IT1079515B - Supporti di palette assorbitori di urti per palette a passo variabile di turbomotori a gas - Google Patents

Supporti di palette assorbitori di urti per palette a passo variabile di turbomotori a gas

Info

Publication number
IT1079515B
IT1079515B IT23636/76A IT2363676A IT1079515B IT 1079515 B IT1079515 B IT 1079515B IT 23636/76 A IT23636/76 A IT 23636/76A IT 2363676 A IT2363676 A IT 2363676A IT 1079515 B IT1079515 B IT 1079515B
Authority
IT
Italy
Prior art keywords
pads
supports
impact absorbing
variable pitch
gas turbo
Prior art date
Application number
IT23636/76A
Other languages
English (en)
Original Assignee
Gen Electric
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 Gen Electric filed Critical Gen Electric
Application granted granted Critical
Publication of IT1079515B publication Critical patent/IT1079515B/it

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04D—NON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00—Details, component parts, or accessories
    • F04D29/26—Rotors specially for elastic fluids
    • F04D29/32—Rotors specially for elastic fluids for axial flow pumps
    • F04D29/321—Rotors specially for elastic fluids for axial flow pumps for axial flow compressors
    • F04D29/322—Blade mountings
    • F04D29/323—Blade mountings adjustable
    • 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
    • F01D5/30—Fixing blades to rotors; Blade roots ; Blade spacers
    • F01D5/3007—Fixing blades to rotors; Blade roots ; Blade spacers of axial insertion type
    • 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
    • F01D5/30—Fixing blades to rotors; Blade roots ; Blade spacers
    • F01D5/3053—Fixing blades to rotors; Blade roots ; Blade spacers by means of pins
    • 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
    • F01D7/00—Rotors with blades adjustable in operation; Control thereof
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K3/00—Plants including a gas turbine driving a compressor or a ducted fan
    • F02K3/02—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber
    • F02K3/04—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber the plant including ducted fans, i.e. fans with high volume, low pressure outputs, for augmenting the jet thrust, e.g. of double-flow type
    • F02K3/06—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber the plant including ducted fans, i.e. fans with high volume, low pressure outputs, for augmenting the jet thrust, e.g. of double-flow type with front fan
    • 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
    • F05D2260/00—Function
    • F05D2260/30—Retaining components in desired mutual position
    • F05D2260/36—Retaining components in desired mutual position by a form fit connection, e.g. by interlocking
    • 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
    • F05D2260/00—Function
    • F05D2260/40—Transmission of power
    • F05D2260/403—Transmission of power through the shape of the drive components
    • F05D2260/4031—Transmission of power through the shape of the drive components as in toothed gearing
    • 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
    • F05D2260/00—Function
    • F05D2260/70—Adjusting of angle of incidence or attack of rotating blades
    • F05D2260/74—Adjusting of angle of incidence or attack of rotating blades by turning around an axis perpendicular the rotor centre line
    • 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
    • F05D2260/00—Function
    • F05D2260/70—Adjusting of angle of incidence or attack of rotating blades
    • F05D2260/79—Bearing, support or actuation arrangements therefor
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
IT23636/76A 1975-05-29 1976-05-26 Supporti di palette assorbitori di urti per palette a passo variabile di turbomotori a gas IT1079515B (it)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US05/581,751 US4047840A (en) 1975-05-29 1975-05-29 Impact absorbing blade mounts for variable pitch blades

Publications (1)

Publication Number Publication Date
IT1079515B true IT1079515B (it) 1985-05-13

Family

ID=24326427

Family Applications (1)

Application Number Title Priority Date Filing Date
IT23636/76A IT1079515B (it) 1975-05-29 1976-05-26 Supporti di palette assorbitori di urti per palette a passo variabile di turbomotori a gas

Country Status (6)

Country Link
US (1) US4047840A (it)
JP (1) JPS51146092A (it)
CA (1) CA1045981A (it)
DE (1) DE2622545A1 (it)
FR (1) FR2312673A1 (it)
IT (1) IT1079515B (it)

Families Citing this family (39)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4343593A (en) * 1980-01-25 1982-08-10 The United States Of America As Represented By The Secretary Of The Air Force Composite blade for turbofan engine fan
DE3718678A1 (de) * 1987-06-04 1988-12-22 Mtu Muenchen Gmbh Fasertechnische verdichterschaufel
DE3818466C1 (it) * 1988-05-31 1989-12-21 Mtu Muenchen Gmbh
US5102302A (en) * 1988-06-02 1992-04-07 General Electric Company Fan blade mount
US5165856A (en) * 1988-06-02 1992-11-24 General Electric Company Fan blade mount
US5022825A (en) * 1988-10-07 1991-06-11 United Technologies Corporation Pitch retention member
US5102300A (en) * 1988-10-07 1992-04-07 United Technologies Corporation Pinned airfoil propeller assembly
US5022824A (en) * 1988-10-07 1991-06-11 United Technologies Corporation Pinned airfoil propeller blade
US5205714A (en) * 1990-07-30 1993-04-27 General Electric Company Aircraft fan blade damping apparatus
US5259728A (en) * 1992-05-08 1993-11-09 General Electric Company Bladed disk assembly
US5310317A (en) * 1992-08-11 1994-05-10 General Electric Company Quadra-tang dovetail blade
US5443365A (en) * 1993-12-02 1995-08-22 General Electric Company Fan blade for blade-out protection
US6364613B1 (en) 2000-08-15 2002-04-02 General Electric Company Hollow finger dovetail pin and method of bucket attachment using the same
FR2933955B1 (fr) * 2008-07-18 2010-09-03 Snecma Dispositif d'attache d'une pale a calage variable
EP2322763A1 (de) * 2009-11-17 2011-05-18 Siemens Aktiengesellschaft Turbinen- oder Verdichterschaufel
FR2970943B1 (fr) 2011-01-31 2014-02-28 Eurocopter France Pale et procede de fabrication de ladite pale
US10315760B2 (en) 2014-03-18 2019-06-11 Joby Aero, Inc. Articulated electric propulsion system with fully stowing blades and lightweight vertical take-off and landing aircraft using same
JP6632542B2 (ja) * 2014-03-18 2020-01-22 ジョビー エイビエイション インクＪｏｂｙ Ａｖｉａｔｉｏｎ， Ｉｎｃ． 旋回する回転翼及び収容される回転翼羽根を有する空気力学的に効率の良い軽量の垂直離着陸航空機
CN112061389A (zh) * 2014-03-18 2020-12-11 杰欧比飞行有限公司 具有枢转旋翼和收拢旋翼桨叶的气动高效的轻型垂直起飞和着陆飞机
GB201514139D0 (en) 2015-08-11 2015-09-23 Rolls Royce Plc A datum feature for a composite component
DE102016215807A1 (de) * 2016-08-23 2018-03-01 MTU Aero Engines AG Innenring für einen Leitschaufelkranz einer Strömungsmaschine
US11073160B2 (en) 2016-09-08 2021-07-27 The United States Of America As Represented By The Secretary Of The Army Adaptable articulating axial-flow compressor/turbine rotor blade
DE102017109952A1 (de) * 2017-05-09 2018-11-15 Rolls-Royce Deutschland Ltd & Co Kg Rotorvorrichtung einer Strömungsmaschine
JP7093467B2 (ja) 2018-05-10 2022-06-29 ジョビー エアロ，インコーポレイテッド 電気チルトロータ航空機
EP3802322A4 (en) 2018-05-31 2022-02-23 Joby Aero, Inc. POWER SYSTEM ARCHITECTURE AND FAULT TOLERANT VTOL AIRPLANE WITH IT
US12006048B2 (en) 2018-05-31 2024-06-11 Joby Aero, Inc. Electric power system architecture and fault tolerant VTOL aircraft using same
DE102018210601A1 (de) * 2018-06-28 2020-01-02 MTU Aero Engines AG Segmentring zur montage in einer strömungsmaschine
US10710741B2 (en) 2018-07-02 2020-07-14 Joby Aero, Inc. System and method for airspeed determination
US11021972B2 (en) * 2018-08-14 2021-06-01 Rolls-Royce North American Technologies Inc. Variable pitch blade holder for gas turbine engine
US11323214B2 (en) 2018-09-17 2022-05-03 Joby Aero, Inc. Aircraft control system
AU2019433213A1 (en) 2018-12-07 2021-07-22 Joby Aero, Inc. Aircraft control system and method
JP7401545B2 (ja) 2018-12-07 2023-12-19 ジョビー エアロ インク 回転翼とその設計方法
US10845823B2 (en) 2018-12-19 2020-11-24 Joby Aero, Inc. Vehicle navigation system
WO2020219747A2 (en) 2019-04-23 2020-10-29 Joby Aero, Inc. Battery thermal management system and method
US11230384B2 (en) 2019-04-23 2022-01-25 Joby Aero, Inc. Vehicle cabin thermal management system and method
EP3959127A4 (en) 2019-04-25 2023-01-11 Joby Aero, Inc. VTOL AIRCRAFT
US11073030B1 (en) * 2020-05-21 2021-07-27 Raytheon Technologies Corporation Airfoil attachment for gas turbine engines
FR3114347B1 (fr) 2020-09-24 2022-08-12 Safran Aircraft Engines Aube de soufflante comprenant un système anti-pivotement amélioré
FR3138836B1 (fr) 2022-08-11 2024-08-02 Safran Aircraft Engines Ensemble comportant un anneau et un manchon de support pivotant de pied d’aubes a calage variable, turbomachine equipee d’un tel ensemble et procede de demontage d’un tel ensemble

Family Cites Families (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CA483633A (en) * 1952-05-27 Mactavish Ogston Walter Bladed bodies
GB750397A (en) * 1951-12-10 1956-06-13 Power Jets Res & Dev Ltd Damped turbine and dynamic compressor blades
GB740757A (en) * 1952-10-27 1955-11-16 Power Jets Res & Dev Ltd Blades for compressors, turbines and like fluid flow machines
US2997274A (en) * 1953-04-13 1961-08-22 Morgan P Hanson Turbo-machine blade vibration damper
NL123379C (it) * 1963-11-01
US3487879A (en) * 1967-08-02 1970-01-06 Dowty Rotol Ltd Blades,suitable for propellers,compressors,fans and the like
US3689177A (en) * 1971-04-19 1972-09-05 Gen Electric Blade constraining structure
GB1430596A (en) * 1972-07-06 1976-03-31 Rolls Royce Multi-bladed fans
US3870434A (en) * 1973-12-21 1975-03-11 Gen Electric Gear arrangement for variable pitch fan
US3900274A (en) * 1974-06-25 1975-08-19 Gen Electric Remote controlled actuation system for the rotor of a gas turbine engine

Also Published As

Publication number Publication date
FR2312673B3 (it) 1979-02-16
US4047840A (en) 1977-09-13
JPS51146092A (en) 1976-12-15
FR2312673A1 (fr) 1976-12-24
DE2622545A1 (de) 1976-12-16
CA1045981A (en) 1979-01-09

Similar Documents

Publication Publication Date Title
IT1079515B (it) Supporti di palette assorbitori di urti per palette a passo variabile di turbomotori a gas
IT1031364B (it) Smorzatori di vibrazione per le piattaforme delle palette di tur bomotori
IT1042705B (it) Smorzatore di schermo per palette di turbomotori a gas
IT1073329B (it) Ugello di scarico a spinta orientabile particolarmente per turbomotori a gas
GB1551860A (en) Gas turbine engines
JPS521223A (en) Divided fan gas turbine engine
SE415385B (sv) Gasturbinmotor
IT1088661B (it) Dispositivo di contenimento delle palette rotanti di un turbomotore a gas
GB1546956A (en) Variable cycle gas turbine engines
JPS521222A (en) Variable cycle gas turbine engine
IT1068895B (it) Apparato motore a turbina a gas per aeromobili
GB1503457A (en) Gas turbine engines
IT1074030B (it) Disposizione di combistore per turbina a gas
IT1059999B (it) Ugello manovabile in volo per turbomotori a gas
IT1064440B (it) Camere di combustione per motori a turbina a gas
SE7513787L (sv) Skiljevegg for raketmotorer
IT1034384B (it) Ammortizzatore palare per turbina
FR2334826A1 (fr) Turbine a gaz
AT353170B (de) Zweimassen-ruettelvorrichtung
IT1067076B (it) Metodo di rivestimento in foglio specialmente per palette di turbomotori a gas
IT1140798B (it) Iniettore radiale fungente da dispositivo per aspirare gas
FR2329512A1 (fr) Perfectionnement aux carenages de moteurs a turbine a gaz
JPS5211315A (en) Gas turbine engine exhaust device
IT1094092B (it) Disco palettato per motore a turbina a gas
IT1058520B (it) Apparecchio per il raffreddamento di un motore a turbina a gas