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
  • F01D5/3007—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
  • F01D5/32—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
• • 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
  • F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
  • F01D25/04—Antivibration arrangements
  • F01D25/06—Antivibration arrangements for preventing blade vibration
• • 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
  • F01D5/3092—Protective layers between blade root and rotor disc surfaces, e.g. anti-friction layers
• • 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
  • F05D2300/00—Materials; Properties thereof
  • F05D2300/40—Organic materials
  • F05D2300/43—Synthetic polymers, e.g. plastics; Rubber

Definitions

• the present invention relates generally to the field of aircraft turbojet blowers, and more particularly to the shims intended to be interposed between the foot of the fan blades, and the bottom of the cells defined by the fan disk.
• Such a turbojet fan is shown in an exploded manner in FIG. 1. It generally comprises a disk 2 centered on the axis 4 of the fan, a disk on the periphery of which are teeth 6 circumferentially spaced apart from each other, and extending each substantially longitudinally and radially, namely substantially parallel to the axis 4. Between two directly consecutive teeth 6 in the circumferential direction, these define a cell 8 intended to receive the foot 12 of a fan blade 10.
• each tooth has an enlarged head so as to ensure the retention of the blades in the radial direction to the outside.
• the cell 8 has a narrowed external radial end allowing the stamina of the blade 10 to pass, with a narrowed section compared to that of its foot 12.
• the conferred assembly is of the dovetail type, or also called "fir fastener”.
• the fan 1 comprises a shim 20 interposed between the lower end of the blade root 12, and a bottom 8a of the cell associated with the blade concerned.
• the wedge 20 makes it possible to block the blade 10 in the radial inward direction, and also contributes to the plating of the bearing surfaces of the foot 12 against the energy end of the teeth 6.
• the shim 20 comprises an abutment 22 for axial retention of its associated blade, this abutment 22 being intended to bear against a retention ring (not shown) carried by the disk 2 and centered on axis 4.
• the shim 20 conventionally has a metal frame 24 around which is placed one or more outer elements 26 made of elastomeric material, this element 26 being in contact with the bottom 8a of the cell and the radially inner end of the foot 12 of dawn.
• each element 26 is made by injection molding on the metal reinforcement, which is preferably made of titanium.
• the overmolding process used is such as to cause the outer element 26 of elastomeric material to adhere to a support surface provided on the reinforcement 24.
• outer member 26 also referred to as a delamination problem. Indeed, this problem arises essentially when the wedge 20 is inserted between the foot 12 and the bottom of the cell 8a during engine assembly and / or during handling operations requiring such a wedge introduction. As shown schematically in Figure 1, it is noted that the introduction of the wedge in its dedicated space is effected by sliding it along its longitudinal direction 30, generally slightly curvilinear.
• the blade retention properties associated with this wedge may no longer be satisfied.
• the wedge also having a vibration reduction function within the blade, its deterioration leads to lowering the vibration damping level experienced by the fan blade in operation.
• the object of the invention is therefore to remedy at least partially the disadvantages mentioned above relating to the embodiments of the prior art.
• the subject of the invention is preferably Preferably, the wedge takes the form of a band extending in a longitudinal direction, said corrugated zone having a plurality of waves succeeding that the same direction.
• the waves thus arranged make it possible to withstand the delamination of the outer element made of elastomer material even more effectively when the wedge is introduced between the blade root and the cell bottom. Indeed, these waves then constitute direct obstacles to the relative displacement between the frame and the outer element of the hold, in the longitudinal direction, which usually corresponds to the direction of introduction of the hold in its dedicated space under the dawn.
• the outer element of elastomeric material is overmolded on the metal reinforcement, preferably by injection under pressure.
• the metal reinforcement is made of titanium.
• the invention also relates to a turbojet fan comprising a plurality of fan blades and a disk defining at its periphery a plurality of cells, the foot of each fan blade being housed in one of the cells, and a shim as described above being interposed between the bottom of the cell and said foot.
• each shim travels along the foot of its associated fan blade.
• each shim has an axial retention stop of its associated fan blade.
• the invention also relates to an aircraft turbojet engine comprising a fan as described above.
• Figure 2 shows a partial cross-sectional view of the blower shown in Figure 1;
• FIG. 3 represents a perspective view of a turbojet fan shim, according to a preferred embodiment of the present invention
• FIG. 4 shows a view similar to that of FIG. 3, in which the elastomeric material outer element has been removed in order to show only the metal reinforcement and its support surface of the outer element
• - Figure 4a shows a sectional view taken along the plane P of Figure 4a, integrating the longitudinal direction of the shim, and showing the corrugated areas of the support surface formed by the metal frame.
• a shim 120 according to a preferred embodiment of the present invention.
• This shim whose outer shape is substantially identical or similar to that of the wedge 20 of the prior art described in Figures 1 and 2, also has a general shape of strip extending on a longitudinal direction 130 of substantially curvilinear shape, corresponding to the direction in which also extends the foot 12 of its associated blade and the bottom of cell 8a.
• the wedge 120 is intended to be introduced between the blade 10 and the bottom 8a of the cell 8 shown in FIG. 1, again for purposes of retention of the blade as well as damping. vibrations suffered by it.
• the metal armature 124 preferably made of titanium, is equipped with an outer element of elastomeric material referenced 126, which partially covers the outer surface of this frame.
• the outer element 126 made by overmolding by pressure injection of elastomeric material on the armature 124, leaves free a portion of the outer surface of this armature.
• FIG. 4 this same armature 124 is shown in a state in which it is not yet covered by its outer element 126. This makes it possible to reveal the support surface 134 of this external element, which, as is visible in FIGS. 4 and 4a, has several corrugated zones 136.
• Each corrugated zone 136 is in fact formed from a succession of waves 140 between which there are rounded depressions 142. Thus, during the overmolding by injection of the elastomeric material , this last penetrates the hollows 142, which has the double consequence of increasing the adhesion surface of the element 126 on the armature 124, and to create a plurality of mechanical engagement of the waves of the armature in the recesses of the outer element, and vice versa. In this regard, to further reduce the risk of delamination of the element 126, it is expected that the waves 140 of each corrugated zone 136 follow one another in the longitudinal direction 130 in which the wedge 120 is usually moved relative to the disk 2, so as to be interposed between the blade root 12 and the cell bottom 8a.
• two corrugated zones 136 oriented in opposite directions are provided here, one of which may optionally be interrupted at one or more points by a portion of the armature 124 intended to form part of the outer surface of the finished block.
• the two corrugated zones 136 are interconnected by a radially outer zone 146 and a radially internal zone (not visible in FIG. 4), these two zones being preferably flat and parallel to the direction 130.
• the shim 120 here also has a stop 122 for axial retention of its associated fan blade, having the same geometry as the stop 22 shown on the shim 20 of FIG.

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• Engineering & Computer Science (AREA)
• Mechanical Engineering (AREA)
• General Engineering & Computer Science (AREA)
• Structures Of Non-Positive Displacement Pumps (AREA)
• Turbine Rotor Nozzle Sealing (AREA)
• Gasket Seals (AREA)

Applications Claiming Priority (2)

Publications (2)

Family

ID=41508313

Family Applications (1)

Country Status (9)

Cited By (1)

Families Citing this family (26)

Family Cites Families (37)

• 2009
  • 2009-04-29 FR FR0952812A patent/FR2945074B1/fr not_active Expired - Fee Related
• 2010
  • 2010-04-28 JP JP2012507727A patent/JP5699131B2/ja active Active
  • 2010-04-28 CN CN201080018604.9A patent/CN102414397B/zh active Active
  • 2010-04-28 US US13/265,200 patent/US8870545B2/en active Active
  • 2010-04-28 RU RU2011148428/06A patent/RU2526607C2/ru active
  • 2010-04-28 EP EP10718553.0A patent/EP2425100B1/de active Active
  • 2010-04-28 WO PCT/EP2010/055689 patent/WO2010125089A1/fr not_active Ceased
  • 2010-04-28 BR BRPI1013981-8A patent/BRPI1013981B1/pt active IP Right Grant
  • 2010-04-28 CA CA2760290A patent/CA2760290C/fr active Active

Non-Patent Citations (1)

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