FR2066676A5 - - Google Patents

Info

Publication number
FR2066676A5
FR2066676A5 FR7038920A FR7038920A FR2066676A5 FR 2066676 A5 FR2066676 A5 FR 2066676A5 FR 7038920 A FR7038920 A FR 7038920A FR 7038920 A FR7038920 A FR 7038920A FR 2066676 A5 FR2066676 A5 FR 2066676A5
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
FR7038920A
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.)
Rolls Royce PLC
Original Assignee
Rolls Royce PLC
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 Rolls Royce PLC filed Critical Rolls Royce PLC
Application granted granted Critical
Publication of FR2066676A5 publication Critical patent/FR2066676A5/fr
Expired legal-status Critical Current

Links

Classifications

    • 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
    • F01D11/00—Preventing or minimising internal leakage of working-fluid, e.g. between stages
    • F01D11/005—Sealing means between non relatively rotating elements
    • F01D11/006—Sealing the gap between rotor blades or blades and rotor
    • F01D11/008—Sealing the gap between rotor blades or blades and rotor by spacer elements between the blades, e.g. independent interblade platforms
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Materials Engineering (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
FR7038920A 1969-10-28 1970-10-28 Expired FR2066676A5 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB5274769 1969-10-28

Publications (1)

Publication Number Publication Date
FR2066676A5 true FR2066676A5 (fr) 1971-08-06

Family

ID=10465132

Family Applications (1)

Application Number Title Priority Date Filing Date
FR7038920A Expired FR2066676A5 (fr) 1969-10-28 1970-10-28

Country Status (4)

Country Link
US (1) US3712757A (fr)
DE (1) DE2052965A1 (fr)
FR (1) FR2066676A5 (fr)
GB (1) GB1232506A (fr)

Families Citing this family (31)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2171151B (en) * 1985-02-20 1988-05-18 Rolls Royce Rotors for gas turbine engines
FR2639402B1 (fr) * 1988-11-23 1990-12-28 Snecma Disque ailete de rotor de turbomachine
FR2679296B1 (fr) * 1991-07-17 1993-10-15 Snecma Plate-forme separee inter-aube pour disque ailete de rotor de turbomachine.
GB9209895D0 (en) * 1992-05-07 1992-06-24 Rolls Royce Plc Rotors for gas turbine engines
US5232346A (en) * 1992-08-11 1993-08-03 General Electric Company Rotor assembly and platform spacer therefor
US5281096A (en) * 1992-09-10 1994-01-25 General Electric Company Fan assembly having lightweight platforms
GB9405473D0 (en) * 1994-03-19 1994-05-04 Rolls Royce Plc A gas turbine engine fan blade assembly
US5738490A (en) * 1996-05-20 1998-04-14 Pratt & Whitney Canada, Inc. Gas turbine engine shroud seals
US6217283B1 (en) * 1999-04-20 2001-04-17 General Electric Company Composite fan platform
FR2858351B1 (fr) * 2003-07-31 2006-01-13 Snecma Moteurs Plate-forme inter-aubes a flechissement lateral, pour un support d'aubes de turboreacteur
US8616849B2 (en) * 2009-02-18 2013-12-31 Pratt & Whitney Canada Corp. Fan blade platform
US8568102B2 (en) * 2009-02-18 2013-10-29 Pratt & Whitney Canada Corp. Fan blade anti-fretting insert
GB0910752D0 (en) * 2009-06-23 2009-08-05 Rolls Royce Plc An annulus filler for a gas turbine engine
US9200593B2 (en) * 2009-08-07 2015-12-01 Hamilton Sundstrand Corporation Energy absorbing fan blade spacer
GB0914060D0 (en) * 2009-08-12 2009-09-16 Rolls Royce Plc A rotor assembly for a gas turbine
GB0922422D0 (en) * 2009-12-23 2010-02-03 Rolls Royce Plc Annulus Filler Assembly for a Rotor of a Turbomachine
GB2478918B8 (en) * 2010-03-23 2013-06-19 Rolls Royce Plc Interstage seal
US8827651B2 (en) * 2010-11-01 2014-09-09 Rolls-Royce Plc Annulus filler
US8777576B2 (en) 2011-08-22 2014-07-15 General Electric Company Metallic fan blade platform
GB201119655D0 (en) * 2011-11-15 2011-12-28 Rolls Royce Plc Annulus filler
US9267386B2 (en) 2012-06-29 2016-02-23 United Technologies Corporation Fairing assembly
SG11201407843UA (en) 2012-08-17 2015-03-30 United Technologies Corp Contoured flowpath surface
US9650902B2 (en) * 2013-01-11 2017-05-16 United Technologies Corporation Integral fan blade wear pad and platform seal
US10082034B2 (en) * 2014-07-03 2018-09-25 United Technologies Corporation Rotor and gas turbine engine including same
US10156151B2 (en) 2014-10-23 2018-12-18 Rolls-Royce North American Technologies Inc. Composite annulus filler
FR3038653B1 (fr) * 2015-07-08 2017-08-04 Snecma Assemblage d'une plateforme rapportee d'aube de soufflante sur un disque de soufflante
US10584592B2 (en) * 2015-11-23 2020-03-10 United Technologies Corporation Platform for an airfoil having bowed sidewalls
US10458425B2 (en) * 2016-06-02 2019-10-29 General Electric Company Conical load spreader for composite bolted joint
CN105909557A (zh) * 2016-06-21 2016-08-31 中国航空工业集团公司沈阳发动机设计研究所 一种风扇转子叶片安装结构
FR3091563B1 (fr) * 2019-01-04 2023-01-20 Safran Aircraft Engines Joint d’étanchéité amélioré de plateforme inter-aubes
US11268397B2 (en) * 2020-02-07 2022-03-08 Raytheon Technologies Corporation Fan blade platform seal and method for forming same

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR877144A (fr) * 1940-11-26 1942-11-27 Messerschmitt Boelkow Blohm Capot pour moyeux d'hélice
GB566427A (en) * 1943-07-20 1944-12-29 Dehavilland Aircraft Improvements in propeller hub fairings
GB681859A (en) * 1949-12-12 1952-10-29 Dehavilland Aircraft Improvements in propeller spinners
US2780297A (en) * 1954-03-11 1957-02-05 Gen Motors Corp Spinner construction
FR1164059A (fr) * 1956-12-28 1958-10-06 Scient Et Tech Bureau Et Carénage d'hélice autodégivrant

Also Published As

Publication number Publication date
GB1232506A (fr) 1971-05-19
DE2052965A1 (de) 1971-05-13
US3712757A (en) 1973-01-23

Similar Documents

Publication Publication Date Title
AU2270770A (fr)
AU465452B2 (fr)
AU429630B2 (fr)
AU450150B2 (fr)
AU2355770A (fr)
AU442375B2 (fr)
AU470301B1 (fr)
AU427401B2 (fr)
AU442380B2 (fr)
AU410358B2 (fr)
AU470661B1 (fr)
AU442285B2 (fr)
AT308690B (fr)
AU438128B2 (fr)
AU442322B2 (fr)
AU428129B2 (fr)
AU414607B2 (fr)
AU417208B2 (fr)
AU442554B2 (fr)
AU442538B2 (fr)
AU442463B2 (fr)
AU428131B2 (fr)
AU442357B2 (fr)
AU428074B2 (fr)
CS148487B1 (fr)

Legal Events

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