FR1577388A - - Google Patents

Info

Publication number
FR1577388A
FR1577388A FR1577388DA FR1577388A FR 1577388 A FR1577388 A FR 1577388A FR 1577388D A FR1577388D A FR 1577388DA FR 1577388 A FR1577388 A FR 1577388A
Authority
FR
France
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
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 filed Critical
Application granted granted Critical
Publication of FR1577388A publication Critical patent/FR1577388A/fr
Expired legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29D—PRODUCING PARTICULAR ARTICLES FROM PLASTICS OR FROM SUBSTANCES IN A PLASTIC STATE
    • B29D99/00—Subject matter not provided for in other groups of this subclass
    • B29D99/0025—Producing blades or the like, e.g. blades for turbines, propellers, or wings
    • 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
    • B32B3/00—Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shape; Layered products comprising a layer having particular features of form
    • B32B3/10—Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shape; Layered products comprising a layer having particular features of form characterised by a discontinuous layer, i.e. formed of separate pieces of material
    • B32B3/12—Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shape; Layered products comprising a layer having particular features of form characterised by a discontinuous layer, i.e. formed of separate pieces of material characterised by a layer of regularly- arranged cells, e.g. a honeycomb structure
    • 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
    • F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/12—Blades
    • F01D5/14—Form or construction
    • F01D5/147—Construction, i.e. structural features, e.g. of weight-saving hollow blades
    • 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
    • F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/12—Blades
    • F01D5/28—Selecting particular materials; Particular measures relating thereto; Measures against erosion or corrosion
    • 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
    • F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/12—Blades
    • F01D5/28—Selecting particular materials; Particular measures relating thereto; Measures against erosion or corrosion
    • F01D5/282—Selecting composite materials, e.g. blades with reinforcing filaments
    • 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
    • F05D2240/00—Components
    • F05D2240/80—Platforms for stationary or moving blades
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/60—Efficient propulsion technologies, e.g. for aircraft
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00—Metal working
    • Y10T29/49—Method of mechanical manufacture
    • Y10T29/49316—Impeller making
    • Y10T29/49336—Blade making
    • Y10T29/49337—Composite blade
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00—Stock material or miscellaneous articles
    • Y10T428/24—Structurally defined web or sheet [e.g., overall dimension, etc.]
    • Y10T428/24149—Honeycomb-like

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Materials Engineering (AREA)
  • Architecture (AREA)
  • Composite Materials (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
FR1577388D 1967-05-05 1968-04-18 Expired FR1577388A (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB21077/67A GB1130285A (en) 1967-05-05 1967-05-05 Method of making an aerofoil shaped blade for a fluid flow machine

Publications (1)

Publication Number Publication Date
FR1577388A true FR1577388A (fr) 1969-08-08

Family

ID=10156825

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1577388D Expired FR1577388A (fr) 1967-05-05 1968-04-18

Country Status (4)

Country Link
US (1) US3566493A (fr)
DE (1) DE1752234A1 (fr)
FR (1) FR1577388A (fr)
GB (1) GB1130285A (fr)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2688264A1 (fr) * 1992-03-04 1993-09-10 Snecma Redresseur de turbomachine a aubes ayant une face alveolee chargee en materiau composite.
US5253419A (en) * 1991-02-20 1993-10-19 Societe Nationale D'etude Et De Construction De Moteurs D'aviation "S.N.E.C.M.A." Method of manufacturing a hollow blade for a turboshaft engine
FR2695163A1 (fr) * 1992-09-02 1994-03-04 Snecma Aube creuse pour turbomachine et son procédé de fabrication.
FR2794167A1 (fr) 1999-05-28 2000-12-01 Snecma Aube creuse pour turbomachine et son procede de fabrication

Families Citing this family (33)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3848483A (en) * 1972-07-17 1974-11-19 Wall Machine Works Method of making router bits
US3813186A (en) * 1972-10-10 1974-05-28 Textron Inc Rotor blade shear reinforcement
US4032089A (en) * 1975-04-16 1977-06-28 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Surface finishing
DE2558882C3 (de) * 1975-12-27 1979-10-11 Walter 5300 Bonn Schoenball Aufbau eines Rotors, insbesondere für Windkraftmaschinen
US4136846A (en) * 1976-12-20 1979-01-30 Boeing Commercial Airplane Company Composite structure
US4118147A (en) * 1976-12-22 1978-10-03 General Electric Company Composite reinforcement of metallic airfoils
US4284443A (en) * 1979-02-05 1981-08-18 The Boeing Company Single stage hot bonding method for producing composite honeycomb core structures
US4326836A (en) * 1979-12-13 1982-04-27 United Technologies Corporation Shroud for a rotor blade
US4336090A (en) * 1980-06-30 1982-06-22 The Boeing Company Method of making sandwich panel
US4346134A (en) * 1980-06-30 1982-08-24 The Boeing Company Honeycomb core assembly including a sacrificial core portion
US4604780A (en) * 1983-02-03 1986-08-12 Solar Turbines Incorporated Method of fabricating a component having internal cooling passages
FR2569783B1 (fr) * 1984-09-06 1986-09-12 Snecma Structure d'anneau et dispositif de decharge de compresseur comportant cet anneau
US5056738A (en) * 1989-09-07 1991-10-15 General Electric Company Damper assembly for a strut in a jet propulsion engine
JP2808500B2 (ja) * 1991-08-23 1998-10-08 三菱重工業株式会社 ガスタービンの中空ファン動翼
US5344235A (en) * 1993-01-21 1994-09-06 General Signal Corp. Erosion resistant mixing impeller
DE19542080C1 (de) * 1995-11-11 1997-01-30 Mtu Muenchen Gmbh Schaufelblatt für Turbotriebwerke zur Herstellung von Laufrädern mit integralen Hohlschaufeln
FR2755055B1 (fr) * 1996-10-31 1999-08-13 Brigantine Sa Nid d'abeilles a absorption variable
DE19956444B4 (de) * 1999-11-24 2004-08-26 Mtu Aero Engines Gmbh Verfahren zur Herstellung eines Leichtbauteils in Verbundbauweise
EP1186748A1 (fr) * 2000-09-05 2002-03-13 Siemens Aktiengesellschaft Aube de rotor pour une turbomachine et turbomachine
GB2398029B (en) * 2003-02-04 2005-05-18 Rolls Royce Plc Production of disc components
DE10307610A1 (de) * 2003-02-22 2004-09-02 Rolls-Royce Deutschland Ltd & Co Kg Verdichterschaufel für ein Flugzeugtriebwerk
GB0601220D0 (en) 2006-01-21 2006-03-01 Rolls Royce Plc Aerofoils for gas turbine engines
GB2438185A (en) 2006-05-17 2007-11-21 Rolls Royce Plc An apparatus for preventing ice accretion
WO2009057532A1 (fr) * 2007-10-31 2009-05-07 Mitsubishi Heavy Industries, Ltd. Aube fixe et turbine à vapeur
DE102008011427B4 (de) * 2008-02-27 2023-08-03 MTU Aero Engines AG Verfahren zur Herstellung und Anwendung einer Schutzschicht
DE102008058786A1 (de) * 2008-11-24 2010-05-27 Rolls-Royce Deutschland Ltd & Co Kg Hybrides Bauteil für ein Gasturbinentriebwerk
US8814527B2 (en) * 2009-08-07 2014-08-26 Hamilton Sundstrand Corporation Titanium sheath and airfoil assembly
DE102010038408B4 (de) * 2010-07-26 2020-11-19 Airbus Operations Gmbh Strukturelement für ein Luft- und Raumfahrzeug und Verfahren zum Herstellen eines derartigen Strukturelementes
PL2663445T5 (pl) * 2011-01-12 2019-12-31 Abc Group Inc. Formowany z rozdmuchiwaniem pusty w środku wyrób z elementami strukturalnymi w postaci słupków oraz proces formowania z rozdmuchiwaniem
CN103786003B (zh) * 2014-01-15 2016-04-06 西安航空动力股份有限公司 一种航空发动机导向叶片缘板的加工方法
CN104690572B (zh) * 2015-03-17 2017-02-01 四川明日宇航工业有限责任公司 弱刚性航空结构件小应力填充吸震装夹加工法
DE102018202685A1 (de) * 2018-02-22 2019-08-22 Siemens Aktiengesellschaft Bauteil sowie Verfahren zum Herstellen eines Bauteils mittels additiven Fertigungsverfahren
US11168572B2 (en) * 2019-02-05 2021-11-09 Raytheon Technologies Corporation Composite gas turbine engine component

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5253419A (en) * 1991-02-20 1993-10-19 Societe Nationale D'etude Et De Construction De Moteurs D'aviation "S.N.E.C.M.A." Method of manufacturing a hollow blade for a turboshaft engine
FR2688264A1 (fr) * 1992-03-04 1993-09-10 Snecma Redresseur de turbomachine a aubes ayant une face alveolee chargee en materiau composite.
US5295789A (en) * 1992-03-04 1994-03-22 Societe Nationale D'etude Et De Construction De Moteurs D'aviation "Snecma" Turbomachine flow-straightener blade
FR2695163A1 (fr) * 1992-09-02 1994-03-04 Snecma Aube creuse pour turbomachine et son procédé de fabrication.
US5407326A (en) * 1992-09-02 1995-04-18 Societe Nationale D'etude Et De Construction De Moteurs D'aviation "S.N.E.C.M.A." Hollow blade for a turbomachine
FR2794167A1 (fr) 1999-05-28 2000-12-01 Snecma Aube creuse pour turbomachine et son procede de fabrication

Also Published As

Publication number Publication date
US3566493A (en) 1971-03-02
DE1752234A1 (de) 1971-08-05
GB1130285A (en) 1968-10-16

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Legal Events

Date Code Title Description
TP Transmission of property
TP Transmission of property
TP Transmission of property
ST Notification of lapse