US20010028848A1 - Turbine rotor disk fitted with blades having christmastree-shaped roots, and a method of mounting a blade on a disk - Google Patents
Turbine rotor disk fitted with blades having christmastree-shaped roots, and a method of mounting a blade on a disk Download PDFInfo
- Publication number
- US20010028848A1 US20010028848A1 US09/774,605 US77460501A US2001028848A1 US 20010028848 A1 US20010028848 A1 US 20010028848A1 US 77460501 A US77460501 A US 77460501A US 2001028848 A1 US2001028848 A1 US 2001028848A1
- Authority
- US
- United States
- Prior art keywords
- blade
- disk
- root
- slot
- stick
- Prior art date
- 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.)
- Granted
Links
- 238000000034 method Methods 0.000 title claims description 7
- 230000000295 complement effect Effects 0.000 claims abstract description 5
- 239000012634 fragment Substances 0.000 description 2
- 241000191291 Abies alba Species 0.000 description 1
- 238000002955 isolation Methods 0.000 description 1
Images
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
- 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
- F01D5/32—Locking, e.g. by final locking blades or keys
- F01D5/323—Locking of axial insertion type blades by means of a key or the like parallel to the axis of the rotor
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01N—INVESTIGATING OR ANALYSING MATERIALS BY DETERMINING THEIR CHEMICAL OR PHYSICAL PROPERTIES
- G01N33/00—Investigating or analysing materials by specific methods not covered by groups G01N1/00 - G01N31/00
- G01N33/22—Fuels; Explosives
- G01N33/225—Gaseous fuels, e.g. natural gas
-
- 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
- Y10T29/4932—Turbomachine making
- Y10T29/49321—Assembling individual fluid flow interacting members, e.g., blades, vanes, buckets, on rotary support member
Definitions
- the present invention relates to a turbine rotor disk fitted with blades having Christmastree-shaped roots.
- the invention relates to means enabling blades having Christmastree-shaped roots to be properly secured to the disk on which they are mounted, even at slow speeds of rotation.
- Each spring is constituted by a single curved strip placed in a setback: the ends of the strip are in the setback and the curved portion is directed outwardly, i.e. against the bottom of the corresponding slot in the rotor disk.
- the depth of the setback is smaller than the deflection in the middle of the curved spring.
- An object of the present invention is to provide a turbine rotor disk fitted with blades having Christmastree-shaped roots, where the teeth of the blade roots are pressed against the complementary grooves formed in the slots of the disk by springs while avoiding the above-mentioned drawbacks of the prior art during assembly.
- the invention thus provides a turbine rotor disk fitted with blades having Christmastree-shaped roots, said disk having complementary slots each receiving the root of a blade, wherein at least one stick having a setback holding a spring strip captive is placed in the bottom of each slot of the disk between said bottom and the end face of the root of the corresponding blade.
- three of said sticks are disposed between the bottom of a slot in the disk and the end face of the root of the corresponding blade.
- the end of the root of each blade has a rim against which one of said sticks comes into abutment.
- the invention also provides a method of assembling a blade having a Christmastree-shaped root to a turbine rotor disk of the invention, the method comprising the following sequence of operations:
- FIG. 1 is a fragmentary view of a steam turbine rotor disk of the invention seen looking along arrow I of FIG. 2;
- FIG. 2 is a section view on II-II of FIG. 1;
- FIG. 3 is an enlargement of fragment III of FIG. 2;
- FIGS. 4 and 5 are respectively a plan view and a section view on V-V of FIG. 4 showing a stick used for mounting a blade on the rotor disk;
- FIG. 6 is a fragmentary diagrammatic view of a turbine rotor in which there can be seen a disk with a blade in position to be assembled;
- FIG. 7 shows a fragment of the disk with a slot in the low position
- FIG. 8 is a view looking along arrow VIII of FIG. 7;
- FIG. 9 shows a blade in position to be assembled in the rotor disk slot shown in FIGS. 7 and 8;
- FIG. 10 shows the FIG. 9 blade seen along arrow X;
- FIGS. 11 and 12 are similar to FIGS. 7 and 8 but after a blade has been installed;
- FIG. 13 is an enlargement of a detail XIII of FIG. 11;
- FIG. 14 is an enlargement of a detail XIV of FIG. 11.
- FIG. 15 shows a tool used for inserting sticks in their locations.
- FIGS. 1 to 3 With reference to FIGS. 1 to 3 , there can be seen a small part of a steam turbine rotor disk 1 having a blade 2 mounted thereon.
- the blade has a root which is said to be “Christmastree-shaped”. This is the base 3 of the blade whose general shape when seen in section perpendicular to the axis Y of the rotor disk resembles a Christmas tree. This Christmastree-shaped root 3 serves to secure the blade 2 relative to the disk 1 .
- the root 3 is inserted in a corresponding slot 4 of the disk 1 .
- a stick 5 is placed between the bottom of the slot 4 and the end of the root 3 of the blade 2 .
- three of these sticks are inserted one after another: they are referenced in FIG. 1.
- Each stick is fitted with a spring strip (not shown in FIGS. 1 to 3 ), but visible in the stick shown on its own in FIGS. 4 and 5.
- the stick 5 has a setback 6 in which a spring strip 7 is placed and held captive.
- FIGS. 11 and 12 the blade 2 can be seen mounted on the disk 1 .
- FIG. 11 corresponds to FIG. 1 after the disk has turned so as to place the blade 2 pointing downwards
- FIG. 12 is a view seen along arrow XII of FIG. 11.
- Detail XIV of FIG. 11, shown on a larger scale in FIG. 14, shows the other face of the disk 1 where the series of blades 2 , all mounted in the same manner as explained above, is closed laterally in conventional manner by a two-part ring 9 A, 9 B made up of a plurality of segments that are subsequently bonded together.
- the empty space between the end of the root 3 and the bottom of the slot 4 in the disk 1 is of height H.
- FIG. 5 which shows the stick 5 in isolation together with its spring strip 7 (which spring is merely a curved spring strip)
- the total height of the stick plus its spring at rest is equal to G and naturally, the height G is greater than H so that the spring can perform its function of pressing the roots of the blades against the grooves in the slots of the disk.
- FIGS. 6 to 10 show how a blade 2 is mounted on the rotor disk 1 .
- the turbine and its disk 1 is placed so that its axis Y is horizontal and the root 3 of the blade 2 for mounting is inserted freely into the slot 4 situated in the bottom-most position. This is also shown in FIGS. 7 and 9.
- the blade is mounted in the disk via its steam outlet face, given that steam travels in the direction shown by arrow F.
- FIGS. 8 and 10 are views looking along arrows VIII and X of FIGS. 7 and 9 and show how the profiles of the slot 4 and of the Christmastree-shaped root 3 are curved.
- the first stick 5 is inserted in the empty space between the end of the blade root 3 and the bottom of the slot 4 using a tool 10 as shown in FIG. 15. It suffices to strike the rear end of the tool in the direction of arrow Fl with a mallet until the first stick comes to bear against the rim 8 on the blade root 3 (FIG. 13). The other two sticks are subsequently inserted in the same manner so as to come to bear against the preceding stick. Thereafter the disk is closed in conventional manner by means of the rings 9 A and 9 B (FIG. 14).
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- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Health & Medical Sciences (AREA)
- Life Sciences & Earth Sciences (AREA)
- Medicinal Chemistry (AREA)
- Physics & Mathematics (AREA)
- Oil, Petroleum & Natural Gas (AREA)
- Chemical Kinetics & Catalysis (AREA)
- General Engineering & Computer Science (AREA)
- Food Science & Technology (AREA)
- Mechanical Engineering (AREA)
- General Chemical & Material Sciences (AREA)
- Analytical Chemistry (AREA)
- Biochemistry (AREA)
- General Health & Medical Sciences (AREA)
- General Physics & Mathematics (AREA)
- Immunology (AREA)
- Pathology (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
- Toys (AREA)
Abstract
Description
- The present invention relates to a turbine rotor disk fitted with blades having Christmastree-shaped roots.
- More particularly, the invention relates to means enabling blades having Christmastree-shaped roots to be properly secured to the disk on which they are mounted, even at slow speeds of rotation.
- With this method of fixing where the root of each blade is said to be “Christmastree-shaped” and is received in a complementary slot in the rotor disk on which the blades are mounted, it is necessary for rotation to be taking place at sufficient speed before centrifugal force ensures that no relative movement is possible. The teeth on the root of the blade do not bear properly against the corresponding grooves in a slot of the disk at low speeds, and a known remedy to this drawback is to provide a few setbacks, generally three setbacks, in the end face of the root to provide housings for receiving springs.
- Each spring is constituted by a single curved strip placed in a setback: the ends of the strip are in the setback and the curved portion is directed outwardly, i.e. against the bottom of the corresponding slot in the rotor disk. Naturally, the depth of the setback is smaller than the deflection in the middle of the curved spring.
- When the blades are mounted on the disk, the springs are placed in their setbacks and the Christmastree-shaped rotor of each blade is inserted into the corresponding slot of the disk, i.e. simultaneously with its three springs. This operation is very difficult and accidents often arise such as springs breaking or jamming.
- An object of the present invention is to provide a turbine rotor disk fitted with blades having Christmastree-shaped roots, where the teeth of the blade roots are pressed against the complementary grooves formed in the slots of the disk by springs while avoiding the above-mentioned drawbacks of the prior art during assembly.
- The invention thus provides a turbine rotor disk fitted with blades having Christmastree-shaped roots, said disk having complementary slots each receiving the root of a blade, wherein at least one stick having a setback holding a spring strip captive is placed in the bottom of each slot of the disk between said bottom and the end face of the root of the corresponding blade.
- Advantageously, three of said sticks are disposed between the bottom of a slot in the disk and the end face of the root of the corresponding blade.
- According to another characteristic, the end of the root of each blade has a rim against which one of said sticks comes into abutment.
- The invention also provides a method of assembling a blade having a Christmastree-shaped root to a turbine rotor disk of the invention, the method comprising the following sequence of operations:
- a) the rotor disk is placed so that its axis is in a horizontal position;
- b) the slot of the disk in which the blade root is to be mounted is placed in the bottom position;
- c) the blade is installed by slidably inserting the root of the blade in the slot of the disk; and
- d) the stick(s) each fitted with a respective spring strip are then inserted into the empty space between the bottom of the slot in the disk and the end of the blade root until the first-inserted stick comes into abutment against said rim on the root of the blade.
- An embodiment of the invention is described below with reference to the accompanying drawings, in which:
- FIG. 1 is a fragmentary view of a steam turbine rotor disk of the invention seen looking along arrow I of FIG. 2;
- FIG. 2 is a section view on II-II of FIG. 1;
- FIG. 3 is an enlargement of fragment III of FIG. 2;
- FIGS. 4 and 5 are respectively a plan view and a section view on V-V of FIG. 4 showing a stick used for mounting a blade on the rotor disk;
- FIG. 6 is a fragmentary diagrammatic view of a turbine rotor in which there can be seen a disk with a blade in position to be assembled;
- FIG. 7 shows a fragment of the disk with a slot in the low position;
- FIG. 8 is a view looking along arrow VIII of FIG. 7;
- FIG. 9 shows a blade in position to be assembled in the rotor disk slot shown in FIGS. 7 and 8;
- FIG. 10 shows the FIG. 9 blade seen along arrow X;
- FIGS. 11 and 12 are similar to FIGS. 7 and 8 but after a blade has been installed;
- FIG. 13 is an enlargement of a detail XIII of FIG. 11;
- FIG. 14 is an enlargement of a detail XIV of FIG. 11; and
- FIG. 15 shows a tool used for inserting sticks in their locations.
- With reference to FIGS.1 to 3, there can be seen a small part of a steam
turbine rotor disk 1 having ablade 2 mounted thereon. - The blade has a root which is said to be “Christmastree-shaped”. This is the
base 3 of the blade whose general shape when seen in section perpendicular to the axis Y of the rotor disk resembles a Christmas tree. This Christmastree-shaped root 3 serves to secure theblade 2 relative to thedisk 1. Theroot 3 is inserted in acorresponding slot 4 of thedisk 1. - In the invention, and as can be seen in the detail III shown on a larger scale in FIG. 3, a
stick 5 is placed between the bottom of theslot 4 and the end of theroot 3 of theblade 2. In practice, three of these sticks are inserted one after another: they are referenced in FIG. 1. - Each stick is fitted with a spring strip (not shown in FIGS.1 to 3), but visible in the stick shown on its own in FIGS. 4 and 5. As can be seen in these figures, the
stick 5 has asetback 6 in which aspring strip 7 is placed and held captive. - In FIGS. 11 and 12, the
blade 2 can be seen mounted on thedisk 1. FIG. 11 corresponds to FIG. 1 after the disk has turned so as to place theblade 2 pointing downwards, and FIG. 12 is a view seen along arrow XII of FIG. 11. - The detail referenced XIII in FIG. 11 and shown on a larger scale in FIG. 13 shows that the end of the Christmastree-
shaped root 3 of theblade 2 has arim 8 against which thefirst stick 5 to be inserted comes into abutment. - Detail XIV of FIG. 11, shown on a larger scale in FIG. 14, shows the other face of the
disk 1 where the series ofblades 2, all mounted in the same manner as explained above, is closed laterally in conventional manner by a two-part ring - As can be seen in the detail shown in FIG. 3, the empty space between the end of the
root 3 and the bottom of theslot 4 in thedisk 1 is of height H. - In FIG. 5 which shows the
stick 5 in isolation together with its spring strip 7 (which spring is merely a curved spring strip), the total height of the stick plus its spring at rest is equal to G and naturally, the height G is greater than H so that the spring can perform its function of pressing the roots of the blades against the grooves in the slots of the disk. - As shown in FIG. 5, the ends of the
spring strip 7 are in the bottom of thesetback 6 while the curved portion in the middle is pressed against the bottom of theslot 4 in therotor disk 1 once thestick 5 has been inserted between the root of the blade and the bottom of the slot, with the plane face of thestick 5 then bearing against the end of theroot 3 of the blade (see FIGS. 3, 13, and 14). - FIGS.6 to 10 show how a
blade 2 is mounted on therotor disk 1. - As shown in FIG. 6, the turbine and its
disk 1 is placed so that its axis Y is horizontal and theroot 3 of theblade 2 for mounting is inserted freely into theslot 4 situated in the bottom-most position. This is also shown in FIGS. 7 and 9. The blade is mounted in the disk via its steam outlet face, given that steam travels in the direction shown by arrow F. - FIGS. 8 and 10 are views looking along arrows VIII and X of FIGS. 7 and 9 and show how the profiles of the
slot 4 and of the Christmastree-shaped root 3 are curved. - Given the empty space H (FIG. 3) between the bottom of the
slot 4 and the tip of theblade root 3, the root can slide freely in theslot 4 without any risk of the teeth of the Christmastree-shape jamming in the grooves of the slot, since the surface state of the teeth and of the grooves is carefully prepared. - Finally, the
first stick 5 is inserted in the empty space between the end of theblade root 3 and the bottom of theslot 4 using atool 10 as shown in FIG. 15. It suffices to strike the rear end of the tool in the direction of arrow Fl with a mallet until the first stick comes to bear against therim 8 on the blade root 3 (FIG. 13). The other two sticks are subsequently inserted in the same manner so as to come to bear against the preceding stick. Thereafter the disk is closed in conventional manner by means of therings
Claims (6)
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR0004078A FR2807096B1 (en) | 2000-03-30 | 2000-03-30 | ROTOR DISC OF TURBINE EQUIPPED WITH FINS ON FOOT AND TREE OF MOUNTING A FIN ON A DISC |
FR0004078 | 2000-03-30 |
Publications (2)
Publication Number | Publication Date |
---|---|
US20010028848A1 true US20010028848A1 (en) | 2001-10-11 |
US6447253B2 US6447253B2 (en) | 2002-09-10 |
Family
ID=8848690
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US09/774,605 Expired - Lifetime US6447253B2 (en) | 2000-03-30 | 2001-02-01 | Turbine rotor disk fitted with blades having christmastree-shaped roots, and a method of mounting a blade on a disk |
Country Status (8)
Country | Link |
---|---|
US (1) | US6447253B2 (en) |
EP (1) | EP1138879B1 (en) |
JP (1) | JP4657482B2 (en) |
AT (1) | ATE307269T1 (en) |
DE (1) | DE60114065T2 (en) |
DK (1) | DK1138879T3 (en) |
ES (1) | ES2247028T3 (en) |
FR (1) | FR2807096B1 (en) |
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2003100220A1 (en) * | 2002-05-24 | 2003-12-04 | Abb Turbo Systems Ag | Axial securing means for impeller blades |
EP1382800A2 (en) * | 2002-07-20 | 2004-01-21 | Rolls Royce Plc | A fan blade assembly |
US20140161617A1 (en) * | 2011-08-03 | 2014-06-12 | Snecma | Bladed rotor wheel for a turbine engine |
US20140199172A1 (en) * | 2013-01-11 | 2014-07-17 | General Electric Company | Turbomachine and method of handling turbomachine components |
US12018590B1 (en) | 2023-04-04 | 2024-06-25 | Ge Infrastructure Technology Llc | Method for turbine blade and assembly with dovetail arrangement for enlarged rotor groove |
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FR2841609B1 (en) * | 2002-06-27 | 2004-09-10 | Snecma Moteurs | BLOWER RETAINER LEVEL RETAINER |
US6796769B2 (en) * | 2002-10-02 | 2004-09-28 | General Electric Company | Radial retainer for single lobe turbine blade attachment and method for radially retaining a turbine blade in a turbine blade slot |
US6761538B2 (en) | 2002-10-31 | 2004-07-13 | General Electric Company | Continual radial loading device for steam turbine reaction type buckets and related method |
JP2005273646A (en) * | 2004-02-25 | 2005-10-06 | Mitsubishi Heavy Ind Ltd | Moving blade element and rotary machine having the moving blade element |
FR2918129B1 (en) | 2007-06-26 | 2009-10-30 | Snecma Sa | IMPROVEMENT TO AN INTERCALE BETWEEN A FOOT OF DAWN AND THE BACKGROUND OF THE ALVEOLE OF THE DISK IN WHICH IT IS MOUNTED |
US8485785B2 (en) | 2007-07-19 | 2013-07-16 | Siemens Energy, Inc. | Wear prevention spring for turbine blade |
US8186961B2 (en) * | 2009-01-23 | 2012-05-29 | Pratt & Whitney Canada Corp. | Blade preloading system |
US8414268B2 (en) * | 2009-11-19 | 2013-04-09 | United Technologies Corporation | Rotor with one-sided load and lock slots |
EP2386721A1 (en) * | 2010-05-14 | 2011-11-16 | Siemens Aktiengesellschaft | Fastening assembly for blades of axial fluid flow turbo machines and procedure for producing the same |
US8851854B2 (en) | 2011-12-16 | 2014-10-07 | United Technologies Corporation | Energy absorbent fan blade spacer |
US10508556B2 (en) | 2013-01-17 | 2019-12-17 | United Technologies Corporation | Rotor blade root spacer with grip element |
US9909431B2 (en) | 2013-10-18 | 2018-03-06 | Siemens Energy, Inc. | Variable dual spring blade root support for gas turbines |
US9739160B2 (en) | 2013-10-18 | 2017-08-22 | Siemens Aktiengesellschaft | Adjustable blade root spring for turbine blade fixation in turbomachinery |
GB201417417D0 (en) * | 2014-10-02 | 2014-11-19 | Rolls Royce Plc | Slider |
US10215035B2 (en) | 2014-12-29 | 2019-02-26 | Rolls-Royce North American Technologies Inc. | Turbine wheels with preloaded blade attachment |
EP3048256A1 (en) * | 2015-01-20 | 2016-07-27 | Siemens Aktiengesellschaft | Rotor comprising a turbine blade with a locking device |
GB201504182D0 (en) * | 2015-03-12 | 2015-04-29 | Rolls Royce Plc | Chocking and retaining device |
US10465537B2 (en) * | 2016-05-27 | 2019-11-05 | General Electric Company | Margin bucket dovetail radial support feature for axial entry buckets |
FR3085992B1 (en) | 2018-09-14 | 2020-12-11 | Safran Aircraft Engines | MOBILE TURBINE WHEEL BLADE WITH A CURVILINE SHAPED FOOT |
KR102355521B1 (en) | 2020-08-19 | 2022-01-24 | 두산중공업 주식회사 | Assembling structure of compressor blade and gas turbine comprising the same and assembling method of compressor blade |
KR102454379B1 (en) * | 2020-09-08 | 2022-10-14 | 두산에너빌리티 주식회사 | rotor and turbo-machine comprising the same |
US11208903B1 (en) * | 2020-11-20 | 2021-12-28 | Solar Turbines Incorporated | Stiffness coupling and vibration damping for turbine blade shroud |
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US3572970A (en) * | 1969-01-23 | 1971-03-30 | Gen Electric | Turbomachinery blade spacer |
US4022545A (en) * | 1974-09-11 | 1977-05-10 | Avco Corporation | Rooted aerodynamic blade and elastic roll pin damper construction |
US4208170A (en) * | 1978-05-18 | 1980-06-17 | General Electric Company | Blade retainer |
US4265595A (en) * | 1979-01-02 | 1981-05-05 | General Electric Company | Turbomachinery blade retaining assembly |
FR2519072B1 (en) * | 1981-12-29 | 1986-05-30 | Snecma | DEVICE FOR AXIAL AND RADIAL RETENTION OF A TURBO JET ROTOR BLADE |
US5160243A (en) * | 1991-01-15 | 1992-11-03 | General Electric Company | Turbine blade wear protection system with multilayer shim |
US5123813A (en) * | 1991-03-01 | 1992-06-23 | General Electric Company | Apparatus for preloading an airfoil blade in a gas turbine engine |
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GB9223593D0 (en) * | 1992-11-11 | 1992-12-23 | Rolls Royce Plc | Gas turbine engine fan blade assembly |
DE4300773C1 (en) * | 1993-01-14 | 1993-11-18 | Mtu Muenchen Gmbh | Axial running blade for gas turbine - has running blades with blade feet anchored in axial grooves distributed over periphery of wheel plate |
US5431543A (en) * | 1994-05-02 | 1995-07-11 | Westinghouse Elec Corp. | Turbine blade locking assembly |
US6102664A (en) * | 1995-12-14 | 2000-08-15 | The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration | Blading system and method for controlling structural vibrations |
DE19823157A1 (en) * | 1998-05-23 | 1999-11-25 | Asea Brown Boveri | Fixing device for running blades of axial-flow turbine machines |
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-
2000
- 2000-03-30 FR FR0004078A patent/FR2807096B1/en not_active Expired - Lifetime
-
2001
- 2001-01-22 ES ES01400176T patent/ES2247028T3/en not_active Expired - Lifetime
- 2001-01-22 AT AT01400176T patent/ATE307269T1/en not_active IP Right Cessation
- 2001-01-22 DE DE60114065T patent/DE60114065T2/en not_active Expired - Lifetime
- 2001-01-22 DK DK01400176T patent/DK1138879T3/en active
- 2001-01-22 EP EP01400176A patent/EP1138879B1/en not_active Expired - Lifetime
- 2001-02-01 US US09/774,605 patent/US6447253B2/en not_active Expired - Lifetime
- 2001-03-29 JP JP2001096177A patent/JP4657482B2/en not_active Expired - Lifetime
Cited By (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2003100220A1 (en) * | 2002-05-24 | 2003-12-04 | Abb Turbo Systems Ag | Axial securing means for impeller blades |
CN100335749C (en) * | 2002-05-24 | 2007-09-05 | Abb涡轮系统有限公司 | Axial securing means for impeller blades |
EP1382800A2 (en) * | 2002-07-20 | 2004-01-21 | Rolls Royce Plc | A fan blade assembly |
EP1382800A3 (en) * | 2002-07-20 | 2006-08-23 | Rolls Royce Plc | A fan blade assembly |
US20140161617A1 (en) * | 2011-08-03 | 2014-06-12 | Snecma | Bladed rotor wheel for a turbine engine |
US9540093B2 (en) * | 2011-08-03 | 2017-01-10 | Snecma | Bladed rotor wheel for a turbine engine |
US20140199172A1 (en) * | 2013-01-11 | 2014-07-17 | General Electric Company | Turbomachine and method of handling turbomachine components |
US12018590B1 (en) | 2023-04-04 | 2024-06-25 | Ge Infrastructure Technology Llc | Method for turbine blade and assembly with dovetail arrangement for enlarged rotor groove |
Also Published As
Publication number | Publication date |
---|---|
JP4657482B2 (en) | 2011-03-23 |
JP2001295602A (en) | 2001-10-26 |
ES2247028T3 (en) | 2006-03-01 |
ATE307269T1 (en) | 2005-11-15 |
EP1138879A1 (en) | 2001-10-04 |
DE60114065D1 (en) | 2005-11-24 |
FR2807096B1 (en) | 2002-05-31 |
FR2807096A1 (en) | 2001-10-05 |
US6447253B2 (en) | 2002-09-10 |
EP1138879B1 (en) | 2005-10-19 |
DE60114065T2 (en) | 2006-04-20 |
DK1138879T3 (en) | 2006-03-06 |
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