material and one or more arranged on the first layer second layers made of fiber-reinforced ceramic and / or fiber-reinforced plastic.
  • Fluid-impingable bodies according to the invention make it possible to increase the process temperatures in comparison to bodies which consist solely of steels. Also, the possibility of pressurization is given, which is larger than usual. This is done according to the invention by the function separation tightness and emergency property of the steel pipe on the one hand and the high temperature creep resistance of the fiber composite material on the other.
  • a multi-layer body which, in particular in steam turbine processes, offers the possibility of increasing the process temperature by at least 200 ° C. compared with the materials used hitherto, so that the thermal efficiency in power stations can be increased by approximately 7%.
  • a corresponding composite tube shows good compressive and tensile stress in the axial and radial directions and a temperature resistance up to in the range between 900 0 C and 1000 0 C.
  • the existing of fiber composite material first layer acts insofar thermo-insulating, ie generates a temperature gradient of the steel pipe in the outer layer so that it does not oxidize. Also, an economical production is possible.
  • CMC ceramic fiber composites
  • the thermal fiber composites are characterized by an embedded between ceramic fibers, especially long fibers, embedded matrix of ceramic, which is reinforced by the ceramic fibers. Therefore one speaks of fiber-reinforced ceramics, composite ceramics or simply fiber ceramics.
  • matrix and fiber may consist of all known ceramic materials, in which context carbon is also treated as a ceramic material.
  • the fibers of the ceramic composite material are alumina, mullite, silicon carbide, zirconia and / or carbon fibers.
  • Mullite consists of mixed crystals of alumina and silica.
  • the ceramic fiber composite used is preferably SiC / SiC, C / C, C / SiC, Al 2 O 3 / Al 2 O 3 and / or mullite / mullite.
  • the material before the slash designates the fiber type and the material after the slash designates the matrix type.
  • Si precursors and various oxides, such as zirconia can be used as a matrix system for the ceramic fiber composite structure and siloxanes.
  • the first layer preferably has a thickness D 1 of 1 mm ⁇ D 1 ⁇ 20 mm and / or the second layer or layers has a total thickness D 2 of 0 mm ⁇ D 2 ⁇ 50 mm.
  • the fibers of the fiber-reinforced carbon can be arranged radially encircling and / or crossing on the first layer.
  • the fibers of the first layer can likewise be deposited radially on the base body and / or crossing each other.
  • the main body preferably consists of martensitic steel or high-alloy nickel-based alloy material.
  • wall thicknesses D 3 with 2 mm ⁇ D 3 ⁇ 50 mm are to be specified as preferred values, without thereby restricting the teaching according to the invention.
  • the fiber volume Fv of the first layer should be 30% ⁇ F v ⁇ 70%.
  • the porosity P of the first layer is 5% ⁇ P ⁇ 50%.
  • the ceramic fiber composite material can be produced by CVI (Chemical Vapor Infiltration) method, pyrolysis, in particular LPI (Liquid Polymer Infiltration) method or by chemical reaction such as LSI (Liquid Silicon Infiltration) method.
  • CVI Chemical Vapor Infiltration
  • LPI Liquid Polymer Infiltration
  • LSI Liquid Silicon Infiltration
  • Si-based precursor is used as the matrix material, to then be converted into SiC by pyrolysis.
  • Si-based precursors have the advantage that they are readily hardenable and pyrolyzable, so that problem-free production is ensured.
  • the invention is also characterized in a very general way by a pressure-resistant body which can be acted upon by fluid or pressure vessel or pressure vessel consisting of steel and a layer surrounding the basic body consisting of or containing fibers which at a temperature T with T> 500 ° C. is no or show minimal creep strain.
  • Fibers in the creep - in the temperature range above 550 0 C - show no or minimal increase in time of permanent deformation, so the creep, whereby the creep of the inner steel tube is stopped.
  • the fibers are characterized by a high creep strength to the effect that the strength is ensured in particular under atmospheric air at high operating temperatures.
  • Suitable fibers are reinforcing fibers which fall into the classes oxide, carbide, nitridic fibers or C fibers and SiBCN fibers.
  • Plastic fibers such as PAN fibers or polyacrylonitrile fibers are also referred to as reinforcing fibers.
  • Fig. 1 is a schematic diagram of a pressure tube
  • Fig. 2 is a schematic diagram of a container.
  • a pressure tube 10 is shown in sectional view, which is used in particular in the power plant area for steam turbine processes used.
  • the tube 10 is formed as a composite tube.
  • the tube 10 consists of a base body 12 made of steel, on which at least two layers 14, 16 are applied.
  • the arranged on the base body 12 layer 14, which is referred to as the first layer made of a ceramic fiber composite material and the at least one first layer 14 covering the second layer 16 of fiber-reinforced plastic and / or fiber-reinforced ceramic.
  • the plastic content serves to increase the expansion compatibility.
  • the ceramic fiber composite material of the first layer 14 may consist of known ceramic materials, wherein preferably SiC / SiC, Al 2 O 3 / Al 2 O 3 or mullite / mullite are mentioned.
  • the first layer 14 of the ceramic fiber composite material ensures that a thermal insulation between the main body 12 and the at least one second layer 16 of the fiber-reinforced plastic, be it fiber-reinforced plastic, be it fiberglass-reinforced plastic, is built up to such an extent that oxidation of the at least one second layer 16 is prevented. This ensures that the at least one second layer 16 provides the desired reinforcement, so that the composite pipe 10 can be acted upon by the desired high pressures.
  • the second layer is also responsible for generating the bias on the pressure tube or pressure vessel, which increases with increasing application temperatures.
  • the first layer 14 allows the composite pipe 10 to increase the efficiency with the required high temperatures of at least 800 0 C - 850 0 C, optionally applied to 1000 0 C.
  • the fibers of the first layer 14 may be deposited according to the requirements. Thus, the fibers may be crossing and / or surrounding the main body 12 radially surrounding. The same applies with regard to the fibers of the at least one second layer 16.
  • a pressure vessel 18 is shown purely in principle, which is also composed of a base body 20 made of steel and arranged on the base body 20 first and second layers 24, 26, wherein the first layer 24 of a ceramic fiber composite material and the at least one second Layer 26 consists of fiber-reinforced plastic and / or fiber-reinforced ceramic.
  • manufacturing methods and materials can be used, as they have been previously explained.
  • FIG. 2 shows fibers 28, 30 of the first layer 24, which are deposited radially on the base body 22 (long fibers 28) or intersecting (long fibers 30). Other fiber processes known from the prior art are also possible.
  • the base body 12 for example, a clear diameter of 500 mm and a wall thickness of 40 mm.
  • the existing of the ceramic fiber composite material first layer 14 has a thickness D 1 - IO mm and the second made of fiber-reinforced carbon layer 16 has a thickness D 2 - IO mm.
  • the base body 22 may have a diameter of 300 mm and a length of 500 mm and a wall thickness of 30 mm.
  • the thickness D 1 of the first layer 24 may be D 1 - IS mm and the thickness D 2 of the second layer 26 may be D 2 - IO mm, to name numbers purely by way of example.
  • Respective composite tubes 10 or composite container 20 can be acted upon by fluids at a temperature of about 850 °, so that a high-temperature use, especially in steam turbine processes can take place, which compared to pressure tubes or pressure bodies of conventional construction, the thermal efficiency can be significantly increased.
  • corresponding composites show a damage tolerant good-natured failure and creep resistance. Compression and tension in both axial and radial directions are possible without damaging the body. Also, an economical production is possible.
  • the invention is also not leave, if only one layer is applied of reinforcing fibers on the base body with no or minimal increase over time in the temperature range above 550 0 C. show the permanent deformation, so the creep, whereby the creep of the inner body is stopped.
  • the corresponding fibers also have a high creep rupture strength, the strength in particular under atmospheric air is ensured at high operating temperatures.
  • Corresponding fibers can be classified into the classes oxide, carbidic, nitridic or C-fibers or SiBCN-fibers. Also plastic fibers such as PAN or polyacrylonitrile fibers come into question.
  • C-fibers C-fibers, Nextel fibers, 3M fibers, Hi-Nicalon fibers, oxide fibers, SiO 2 , Al 2 O 3 , SiC, SiBCN, PAN and Si 3 N 4 - fibers.
  • a boiler tube which may consist of austenitic or martensitic steel (9% chromium steel), which for example has an outer diameter of about 42 mm and a wall thickness of about 6 mm. This may be wrapped with a layer of previously stated reinforcing fibers having a thickness in the range of 3 mm to 4 mm in order to achieve the desired properties.

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  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Ceramic Engineering (AREA)
  • Laminated Bodies (AREA)
  • Rigid Pipes And Flexible Pipes (AREA)
  • Pressure Vessels And Lids Thereof (AREA)

Abstract

The invention relates to a pressure-resistant body (10), such as a pressure pipe or pressure container, consisting of a steel base body (12), a first layer (14) of a ceramic fibre composite that surrounds the exterior of the base body and at least one second layer (16) of a fibre-reinforced plastic and/or a fibre-reinforced ceramic that is situated on the first layer.

Description

Druckfester fluidbeaufschlagter KörperPressure-resistant fluid-loaded body
Die Erfindung bezieht sich auf einen druckfesten fluidbeaufschlagbaren bzw. -ten Körper wie Druckrohr oder Druckbehälter.The invention relates to a pressure-resistant fluidbeaufschlagbaren or -ten body such as pressure tube or pressure vessel.
Bei Dampfturbinenprozessen hängt der Wirkungsgrad von der Prozesstemperatur ab. Daher ist man bestrebt, die Prozesstemperatur so hoch wie möglich einzustellen. Nach dem Stand der Technik werden für für Dampfturbinenprozesse benötigte druckfeste Körper wie Druckrohre oder Druckbehälter aus martensitischen Stählen oder hochlegierten Nickel- Basislegierungen hergestellt. Mit diesen Materialien lassen sich Prozesstemperaturen bis 650 0C bzw. 700 0C erzielen. Allerdings wird bei martensitischen Stählen aus Sicherheitsgründen üblicherweise eine Temperatur von mehr als 620 0C nicht überschritten.For steam turbine processes, the efficiency depends on the process temperature. Therefore, one strives to set the process temperature as high as possible. According to the state of the art, pressure-resistant bodies, such as pressure pipes or pressure vessels, required for steam turbine processes, are produced from martensitic steels or high-alloy nickel base alloys. With these materials, process temperatures up to 650 0 C and 700 0 C can be achieved. However, for martensitic steels usually a temperature of more than 620 0 C is not exceeded for safety reasons.
Die zum Einsatz gelangenden Körper aus zuvor genannten Stählen halten Drücke bis 300 bar aus. Höhere Temperaturen und Drücke sind nicht realisierbar, wegen der erforderlichen Beständigkeit gegen das Werkstoffkriechverhalten, wegen der Sicherheit und wegen der Wirtschaftlichkeit nicht realisierbar.The used bodies of the aforementioned steels withstand pressures of up to 300 bar. Higher temperatures and pressures are not feasible, because of the required resistance to the material creep behavior, not feasible for safety and economy.
Der vorliegenden Erfindung liegt die Aufgabe zugrunde, einen druckfesten fluidbeaufschlagbaren bzw. -ten Körper wie Druckrohr oder Druckbehälter derart weiterzubilden, dass eine Erhöhung der Prozesstemperaturen im Vergleich zu Körpern, die aus Stählen bestehen, erreicht wird. Auch sollen die Körper mit Drücken beaufschlagbar sein, die größer als die bisher üblicherweise zum Einsatz gelangenden sind Zur Lösung der Aufgabe schlägt die Erfindung im Wesentlichen vor einen druckfesten fluidbeaufschlagbaren bzw. -ten Körper wie Druckrohr oder Druckbehälter bestehend aus einem Grundkörper aus Stahl, einer den Grundkörper außenseitig umschließenden ersten Schicht aus keramischem Faserverbundwerkstoff und einer oder mehreren auf der ersten Schicht angeordneten zweiten Schichten aus faserverstärkter Keramik und/oder faserverstärktem Kunststoff.The present invention has the object, a pressure-resistant fluidbeaufschlagbaren or -ten body such as pressure tube or pressure vessel in such a way that an increase in the process temperatures compared to bodies, which consist of steels, is achieved. Also, the body should be acted upon with pressures that are greater than those previously used are usually used To achieve the object, the invention proposes essentially in front of a pressure-resistant fluidbeaufschlagbaren or -ten body such as pressure tube or pressure vessel consisting of a base body made of steel, a body surrounding the outside first layer of ceramic fiber composite material and one or more arranged on the first layer second layers made of fiber-reinforced ceramic and / or fiber-reinforced plastic.
Erfindungsgemäße fluidbeaufschlagbare bzw. -te Körper wie Druckrohre oder Druckbehälter ermöglichen eine Erhöhung der Prozesstemperaturen im Vergleich zu Körpern, die allein aus Stählen bestehen. Auch ist die Möglichkeit einer Druckbeaufschlagung gegeben, die größer als bisher üblich ist. Dies erfolgt erfindungsgemäß durch die Funktionstrennung Dichtheit und Notfalleigenschaft des Stahlrohres einerseits und der Hochtemperatur- Kriechbeständigkeit des Faserverbundwerkstoffs andererseits.Fluid-impingable bodies according to the invention, such as pressure pipes or pressure vessels, make it possible to increase the process temperatures in comparison to bodies which consist solely of steels. Also, the possibility of pressurization is given, which is larger than usual. This is done according to the invention by the function separation tightness and emergency property of the steel pipe on the one hand and the high temperature creep resistance of the fiber composite material on the other.
Erfindungsgemäß wird ein Mehrschichtkörper zur Verfügung gestellt, der insbesondere bei Dampfturbinenprozessen die Möglichkeit bietet, die Prozesstemperatur im Vergleich zu den bisher zum Einsatz gelangenden Materialien um zumindest 200 0C zu erhöhen, wodurch der thermische Wirkungsgrad bei Kraftwerken um ca. 7 % gesteigert werden kann. Ein entsprechendes Verbundrohr zeigt gute Druck- und Zugbeanspruchung in axialer und radialer Richtung und eine Temperaturbeständigkeit bis im Bereich zwischen 900 0C und 1000 0C. Die aus Faserverbundwerkstoff bestehende erste Schicht wirkt insoweit thermo- isolierend, d.h. erzeugt einen Temperaturgradient von dem Stahlrohr in die äußere Schicht, so dass diese nicht oxidiert. Auch ist eine wirtschaftliche Herstellung möglich.According to the invention, a multi-layer body is provided which, in particular in steam turbine processes, offers the possibility of increasing the process temperature by at least 200 ° C. compared with the materials used hitherto, so that the thermal efficiency in power stations can be increased by approximately 7%. A corresponding composite tube shows good compressive and tensile stress in the axial and radial directions and a temperature resistance up to in the range between 900 0 C and 1000 0 C. The existing of fiber composite material first layer acts insofar thermo-insulating, ie generates a temperature gradient of the steel pipe in the outer layer so that it does not oxidize. Also, an economical production is possible.
Zwar ist es bekannt, keramische Faserverbundwerkstoffe (Ceramic Matrix Composites (CMC)) bei hohen Temperaturen einzusetzen. So werden CMC -Werkstoffe für Gasturbinen im Bereich der heißen Gase, also der Turbinenbrennkammer, den statischen, den Gasstrom lenkenden Leitschaufeln und den eigentlichen Turbinenschaufeln, die den Verdichter der Gasturbine antreiben, eingesetzt. Allerdings bestehen die entsprechenden Komponenten ausschließlich aus CMC -Werkstoffen und weisen nicht den erfindungsgemäßen Schichtaufbau auf. Dieser stellt jedoch sicher, dass ein Einsatz bei hohen Temperaturen bis 1000 0C und Drücken von 300 bar und mehr problemlos erfolgen kann, wobei gleichzeitig eine Kriechbeständigkeit des Körpers von zumindest 30 Jahren gewährleistet ist.Although it is known to use ceramic fiber composites (CMC) at high temperatures. Thus, CMC materials for gas turbines in the field of hot gases, so the turbine combustor, the static, the gas flow directing vanes and the actual turbine blades that drive the compressor of the gas turbine used. However, the corresponding components consist exclusively of CMC materials and do not have the layer structure according to the invention. However, this ensures that use at high temperatures up 1000 0 C and pressures of 300 bar and more can be done easily, at the same time a creep resistance of the body is guaranteed by at least 30 years.
Die thermischen Faserverbundwerkstoffe sind charakterisiert durch eine zwischen keramischen Fasern, insbesondere Langfasern, eingebettete Matrix aus Keramik, die durch die keramischen Fasern verstärkt wird. Daher spricht man von faserverstärkter Keramik, Verbundkeramik oder auch einfach Faserkeramik. Matrix und Faser können dabei im Prinzip aus allen bekannten keramischen Werkstoffen bestehen, wobei in diesem Zusammenhang auch Kohlenstoff als keramischer Werkstoff behandelt wird.The thermal fiber composites are characterized by an embedded between ceramic fibers, especially long fibers, embedded matrix of ceramic, which is reinforced by the ceramic fibers. Therefore one speaks of fiber-reinforced ceramics, composite ceramics or simply fiber ceramics. In principle, matrix and fiber may consist of all known ceramic materials, in which context carbon is also treated as a ceramic material.
Insbesondere ist vorgesehen, dass die Fasern des keramischen Verbundwerkstoffes Aluminiumoxid-, Mullit-, Siliziumcarbid-, Zirkonoxid- und/oder Kohlenstoff-Fasern sind. Mullit besteht dabei aus Mischkristallen aus Aluminiumoxid und Siliziumoxid.In particular, it is provided that the fibers of the ceramic composite material are alumina, mullite, silicon carbide, zirconia and / or carbon fibers. Mullite consists of mixed crystals of alumina and silica.
Bevorzugterweise wird als keramischer Faserverbundwerkstoff SiC/SiC, C/C, C/SiC, AI2O3/AI2O3 und/oder Mullit/Mullit eingesetzt. Dabei bezeichnet das Material vor dem Schrägstrich den Fasertyp und das Material nach dem Schrägstrich den Matrixtyp. Als Matrixsystem für die keramische Faserverbundstruktur können auch Siloxane, Si- Precursoren und unterschiedlichste Oxide, wie zum Beispiel auch Zirkonoxid, eingesetzt werden.The ceramic fiber composite used is preferably SiC / SiC, C / C, C / SiC, Al 2 O 3 / Al 2 O 3 and / or mullite / mullite. In this case, the material before the slash designates the fiber type and the material after the slash designates the matrix type. As a matrix system for the ceramic fiber composite structure and siloxanes, Si precursors and various oxides, such as zirconia, can be used.
Bevorzugterweise weisen die erste Schicht eine Dicke D1 mit 1 mm < D1 < 20 mm und/oder die zweite Schicht bzw. Schichten insgesamt eine Dicke D2 mit 0 mm < D2 ≤ 50 mm auf.The first layer preferably has a thickness D 1 of 1 mm <D 1 <20 mm and / or the second layer or layers has a total thickness D 2 of 0 mm <D 2 ≦ 50 mm.
Um eine gewünschte Armierung durch die zumindest eine zweite Schicht zu erzielen, können die Fasern des faserverstärkten Kohlenstoffs radial umlaufend und/oder sich kreuzend auf der ersten Schicht angeordnet sein. Die Fasern der ersten Schicht können gleichfalls radial umlaufend und/oder sich kreuzend auf dem Grundkörper abgelegt sein. Der Grundkörper besteht bevorzugterweise aus martensitischem Stahl oder hochlegiertem Nickel-Basislegierungsmaterial. Dabei sind Wandstärken D3 mit 2 mm < D3 < 50 mm als bevorzugte Werte anzugeben, ohne dass hierdurch eine Einschränkung der erfindungsgemäßen Lehre erfolgt.In order to achieve a desired reinforcement by the at least one second layer, the fibers of the fiber-reinforced carbon can be arranged radially encircling and / or crossing on the first layer. The fibers of the first layer can likewise be deposited radially on the base body and / or crossing each other. The main body preferably consists of martensitic steel or high-alloy nickel-based alloy material. In this case, wall thicknesses D 3 with 2 mm <D 3 <50 mm are to be specified as preferred values, without thereby restricting the teaching according to the invention.
Das Faservolumen Fv der ersten Schicht sollte betragen 30 % < Fv ≤ 70 %. Bevorzugterweise beträgt die Porosität P der ersten Schicht 5 % < P < 50 %.The fiber volume Fv of the first layer should be 30% <F v ≦ 70%. Preferably, the porosity P of the first layer is 5% <P <50%.
Der keramische Faserverbundwerkstoff kann durch CVI (Chemical Vapour Infiltration) - Verfahren, Pyrolyse, insbesondere LPI (Liquid Polymer Infiltration) -Verfahren oder durch chemische Reaktion wie LSI (Liquid Silicon Infiltration) -Verfahren hergestellt werden.The ceramic fiber composite material can be produced by CVI (Chemical Vapor Infiltration) method, pyrolysis, in particular LPI (Liquid Polymer Infiltration) method or by chemical reaction such as LSI (Liquid Silicon Infiltration) method.
Bevorzugterweise wird als Matrixmaterial ein Precursor auf Si-Basis benutzt, um sodann mittels Pyrolyse in SiC umgewandelt zu werden. Precursor auf Si-Basis zeigen den Vorteil, dass diese leicht hart- und pyrolisierbar sind, so dass eine problemlose Herstellung gegeben ist.Preferably, an Si-based precursor is used as the matrix material, to then be converted into SiC by pyrolysis. Si-based precursors have the advantage that they are readily hardenable and pyrolyzable, so that problem-free production is ensured.
Die Erfindung zeichnet sich ganz allgemein auch durch einen druckfesten fluid- beaufschlagbaren bzw. -ten Körper wie Druckrohr oder Druckbehälter bestehend aus Stahl und einer den Grundkörper umgebenden Schicht bestehend aus oder enthaltend Fasern, die bei einer Temperatur T mit T > 500 0C keine oder minimale Kriechdehnung zeigen.The invention is also characterized in a very general way by a pressure-resistant body which can be acted upon by fluid or pressure vessel or pressure vessel consisting of steel and a layer surrounding the basic body consisting of or containing fibers which at a temperature T with T> 500 ° C. is no or show minimal creep strain.
Es gelangen kriechbeständige Fasern zum Einsatz, d. h. Fasern, die im Kriechbereich - im Temperaturbereich oberhalb 550 0C - keine oder minimale zeitliche Zunahme der bleibenden Verformung, also der Kriechdehnung zeigen, wodurch das Kriechen des innenliegenden Stahlrohres aufgehalten wird. Chemisch sind die Fasern durch eine hohe Zeitstandfestigkeit dahingehend zu charakterisieren, dass die Festigkeit insbesondere unter atmosphärischer Luft bei hohen Betriebstemperaturen gewährleistet ist. Als Fasern kommen Verstärkungsfasern in Frage, die in die Klassen oxidische, carbidi- sche, nitridische Fasern bzw. C-Fasern und SiBCN-Fasern fallen. Kunststofffasern wie PAN-Fasern oder Polyacrylnitril-Fasern sind auch als Verstärkungsfasern zu bezeichnen.It creep-resistant fibers are used, ie fibers in the creep - in the temperature range above 550 0 C - show no or minimal increase in time of permanent deformation, so the creep, whereby the creep of the inner steel tube is stopped. Chemically, the fibers are characterized by a high creep strength to the effect that the strength is ensured in particular under atmospheric air at high operating temperatures. Suitable fibers are reinforcing fibers which fall into the classes oxide, carbide, nitridic fibers or C fibers and SiBCN fibers. Plastic fibers such as PAN fibers or polyacrylonitrile fibers are also referred to as reinforcing fibers.
Weitere Einzelheiten, Vorteile und Merkmale der Erfindung ergeben sich nicht nur aus den Ansprüchen, den diesen zu entnehmenden Merkmalen -für sich und/oder in Kombination-, sondern auch aus der nachfolgenden Beschreibung von der Zeichnung zu entnehmenden bevorzugten Ausführungsbeispielen.Further details, advantages and features of the invention will become apparent not only from the claims, the features to be taken from them-alone and / or in combination-but also from the following description of preferred embodiments to be taken from the drawings.
Es zeigen:Show it:
Fig. 1 eine Prinzipdarstellung eines Druckrohres undFig. 1 is a schematic diagram of a pressure tube and
Fig. 2 eine Prinzipdarstellung eines Behälters.Fig. 2 is a schematic diagram of a container.
In Fig. 1 ist ein Druckrohr 10 in Schnittdarstellung wiedergegeben, das insbesondere im Kraftwerksbereich für Dampfturbinenprozesse zum Einsatz gelangt. Um das Druckrohr 10 von Fluiden unter Drücken bis 300 bar oder mehr bei Temperaturen von 800°, insbesondere 850° oder mehr durchströmen zu lassen, ist das Rohr 10 als Verbundrohr ausgebildet. Das Rohr 10 besteht aus einem Grundkörper 12 aus Stahl, auf dem zumindest zwei Schichten 14, 16 aufgebracht sind. Dabei besteht die auf dem Grundkörper 12 angeordnete Schicht 14, die als erste Schicht bezeichnet wird, aus einem keramischen Faserverbundwerkstoff und die zumindest eine die erste Schicht 14 abdeckende zweite Schicht 16 aus faserverstärktem Kunststoff und/oder faserverstärkter Keramik. Der Kunststoffanteil dient zur Steigerung der Dehnungsverträglichkeit.In Fig. 1, a pressure tube 10 is shown in sectional view, which is used in particular in the power plant area for steam turbine processes used. In order to let the pressure tube 10 of fluids flow under pressures of up to 300 bar or more at temperatures of 800 °, in particular 850 ° or more, the tube 10 is formed as a composite tube. The tube 10 consists of a base body 12 made of steel, on which at least two layers 14, 16 are applied. Here, the arranged on the base body 12 layer 14, which is referred to as the first layer, made of a ceramic fiber composite material and the at least one first layer 14 covering the second layer 16 of fiber-reinforced plastic and / or fiber-reinforced ceramic. The plastic content serves to increase the expansion compatibility.
Der keramische Faserverbundwerkstoff aus der ersten Schicht 14 kann aus bekannten keramischen Werkstoffen bestehen, wobei bevorzugterweise SiC/SiC, AI2O3/AI2O3 oder Mullit/Mullit zu nennen sind. Die erste Schicht 14 aus dem keramischen Faserverbundwerkstoff stellt sicher, dass eine thermische Isolierung zwischen dem Grundkörper 12 und der zumindest einen zweiten Schicht 16 aus dem faserverstärkten Kunststoff, sei es kohlen- stofffaserverstärkter Kunststoff, sei es glasfaserverstärkter Kunststoff, in einem Umfang aufgebaut wird, dass eine Oxidation der zumindest einen zweiten Schicht 16 unterbleibt. Hierdurch ist sichergestellt, dass die zumindest eine zweite Schicht 16 die gewünschte Armierung bietet, so dass das Verbundrohr 10 mit den gewünschten hohen Drücken beaufschlagbar ist. Die zweite Schicht ist auch für die Erzeugung der Vorspannung auf dem Druckrohr bzw. Druckbehälter verantwortlich, wobei diese mit zunehmenden Anwendungstemperaturen steigt.The ceramic fiber composite material of the first layer 14 may consist of known ceramic materials, wherein preferably SiC / SiC, Al 2 O 3 / Al 2 O 3 or mullite / mullite are mentioned. The first layer 14 of the ceramic fiber composite material ensures that a thermal insulation between the main body 12 and the at least one second layer 16 of the fiber-reinforced plastic, be it fiber-reinforced plastic, be it fiberglass-reinforced plastic, is built up to such an extent that oxidation of the at least one second layer 16 is prevented. This ensures that the at least one second layer 16 provides the desired reinforcement, so that the composite pipe 10 can be acted upon by the desired high pressures. The second layer is also responsible for generating the bias on the pressure tube or pressure vessel, which increases with increasing application temperatures.
Zur Vorspannung ist anzumerken, dass diese beim Anfahren mit steigendem Druck und Temperatur in der Faserummantelung entsteht und mit der Zeit teilweise durch das Kriechverhalten des innenliegenden Strahlrohres zeitabhängig abgebaut wird.For prestressing, it should be noted that this arises during start-up with increasing pressure and temperature in the fiber casing and is degraded over time in part by the creep behavior of the inner jet pipe in a time-dependent manner.
Die erste Schicht 14 ermöglicht, dass das Verbundrohr 10 zur Steigerung des Wirkungsgrades mit den erforderlichen hohen Temperaturen von zumindest 800 0C - 850 0C, gegebenenfalls bis 1000 0C beaufschlagt werden kann.The first layer 14 allows the composite pipe 10 to increase the efficiency with the required high temperatures of at least 800 0 C - 850 0 C, optionally applied to 1000 0 C.
Die Fasern der ersten Schicht 14 können den Anforderungen entsprechend abgelegt sein. So können die Fasern sich kreuzend und/oder radial umlaufend den Grundkörper 12 umgeben. Gleiches gilt bezüglich der Fasern der zumindest einen zweiten Schicht 16.The fibers of the first layer 14 may be deposited according to the requirements. Thus, the fibers may be crossing and / or surrounding the main body 12 radially surrounding. The same applies with regard to the fibers of the at least one second layer 16.
In Fig. 2 ist rein prinzipiell ein Druckbehälter 18 dargestellt, der ebenfalls aus einem Grundkörper 20 aus Stahl und auf dem Grundkörper 20 angeordneten ersten und zweiten Schichten 24, 26 aufgebaut ist, wobei die erste Schicht 24 aus einem keramischen Faserverbundwerkstoff und die zumindest eine zweite Schicht 26 aus faserverstärktem Kunststoff und/oder faserverstärkter Keramik besteht. Dabei können Herstellungsverfahren und Materialien zum Einsatz gelangen, wie diese zuvor erläutert worden sind. Rein beispielhaft sind der Fig. 2 Fasern 28, 30 der ersten Schicht 24 zu entnehmen, die radial umlaufend (Langfasern 28) oder sich kreuzend (Langfasern 30) auf dem Grundkörper 22 abgelegt sind. Andere aus dem Stand der Technik bekannte Faserverläufe sind gleichfalls möglich. Bei dem Ausführungsbeispiel der Fig. 1 weist der Grundkörper 12 zum Beispiel einen lichten Durchmesser von 500 mm und eine Wandstärke von 40 mm auf. Die aus dem keramischen Faserverbundwerkstoff bestehende erste Schicht 14 weist eine Dicke D1 - IO mm und die zweite aus faserverstärktem Kohlenstoff bestehende Schicht 16 eine Dicke D2 - IO mm auf.In Fig. 2, a pressure vessel 18 is shown purely in principle, which is also composed of a base body 20 made of steel and arranged on the base body 20 first and second layers 24, 26, wherein the first layer 24 of a ceramic fiber composite material and the at least one second Layer 26 consists of fiber-reinforced plastic and / or fiber-reinforced ceramic. In this case, manufacturing methods and materials can be used, as they have been previously explained. By way of example, FIG. 2 shows fibers 28, 30 of the first layer 24, which are deposited radially on the base body 22 (long fibers 28) or intersecting (long fibers 30). Other fiber processes known from the prior art are also possible. In the embodiment of Fig. 1, the base body 12, for example, a clear diameter of 500 mm and a wall thickness of 40 mm. The existing of the ceramic fiber composite material first layer 14 has a thickness D 1 - IO mm and the second made of fiber-reinforced carbon layer 16 has a thickness D 2 - IO mm.
Bei dem Druckbehälter 20 nach der Fig. 2 kann der Grundkörper 22 einen Durchmesser von 300 mm und eine Länge von 500 mm sowie eine Wandstärke von 30 mm aufweisen. Die Dicke D1 der ersten Schicht 24 kann betragen D1 - IS mm und die Dicke D2 der zweiten Schicht 26 kann betragen D2 - IO mm, um rein beispielhaft Zahlen zu nennen.In the pressure vessel 20 according to FIG. 2, the base body 22 may have a diameter of 300 mm and a length of 500 mm and a wall thickness of 30 mm. The thickness D 1 of the first layer 24 may be D 1 - IS mm and the thickness D 2 of the second layer 26 may be D 2 - IO mm, to name numbers purely by way of example.
Erfindungsgemäß soll die Dicke D der Faserummantelung sich zu der Wanddicke d des Druckbehälters 20 verhalten wie 0,4 d < D < 0,6, insbesondere d/2 = D.According to the invention, the thickness D of the fiber cladding should behave as the wall thickness d of the pressure vessel 20 as 0.4 d <D <0.6, in particular d / 2 = D.
Entsprechende Verbundrohre 10 bzw. Verbundbehälter 20 können mit Fluiden einer Temperatur von in etwa 850° beaufschlagt werden, so dass ein Hochtemperatureinsatz, insbesondere bei Dampfturbinenprozessen erfolgen kann, wodurch im Vergleich zu Druckrohren bzw. Druckkörpern üblichen Aufbaus der thermische Wirkungsgrad erheblich erhöht werden kann. Gleichzeitig zeigen entsprechende Verbundkörper ein schadenstolerantes gutmütiges Bruchversagen und eine Kriechbeständigkeit. Druck- und Zugbeanspruchung in sowohl axialer als auch radialer Richtung sind möglich, ohne dass der Körper beschädigt wird. Auch ist eine wirtschaftliche Herstellung möglich.Respective composite tubes 10 or composite container 20 can be acted upon by fluids at a temperature of about 850 °, so that a high-temperature use, especially in steam turbine processes can take place, which compared to pressure tubes or pressure bodies of conventional construction, the thermal efficiency can be significantly increased. At the same time corresponding composites show a damage tolerant good-natured failure and creep resistance. Compression and tension in both axial and radial directions are possible without damaging the body. Also, an economical production is possible.
Sind die Ausführungsbeispiele anhand eines Grundkörpers mit auf diesen aufgebrachter ersten und zweiten Schicht erläutert worden, so wird die Erfindung auch dann nicht verlassen, wenn auf den Grundkörper nur eine Schicht aus Verstärkungsfasern aufgebracht wird, die im Temperaturbereich oberhalb 550 0C keine oder minimale zeitliche Zunahme der bleibenden Verformung, also der Kriechdehnung zeigen, wodurch das Kriechen des innenliegenden Grundkörpers aufgehalten wird. Die entsprechenden Fasern weisen auch eine hohe Zeitstandfestigkeit auf, wobei die Festigkeit insbesondere unter atmosphärischer Luft bei hohen Betriebstemperaturen gewährleistet wird. Entsprechende Fasern können in die Klassen oxidische, carbidische, nitridische Fasern oder C-Fasern oder SiBCN-Fasern klassifiziert werden. Auch Kunststofffasern wie PAN- oder Polyacrylnitril-Fasern kommen in Frage.Are the embodiments have been explained using a base body with applied on these first and second layers, the invention is also not leave, if only one layer is applied of reinforcing fibers on the base body with no or minimal increase over time in the temperature range above 550 0 C. show the permanent deformation, so the creep, whereby the creep of the inner body is stopped. The corresponding fibers also have a high creep rupture strength, the strength in particular under atmospheric air is ensured at high operating temperatures. Corresponding fibers can be classified into the classes oxide, carbidic, nitridic or C-fibers or SiBCN-fibers. Also plastic fibers such as PAN or polyacrylonitrile fibers come into question.
Insbesondere sind nachstehende Fasern zu nennen: C-Fasern, Nextel-Fasern, 3M-Fasern, Hi-Nicalon-Fasern, oxidische Fasern, SiO2-, Al2O3-, SiC-, SiBCN-, PAN- und Si3N4- Fasern.In particular, the following fibers are mentioned: C-fibers, Nextel fibers, 3M fibers, Hi-Nicalon fibers, oxide fibers, SiO 2 , Al 2 O 3 , SiC, SiBCN, PAN and Si 3 N 4 - fibers.
Anwendungsbeispiel eines entsprechenden Körpers ist z. B. ein Kesselrohr, das aus Auste- nit oder martensitischem Stahl (9 % Chromstahl) bestehen kann, das beispielhaft einen Außendurchmesser von in etwa 42 mm und eine Wanddicke von in etwa 6 mm aufweist. Dieses kann mit einer Schicht zuvor angegebener Verstärkungsfasern einer Dicke im Bereich von 3 mm bis 4 mm umwickelt sein, um die gewünschten Eigenschaften zu erzielen. Application example of a corresponding body is z. Example, a boiler tube, which may consist of austenitic or martensitic steel (9% chromium steel), which for example has an outer diameter of about 42 mm and a wall thickness of about 6 mm. This may be wrapped with a layer of previously stated reinforcing fibers having a thickness in the range of 3 mm to 4 mm in order to achieve the desired properties.

Claims

PatentansprücheDruckfester fluidbeaufschlagter Körper Claims Pressure-resistant fluid-loaded body
1. Druckfester fluidbeauf schlagbarer bzw. -ter Körper (10, 20) wie Druckrohr oder Druckbehälter bestehend aus einem Grundkörper (12, 22) aus Stahl, einer den Grundkörper außenseitig umschließenden ersten Schicht (14, 24) aus keramischem Faserverbundwerkstoff und zumindest einer auf der ersten Schicht angeordneten zweiten Schicht (16, 26) aus faserverstärktem Kunststoff und/oder faserverstärkter Keramik.1. Pressure-resistant fluidbeauf beatable or -ter body (10, 20) such as pressure tube or pressure vessel consisting of a base body (12, 22) made of steel, the outer body surrounding the outer first layer (14, 24) of ceramic fiber composite material and at least one on the first layer arranged second layer (16, 26) made of fiber-reinforced plastic and / or fiber-reinforced ceramic.
2. Körper nach Anspruch 1, dadurch gekennzeichnet, dass Fasern des keramischen Verbundwerkstoffs Aluminiumoxid-, Mullit-, Silizium- carbid-, Zirkonoxid- und/oder Kohlenstoff-Fasern sind.2. Body according to claim 1, characterized in that fibers of the ceramic composite material are alumina, mullite, silicon carbide, zirconia and / or carbon fibers.
3. Körper nach Anspruch 1 oder 2, dadurch gekennzeichnet, dass der keramische Faserverbundwerkstoff aus SiC/SiC, C/C, C/SiC, AI2O3/AI2O3, C/Siloxan, SiC/Siloxan und/oder Mullit/Mullit besteht.3. Body according to claim 1 or 2, characterized in that the ceramic fiber composite material of SiC / SiC, C / C, C / SiC, Al 2 O 3 / Al 2 O 3 , C / siloxane, SiC / siloxane and / or mullite / Mullite exists.
4. Körper nach zumindest einem der vorhergehenden Ansprüche, dadurch gekennzeichnet, dass die erste Schicht (14) eine Dicke D1 mit 1 mm < D1 < 20 mm aufweist. 4. Body according to at least one of the preceding claims, characterized in that the first layer (14) has a thickness D 1 with 1 mm <D 1 <20 mm.
5. Körper nach zumindest einem der vorhergehenden Ansprüche, dadurch gekennzeichnet, dass die zumindest eine zweite Schicht (16, 26) bzw. die zweiten Schichten insgesamt eine Dicke D2 mit 0 mm < D2 < 50 mm aufweist.5. Body according to at least one of the preceding claims, characterized in that the at least one second layer (16, 26) or the second layers has a total thickness D 2 with 0 mm <D 2 <50 mm.
6. Körper nach zumindest einem der vorhergehenden Ansprüche, dadurch gekennzeichnet, dass die Fasern (28, 30) der ersten Schicht (14, 24) radial umlaufend und/oder sich kreuzend auf dem Grundkörper (12, 22) abgelegt sind.6. Body according to at least one of the preceding claims, characterized in that the fibers (28, 30) of the first layer (14, 24) are radially circumferentially and / or intersecting on the base body (12, 22) are stored.
7. Körper nach zumindest einem der vorhergehenden Ansprüche, dadurch gekennzeichnet, dass die Fasern der zumindest einen zweiten Schicht (16, 26) in Bezug auf den Grundkörper (12, 22) radial umlaufend und/oder sich kreuzend auf der ersten Schicht angeordnet sind.7. Body according to at least one of the preceding claims, characterized in that the fibers of the at least one second layer (16, 26) with respect to the base body (12, 22) are arranged radially encircling and / or crossing on the first layer.
8. Körper nach zumindest einem der vorhergehenden Ansprüche, dadurch gekennzeichnet, dass der Grundkörper (12, 22) aus martensitischem Stahl besteht.8. Body according to at least one of the preceding claims, characterized in that the base body (12, 22) consists of martensitic steel.
9. Körper nach zumindest einem der vorhergehenden Ansprüche, dadurch gekennzeichnet, dass der Grundkörper (12, 22) aus hochlegierter Nickel-Basislegierung besteht.9. Body according to at least one of the preceding claims, characterized in that the base body (12, 22) consists of high-alloy nickel-based alloy.
10. Körper nach zumindest einem der vorhergehenden Ansprüche, dadurch gekennzeichnet, dass der Grundkörper (12, 22) eine Wandstärke D mit 1 mm < D < 50 mm aufweist.10. Body according to at least one of the preceding claims, characterized in that the base body (12, 22) has a wall thickness D with 1 mm <D <50 mm.
11. Druckfester fluidbeauf schlagbarer bzw. -ter Körper wie Druckrohr oder Druckbehälter bestehend aus einem Grundkörper aus Stahl und zumindest einer den Grundkörper umgebenden Schicht bestehend aus oder enthaltend Fasern, die bei einer Temperatur mit T mit T > 5000C keine oder minimale Kriechdehnung zeigen. 11. Pressure-resistant fluidbeauf beatable or -ter body such as pressure tube or pressure vessel consisting of a base made of steel and at least one surrounding the body layer consisting of or containing fibers that show no or minimal creep at a temperature with T with T> 500 0 C. ,
12. Körper nach zumindest Anspruch 11, dadurch gekennzeichnet, dass die Fasern Verstärkungsfasern sind.Body according to at least claim 11, characterized in that the fibers are reinforcing fibers.
13. Körper nach zumindest Anspruch 11 oder 12, dadurch gekennzeichnet, dass oxidische, karbidische, nitridische Fasern, C-Fasern, SiBCN-Fasern, PAN- Fasern und/oder Polyacrylnitril-Fasern die Verstärkungsfasern sind.13. Body according to at least claim 11 or 12, characterized in that oxidic, carbidic, nitridic fibers, C-fibers, SiBCN fibers, PAN fibers and / or polyacrylonitrile fibers are the reinforcing fibers.
14. Körper nach zumindest einem der vorhergehenden Ansprüche, dadurch gekennzeichnet, dass die Faserschicht bzw. Faserschichten eine Dicke D und der Behälter eine Materialdicke d mit 0,4 d < D < 0,6 d, vorzugsweise d/2 = D aufweisen. 14. Body according to at least one of the preceding claims, characterized in that the fiber layer or fiber layers have a thickness D and the container has a material thickness d with 0.4 d <D <0.6 d, preferably d / 2 = D.
EP07728989A 2006-05-10 2007-05-10 Pressure-resistant body that is supplied with fluid Withdrawn EP2015935A1 (en)

Applications Claiming Priority (3)

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DE102006022005 2006-05-10
DE102006038713A DE102006038713A1 (en) 2006-05-10 2006-08-18 Pressure-resistant fluid-loaded body
PCT/EP2007/054537 WO2007128837A1 (en) 2006-05-10 2007-05-10 Pressure-resistant body that is supplied with fluid

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US (1) US20090101658A1 (en)
EP (1) EP2015935A1 (en)
JP (1) JP5249924B2 (en)
KR (1) KR20090019823A (en)
CN (1) CN101448636B (en)
CA (1) CA2651100C (en)
DE (1) DE102006038713A1 (en)
WO (1) WO2007128837A1 (en)

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KR20090019823A (en) 2009-02-25
CN101448636B (en) 2013-02-20
CN101448636A (en) 2009-06-03
CA2651100C (en) 2014-07-08
US20090101658A1 (en) 2009-04-23
JP2009536297A (en) 2009-10-08
JP5249924B2 (en) 2013-07-31
DE102006038713A1 (en) 2007-11-29
CA2651100A1 (en) 2007-11-15
WO2007128837A1 (en) 2007-11-15

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