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Bladed rotor with a tiered blade to hub interface 원문보기

IPC분류정보
국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판)
  • F01D-005/32
출원번호 US-0123549 (2002-04-16)
발명자 / 주소
  • Barnette, Amanda E.
  • Rootes, David
출원인 / 주소
  • United Technologies Corporation
대리인 / 주소
    Baran, Kenneth C.
인용정보 피인용 횟수 : 15  인용 특허 : 20

초록

A bladed rotor features a tiered interface between each blade40and its respective slot16in a rotor hub12.Ideally the interface is a tiered spacer58that occupies the hub slot radially inboard of the blade attachment44.The spacer ensures a tight fit to resist windmilling induced wear. The tiered chara

대표청구항

1. A bladed rotor, comprising: a rotor hub having peripheral slots, each slot having a floor and extending a length L; a plurality of blades, each blade having an attachment occupying one of the slots, each attachment having a base surface; and a tiered interface between each blade and the f

이 특허에 인용된 특허 (20)

  1. Przytulski James C. (Fairfield OH) Hemsworth Martin C. (Cincinnati OH), Apparatus for preloading an airfoil blade in a gas turbine engine.
  2. Dhuic Jean-Claude (Melun FRX), Axial and radial holding system for the rotor vane of a turbojet engine.
  3. Adde Danielle C. R. (Cesson FRX) Charbonnel Jean-Louis (Boissise le Roi FRX) Gougeon Philippe F. P. (Fontainebleau FRX) Miraucourt Gerard G. (Brie Comte Robert FRX), Axial fixing arrangement for rotor blades of a turbomachine.
  4. Tucker James W. (Forest Park OH) Peck Robert A. (Loveland OH), Blade retainer.
  5. Tucker James W. (Cincinnati OH) Bobinger Robert O. (Cincinnati OH), Device for locking turbomachinery blades.
  6. Surdi Jean M. (Melun FRX), Fan blade axial and radial retention device.
  7. James Michael Forrester, Fan blade retainer.
  8. Szpunar Stephen J. (West Chester OH), Fan blade retainer.
  9. Prentice Ian F. (Cincinnati OH) Juenger Jerome A. (Cincinnati OH), Gas turbine engine blade retainer sub-assembly.
  10. Kemsley Nicholas J. (Derby GB2) Knott David S. (Loughborough GB2) Benson Kenneth R. (Derby GB2), Gas turbine engine fan blade assembly.
  11. Knott David S. (Loughborough GB2) Paluszkiewicz Czeslaw (Loughborough GB2) Adams Martyn P. (Leicestershire GB2) Sathianathan Sivasubramaniam K. (Burton-on-Trent GB2), Gas turbine engine fan blade assembly.
  12. Partington Albert J. (Winter Park FL) Brown Wilmott G. (Winter Park FL), Platform motion restraints for freestanding turbine blades.
  13. Weisse Michael (Tolland CT) Daley David M. (Manchester CT) Smart ; Jr. Harold R. (Hebron CT), Ramped dovetail rails for rotor blade assembly.
  14. Shank Wayne C. (Tucson AZ), Rooted aerodynamic blade and elastic roll pin damper construction.
  15. Honda Keith T. (Manchester CT) Smith Stephen L. (South Windsor CT) Voyer Peter E. (Tolland CT), Rotor blade assembly.
  16. Acres Ronald C. (Hamilton OH) Gravitt Robert D. (Cincinnati OH) Roth Robert H. (Cincinnati OH), Segmented blade retainer.
  17. Gonsor Michael ; Kelley ; III Sanford E. ; Houston David P., Turbine blade damper and seal.
  18. Houston David P. ; Pelland Natalie A. ; Gonsor Michael ; Airey David, Turbine blade damper and seal.
  19. Surdi Jean M. (Rubelles FRX), Turbine engine rotor having axial or inclined, issuing blade grooves.
  20. Bucy ; Jr. Raymond W. (Terrace Park OH) Gallardo ; Jr. Vicente C. (Hamilton OH) Hollett Ronald C. (Cincinnati OH) Young Eric A. (Cincinnati OH), Turbomachinery blade retaining assembly.

이 특허를 인용한 특허 (15)

  1. Uskert, Richard Christopher; Harris, Darrell Curtis, Apparatus and method for locking a composite component.
  2. Rivers, Jonathan M.; Powers, Bronwyn, Attachment feature of a gas turbine engine blade having a curved profile.
  3. Anderson, Carney R.; Tomeo, Peter V., Axial retention system for a bladed rotor with multiple blade types.
  4. Barnett, Barry; Bonniere, Philippe, Blade fixing design for protecting against low speed rotation induced wear.
  5. Storace, Albert Frank, Decoupler system for rotor assemblies.
  6. Kurz, Leslie Charles, Fan blade positioning and support system for variable pitch, spherical tip fan blade engines.
  7. Beeck,Alexander Ralph; Irmisch,Stefan, Gas turbine blade or vane and platform element for a gas turbine blade or vane ring of a gas turbine, supporting structure for securing gas turbine blades or vanes arranged in a ring, gas turbine blade or vane ring and the use of a gas turbine blade or vane ring.
  8. Vu, Ky H.; O'Neill, Lisa P.; Fukuda, Takao; Mace, Jr., Gerald M.; Turko, Andy; Boursy, Andrew P.; Boy, Lynn M., Gas turbine engine airfoil platform edge geometry.
  9. Hubbert, Corey L.; Tomeo, Peter V.; Anderson, Carney R., Gas turbine engine nose cone attachment.
  10. Cosby, James; Hui, Kwan; Weisse, Michael A., Lightweight blade for gas turbine engine.
  11. Duelm, Shelton O.; Quinn, Christopher M.; Brown, Charles W., Low profile fan platform attachment.
  12. Maalouf, Fadi S.; Malmborg, Eric W.; Bintz, Matthew E., Split disk assembly for a gas turbine engine.
  13. Tomeo, Peter V.; Anderson, Carney R.; Ganoe, William Richard, Turbine engine rotor assembly.
  14. Piersall, Matthew Robert; Potter, Brian Denver, Turbomachine rotor assembly and method.
  15. Piersall, Matthew Robert; Potter, Brian Denver, Turbomachine rotor assembly and method.
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