IT8220186A0 - Complesso di stampo per pale della ventola di un motore a turbina agas. - Google Patents

Complesso di stampo per pale della ventola di un motore a turbina agas.

Info

Publication number
IT8220186A0
IT8220186A0 IT8220186A IT2018682A IT8220186A0 IT 8220186 A0 IT8220186 A0 IT 8220186A0 IT 8220186 A IT8220186 A IT 8220186A IT 2018682 A IT2018682 A IT 2018682A IT 8220186 A0 IT8220186 A0 IT 8220186A0
Authority
IT
Italy
Prior art keywords
turbine engine
fan blade
mold assembly
engine fan
blade mold
Prior art date
Application number
IT8220186A
Other languages
English (en)
Other versions
IT1150327B (it
Inventor
John Richard Legge
Original Assignee
United Technologies Corp
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 United Technologies Corp filed Critical United Technologies Corp
Publication of IT8220186A0 publication Critical patent/IT8220186A0/it
Application granted granted Critical
Publication of IT1150327B publication Critical patent/IT1150327B/it

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B21—MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
    • B21D—WORKING OR PROCESSING OF SHEET METAL OR METAL TUBES, RODS OR PROFILES WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
    • B21D22/00—Shaping without cutting, by stamping, spinning, or deep-drawing
    • B21D22/10—Stamping using yieldable or resilient pads
    • B21D22/12—Stamping using yieldable or resilient pads using enclosed flexible chambers
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B21—MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
    • B21D—WORKING OR PROCESSING OF SHEET METAL OR METAL TUBES, RODS OR PROFILES WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
    • B21D53/00—Making other particular articles
    • B21D53/78—Making other particular articles propeller blades; turbine blades
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B30—PRESSES
    • B30B—PRESSES IN GENERAL
    • B30B5/00—Presses characterised by the use of pressing means other than those mentioned in the preceding groups
    • B30B5/02—Presses characterised by the use of pressing means other than those mentioned in the preceding groups wherein the pressing means is in the form of a flexible element, e.g. diaphragm, urged by fluid pressure
    • 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
    • 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
    • Y10T29/49805—Shaping by direct application of fluent pressure

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Pressure Welding/Diffusion-Bonding (AREA)
  • Moulds For Moulding Plastics Or The Like (AREA)
  • Forging (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Shaping Metal By Deep-Drawing, Or The Like (AREA)
  • Blow-Moulding Or Thermoforming Of Plastics Or The Like (AREA)
IT20186/82A 1981-03-16 1982-03-16 Complesso di stampo per pale della ventola di un motore a turbina a gas IT1150327B (it)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US06/243,688 US4383426A (en) 1981-03-16 1981-03-16 Die construction for fan blades

Publications (2)

Publication Number Publication Date
IT8220186A0 true IT8220186A0 (it) 1982-03-16
IT1150327B IT1150327B (it) 1986-12-10

Family

ID=22919725

Family Applications (1)

Application Number Title Priority Date Filing Date
IT20186/82A IT1150327B (it) 1981-03-16 1982-03-16 Complesso di stampo per pale della ventola di un motore a turbina a gas

Country Status (10)

Country Link
US (1) US4383426A (it)
JP (1) JPS57160539A (it)
CA (1) CA1178129A (it)
DE (1) DE3208303A1 (it)
FR (1) FR2501544B1 (it)
GB (1) GB2094691B (it)
IL (1) IL65173A (it)
IT (1) IT1150327B (it)
NL (1) NL8200948A (it)
SE (1) SE441985B (it)

Families Citing this family (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4595444A (en) * 1983-11-14 1986-06-17 United Technologies Corporation Isostatic die and method for assembly of skeletal structures
US4811584A (en) * 1985-06-03 1989-03-14 Brimm Daniel J Thermal processing methods
FI74239C (fi) * 1985-08-14 1988-01-11 Artlog Oy Foerfarande foer framstaellning av kroekta laminatytor genom limning.
US4855011A (en) * 1986-12-12 1989-08-08 United Technologies Corporation Isostatic self-contained bond or mold tool
US5046245A (en) * 1987-03-26 1991-09-10 General Signal Corporation Methods of fabricating impeller blades for mixing apparatus
US5694683A (en) * 1993-04-20 1997-12-09 Chromalloy Gas Turbine Corporation Hot forming process
US5429877A (en) * 1993-10-20 1995-07-04 The United States Of America As Represented By The Secretary Of The Air Force Internally reinforced hollow titanium alloy components
GB0001753D0 (en) * 2000-01-27 2000-03-15 Sermatech Repair Services Limi Thermal processing apparatus and method
JP4028442B2 (ja) 2002-06-26 2007-12-26 株式会社東芝 ガスタービン翼の変形修正装置及び方法
US8127442B2 (en) * 2005-12-15 2012-03-06 United Technologies Corporation Compressor blade flow form technique for repair
GB0719873D0 (en) 2007-10-12 2007-11-21 Rolls Royce Plc Shape correcting components
ES2954914T3 (es) * 2016-07-08 2023-11-27 Quintus Technologies Ab Proceso y sistema para el conformado a presión de una pieza de trabajo
CN109530495A (zh) * 2018-12-29 2019-03-29 无锡市振华亿美嘉科技有限公司 锁支撑口部整形模具

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR1543936A (fr) * 1966-12-30 1968-10-31 Parsons Corp Outillages gonflables, notamment pour appliquer des pressions dans des opérations d'encollage
US3736638A (en) * 1971-04-07 1973-06-05 United Aircraft Corp Method for bonding opposed parts of a hollow article together
US3701190A (en) * 1971-04-07 1972-10-31 United Aircraft Corp Apparatus for and the method of compacting an irregularly shaped article
JPS5615971B2 (it) * 1974-01-29 1981-04-14
US4087037A (en) * 1976-07-09 1978-05-02 Mcdonnell Douglas Corporation Method of and tools for producing superplastically formed and diffusion bonded structures
US4188811A (en) * 1978-07-26 1980-02-19 Chem-Tronics, Inc. Metal forming methods
US4301584A (en) * 1980-01-31 1981-11-24 United Technologies Corporation Method of forming fiber and metal matrix composite

Also Published As

Publication number Publication date
DE3208303A1 (de) 1982-11-04
IT1150327B (it) 1986-12-10
SE441985B (sv) 1985-11-25
SE8201564L (sv) 1982-09-17
US4383426A (en) 1983-05-17
GB2094691A (en) 1982-09-22
GB2094691B (en) 1984-07-18
FR2501544B1 (fr) 1987-06-19
IL65173A0 (en) 1982-05-31
JPS57160539A (en) 1982-10-02
IL65173A (en) 1985-04-30
NL8200948A (nl) 1982-10-18
CA1178129A (en) 1984-11-20
FR2501544A1 (fr) 1982-09-17

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