EP2466072A2 - Axial air movement fans - Google Patents
Axial air movement fans Download PDFInfo
- Publication number
- EP2466072A2 EP2466072A2 EP11075270A EP11075270A EP2466072A2 EP 2466072 A2 EP2466072 A2 EP 2466072A2 EP 11075270 A EP11075270 A EP 11075270A EP 11075270 A EP11075270 A EP 11075270A EP 2466072 A2 EP2466072 A2 EP 2466072A2
- Authority
- EP
- European Patent Office
- Prior art keywords
- fan
- plate
- blade
- secured
- fan blade
- 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
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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
- F01D5/12—Blades
- F01D5/14—Form or construction
- F01D5/16—Form or construction for counteracting blade vibration
-
- 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
- F04D29/66—Combating cavitation, whirls, noise, vibration or the like; Balancing
- F04D29/661—Combating cavitation, whirls, noise, vibration or the like; Balancing especially adapted for elastic fluid pumps
- F04D29/668—Combating cavitation, whirls, noise, vibration or the like; Balancing especially adapted for elastic fluid pumps damping or preventing mechanical vibrations
-
- 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
- F04D29/324—Blades
-
- 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
- F04D29/38—Blades
- F04D29/388—Blades characterised by construction
Definitions
- the present invention relates to axial air movement fans comprising a plurality of elongate fan blades disposed about a hub so as to extend in a generally radial direction.
- Each fan blade therefore constitutes a cantilever secured to the hub and extending outwardly to the outer free end of the blade.
- the fan blades are elongate and typically placed at an angle to the circumferential plane of the axis of rotation and may have an aerofoil type cross-section to drive air across the fan. In cross-section, the fan blades have a major axis and a minor axis.
- the fan blades In operation, when driving air, the fan blades are subject to air pressure and further forces caused by buffeting and turbulence of the air passing through the faun. These forces are transmitted to the hub as a cyclical bending moment through the root of the fan blade which is secured to the hub. The blades thus tend to bend about the major axis and the stress concentration at this point can lead to cracking and failure of the blade.
- the present invention seeks to provide a solution to this problem.
- an axial air movement fan comprising a hub with a plurality of elongate fan blades extending generally radially outwardly therefrom, wherein each fan blade is at least partially hollow and at least one damping mass is located within the hollow part, the mass being at least partially provided by a resilient plate, one edge of which is secured to the fan blade to form a cantilever, and being secured to the fan blade in such a way as oscillate relative to the fan blade in response to oscillatory flexing of the fan blade in a first plane, thereby to damp the flexing of the fan blade, the end of the plate remote from said secured end being held in a guide device to constrain its movement in a controlled manner when the plate is oscillating, and wherein a further guide device is located between the secured end of the plate and the first guide device and engages the plate in such a way as to enable the natural frequency of oscillation of the mass to be adjusted to match the natural frequency of the blade.
- the plate is constrained against radial movement caused by centrifugal force, but is permitted a degree of lateral resilient movement to enable the plate to oscillate.
- a resilient damping mass is located between each of the two members and the plate.
- the further guide device is located closer to the secured end than the outermost end.
- the cross-sectional area of the plate varies along its length to give a desired form of flexure.
- a plurality of said plates may be provided in each fan blade.
- Figure 1 shows a hub 1 of an axial fan mounted for rotation about an axis 2.
- a plurality of elongate fan blades equidistantly disposed about the periphery of the hub and secured thereto so as to extend in a generally radial direction.
- the fan blade consists of an elongate member extending generally radially and is secured at its root to the hub at a slight angle to the plane of rotation of the hub.
- the fan has in cross-section a major axis 4 and a minor axis 5. It also has a radially extending longitudinal main axis 6.
- the weight of the mass, the resilience of the wire and the initial tension in the wire is calculated to permit the mass to oscillate in response to vibratory movement of the blade at its first natural frequency.
- the fan blade acts as a cantilever and if an exciting force caused by turbulent airflow over the fan blade is present at the first natural frequency of the fan blade, permanent oscillation at the natural frequency may occur and this vibratory movement is opposed and dampened by the corresponding transverse oscillations of the mass, which responds to the oscillation of the fan blade and serves to damp out the induced oscillations in the fan blade. In this way, the stresses in the blade, particularly at the root of the blade, which could lead to early failure of the blade, are substantially reduced.
- the mass it is desirable for the mass to be located as far towards the outer tip of the fan blade as possible as this reduces the size of the mass needed.
- the mass may be supported on a synthetic rubber bushing system designed to restrain the mass against movement in a radial direction but to move in a controlled resilient manner in a direction normal to the major axis of the blade.
- Figure 3a shows a flexible plate 12 located in the interior of a fan blade casing 13.
- the radially innermost edge 14 of the plate 12 is secured by bolts in a mounting 15 secured to the main body of the fan blade.
- the plate 12 is located in a guide device 17 which has a pair of opposing clamping members 18 and 19 between which the plate is located.
- the locating members are secured by bolts to a mounting bracket 20 secured to the main body of the fan blade13.
- the surfaces 21, 22 of the clamping members facing and engaging with the plate 12 are curved or arcuate so that there is only a single line contact between the clamping members and the plate on a line a short distance from the outer edge 14 of the plate.
- the outer part of the plate 12 is able to pivot slightly when the plate curves due to oscillatory forces and is also able to accommodate the slight change in length, that is longitudinal extent, of the plate due to the curvature it adopts when being deflected.
- resilient means such as rubber bushing is positioned between the surfaces of the clamping members and the plate, the resilient means having sufficient flexibility to accommodate the required slight movement of the end of the plate.
- a further guide 23 may be positioned intermediate the ends of the plate 12 to control the amount of movement of the plate in this mid-position and to fine tune the natural frequency of vibration of the plate to conform to that of the individual blade.
- this further guide' device is located approximately one quarter of the way from the fixed end of the plate towards the free end, but the position at which it engages the plate may be varied to give the oscillatory characteristics desired.
- the further guide device has two clamping members 24, 25 which engage the plate 12 on a line contact. The two clamping members are again bolted to a mount 26 secured to the main body of the fan blade. It is also envisaged that resilient damping means may be disposed between the clamping faces of the members 24 and 25 and the plate 12.
- FIG 4 there is shown a part sectional view of a fan blade 13 having a hollow interior containing two damping plates 12, both in accordance with the present invention.
- the two damping plates 12 are identical and only one will be described for convenience, although it will be appreciated that the two devices may be of different size, thickness and shape to achieve the damping characteristics required.
- the plate 12 is secured in a mounting bracket 15 in turn secured to the main body of the fan blade 13. At its radially outermost end 16, the plate is located in a guide device 17 as described in connection with Figure 3a .
- a further guide 23 is located, although, compared to the embodiment of Figure 3a , the clamping members 24, 25 are directed in the radially outward direction rather than radially inwardly.
- the point at which the clamping members engage the plate is adjustable by means of changing the shape of the members or by spacers positioned between the clamping members and the mounting 24 through which the device is secured to the fan blade. In this way the natural frequency of oscillation can be fine-tuned to match the individual blade.
- a further damping means 27 is located generally intermediate the guide devices 17 and 23.
- the damping means 27 consists of brackets 28, 29 secured to the main body of the fan blade 13 and each carrying a pair of resilient damping masses 31, 32 formed by rubber bushes, which abut the faces of the plate 12 and are designed to limit and damp the oscillatory movement of the plate. Although shown as abutting the plate, it will be understood that in certain circumstances these resilient masses 31, 32 may be spaced from the surface of the plate in the static position.
- the fan blade 13 contains two identical plates 12 but it is envisaged that these plates may differ in size and thickness, and response rate to give the desired damping characteristics.
- the mountings 24 for the plates 12 are located in elongate slots 32 in a subframe 33 which is itself secured to the fan blade. In this way, the whole damping assembly can be built as a subassembly with varying widths of plate for easy incorporation into the fan blade on final assembly.
- the mass may be suspended on the outside of the blade with the wire being secured to limbs extending outwardly from the blade face. It is possible that two masses may be provided, one on each face of the blade. It is also possible for the mass or masses to be secured directly to the blade by means of a resilient mounting bush formed of synthetic rubber.
- a higher frequency harmonic may be generated in the fan blade causing the blades to oscillate about its longitudinal axis 6.
- a smaller mass may be secured in the hollow section of the blade in such a way that it is constrained against radial movement but is able to oscillate about the longitudinal axis 6 of the blade.
- the mass it may be preferable for the mass to be a disc like structure with its mass concentrated at the periphery.
- the mass may be formed by an outer skin section bonded to the rest of the blade by means of a resilient bushing and having the same profile as the fan blade so as not to adversely effect the flow of air past the blade.
Abstract
Description
- The present invention relates to axial air movement fans comprising a plurality of elongate fan blades disposed about a hub so as to extend in a generally radial direction.
- Each fan blade therefore constitutes a cantilever secured to the hub and extending outwardly to the outer free end of the blade. The fan blades are elongate and typically placed at an angle to the circumferential plane of the axis of rotation and may have an aerofoil type cross-section to drive air across the fan. In cross-section, the fan blades have a major axis and a minor axis. In operation, when driving air, the fan blades are subject to air pressure and further forces caused by buffeting and turbulence of the air passing through the faun. These forces are transmitted to the hub as a cyclical bending moment through the root of the fan blade which is secured to the hub. The blades thus tend to bend about the major axis and the stress concentration at this point can lead to cracking and failure of the blade.
- The normal operating forces are exacerbated if the vibratory loads on the blade are generated at the natural frequency of oscillation of the cantilevered blade. This can cause a permanent oscillation or vibration about the major axis of the blade at its root which can lead to premature and catastrophic failure of the blade..
- Previous proposals have been made to provide an internal damping mass to counterbalance such oscillations in rotating blades but these have had limitations. Examples of prior art proposals are shown in
US Patent No. 2828941 ,EP1754866 A1 andUS 2009/0324406 . It has been found, particularly in large fans, that the natural frequencies of the individual blades varies. This is commonly due to slight variations between the blades which are inevitably caused by production tolerances in the construction and materials of the blade. A consequence of this is that the fan as a whole can be operating outside its natural frequency but an individual blade can be operating, undetected, at its own natural frequency. This leads to unexpected catastrophic failure of the blade which can destroy the whole fan. - The present invention seeks to provide a solution to this problem.
- According to the present invention there is provided an axial air movement fan comprising a hub with a plurality of elongate fan blades extending generally radially outwardly therefrom, wherein each fan blade is at least partially hollow and at least one damping mass is located within the hollow part, the mass being at least partially provided by a resilient plate, one edge of which is secured to the fan blade to form a cantilever, and being secured to the fan blade in such a way as oscillate relative to the fan blade in response to oscillatory flexing of the fan blade in a first plane, thereby to damp the flexing of the fan blade, the end of the plate remote from said secured end being held in a guide device to constrain its movement in a controlled manner when the plate is oscillating, and wherein a further guide device is located between the secured end of the plate and the first guide device and engages the plate in such a way as to enable the natural frequency of oscillation of the mass to be adjusted to match the natural frequency of the blade.
- In this way, the plate is constrained against radial movement caused by centrifugal force, but is permitted a degree of lateral resilient movement to enable the plate to oscillate.
- Although only one mass is shown in this embodiment, it will be understood that two separate masses may be located in the hollow space in the blade and these two masses may be tuned to be responsive to different frequencies.
- Preferably, the guide device comprises two members between faces of which said outermost end is clamped so as to be constrained against lateral movement but is able to pivot relative to the members, in which case said faces may be curved so that the contact between the members and the plate is a line contact.
- In one form, a resilient damping mass is located between each of the two members and the plate.
- Preferably, the further guide device is located closer to the secured end than the outermost end.
- Furthermore, a resilient damping mass may be located between each of the two members and the plate.
- In a preferred embodiment, the cross-sectional area of the plate varies along its length to give a desired form of flexure.
- A plurality of said plates may be provided in each fan blade.
- A preferred embodiment of the present invention will now be described by way of example with reference to the accompanying informal sketch in which:
-
Figure 1 shows a schematic view of a blade of an air movement fan illustrating the principle of the invention, -
Figure 2 shows a schematic cross-sectional view showing the hollow interior of the fan blade ofFigure 1 -
Figures 3a and 3b show a schematic arrangement of a preferred embodiment of the invention, and -
Figure 4 shows an embodiment in which a plurality of plates are provided. -
Figure 1 shows ahub 1 of an axial fan mounted for rotation about anaxis 2. A plurality of elongate fan blades, only one of which is shown asreference 3, equidistantly disposed about the periphery of the hub and secured thereto so as to extend in a generally radial direction. As shown, the fan blade consists of an elongate member extending generally radially and is secured at its root to the hub at a slight angle to the plane of rotation of the hub. The fan has in cross-section amajor axis 4 and a minor axis 5. It also has a radially extending longitudinalmain axis 6. - Adjacent to its outer end, the fan blade has a
hollow section 7 which contains a mass-spring system. The system consists of amass 11, which may be formed of lead, which is suspended on a wire 8 intermediate the length thereof. The wire extends along theaxis 6 of theblade 3 and is secured to the blade at its ends,references 9 and 10. The mass is thus constrained by the wire against movement in the radial direction caused by centrifugal force apart from a slight resilient extension of the part of the wire between the mass and the radially innermost fastening, but is permitted a degree of lateral movement against the resilience of the wire. It is envisaged that some degree of damping of the movement of the mass may be provided, which may be accomplished by means of a resilient damper such as a rubber bushing. The weight of the mass, the resilience of the wire and the initial tension in the wire is calculated to permit the mass to oscillate in response to vibratory movement of the blade at its first natural frequency. The fan blade acts as a cantilever and if an exciting force caused by turbulent airflow over the fan blade is present at the first natural frequency of the fan blade, permanent oscillation at the natural frequency may occur and this vibratory movement is opposed and dampened by the corresponding transverse oscillations of the mass, which responds to the oscillation of the fan blade and serves to damp out the induced oscillations in the fan blade. In this way, the stresses in the blade, particularly at the root of the blade, which could lead to early failure of the blade, are substantially reduced. - It is desirable for the mass to be located as far towards the outer tip of the fan blade as possible as this reduces the size of the mass needed. Although shown as a mass suspended on a wire, it is conceivable that the mass may be supported on a synthetic rubber bushing system designed to restrain the mass against movement in a radial direction but to move in a controlled resilient manner in a direction normal to the major axis of the blade.
-
Figures 3a, 3b and4 show an embodiment of the invention, in whichFigure 3a shows a cross-section through the hollow part of a fan blade viewed in the circumferential direction showing a flexible plate,Figure 3b shows a view of the flexible plate in the direction of the arrow A inFigure 3a , andFigure 4 shows a part sectional perspective view of an arrangement in which two plates are located in the interior of the fan blade. -
Figure 3a shows aflexible plate 12 located in the interior of afan blade casing 13. The radiallyinnermost edge 14 of theplate 12 is secured by bolts in amounting 15 secured to the main body of the fan blade. At its radiallyoutermost end 16, theplate 12 is located in aguide device 17 which has a pair of opposingclamping members mounting bracket 20 secured to the main body of the fan blade13. Thesurfaces plate 12 are curved or arcuate so that there is only a single line contact between the clamping members and the plate on a line a short distance from theouter edge 14 of the plate. In this way, the outer part of theplate 12 is able to pivot slightly when the plate curves due to oscillatory forces and is also able to accommodate the slight change in length, that is longitudinal extent, of the plate due to the curvature it adopts when being deflected. In an alternative embodiment (not shown), resilient means such as rubber bushing is positioned between the surfaces of the clamping members and the plate, the resilient means having sufficient flexibility to accommodate the required slight movement of the end of the plate. - Additionally, a
further guide 23 may be positioned intermediate the ends of theplate 12 to control the amount of movement of the plate in this mid-position and to fine tune the natural frequency of vibration of the plate to conform to that of the individual blade. As shown, this further guide' device is located approximately one quarter of the way from the fixed end of the plate towards the free end, but the position at which it engages the plate may be varied to give the oscillatory characteristics desired. In a similar manner to the first guide device, the further guide device has two clampingmembers plate 12 on a line contact. The two clamping members are again bolted to amount 26 secured to the main body of the fan blade. It is also envisaged that resilient damping means may be disposed between the clamping faces of themembers plate 12. In this way, when the plate flexes due to oscillatory forces, its assumes a shallow S shape with the part below thelower guide 23 curving in one direction and the part between the twoguides - Referring now to
Figure 3b , it can be seen that the cross-sectional area of the plate can be varied by varying its width, or metal thickness, to give the desired damping characteristics. - Turning now to
Figure 4 , there is shown a part sectional view of afan blade 13 having a hollow interior containing twodamping plates 12, both in accordance with the present invention. In this embodiment the twodamping plates 12 are identical and only one will be described for convenience, although it will be appreciated that the two devices may be of different size, thickness and shape to achieve the damping characteristics required. - In this description of
Figure 4 like parts will bear like references to those shown inFigure 3a . Theplate 12 is secured in amounting bracket 15 in turn secured to the main body of thefan blade 13. At its radiallyoutermost end 16, the plate is located in aguide device 17 as described in connection withFigure 3a . Just radially outwardly of the mountingbracket 15, afurther guide 23 is located, although, compared to the embodiment ofFigure 3a , the clampingmembers - In addition, in this embodiment, a further damping
means 27 is located generally intermediate theguide devices brackets fan blade 13 and each carrying a pair of resilient dampingmasses plate 12 and are designed to limit and damp the oscillatory movement of the plate. Although shown as abutting the plate, it will be understood that in certain circumstances theseresilient masses - It can be seen that the
fan blade 13 contains twoidentical plates 12 but it is envisaged that these plates may differ in size and thickness, and response rate to give the desired damping characteristics. To increase flexibility, themountings 24 for theplates 12 are located inelongate slots 32 in asubframe 33 which is itself secured to the fan blade. In this way, the whole damping assembly can be built as a subassembly with varying widths of plate for easy incorporation into the fan blade on final assembly. - For relatively small sizes of fan blade, it may not be practical to locate the mass within the blade, in which case the mass may be suspended on the outside of the blade with the wire being secured to limbs extending outwardly from the blade face. It is possible that two masses may be provided, one on each face of the blade. It is also possible for the mass or masses to be secured directly to the blade by means of a resilient mounting bush formed of synthetic rubber.
- In certain installations, under certain conditions, a higher frequency harmonic may be generated in the fan blade causing the blades to oscillate about its
longitudinal axis 6. To counter this, a smaller mass may be secured in the hollow section of the blade in such a way that it is constrained against radial movement but is able to oscillate about thelongitudinal axis 6 of the blade. In such an arrangement, it may be preferable for the mass to be a disc like structure with its mass concentrated at the periphery. - In a further embodiment, the mass may be formed by an outer skin section bonded to the rest of the blade by means of a resilient bushing and having the same profile as the fan blade so as not to adversely effect the flow of air past the blade.
- When more than one mass is provided these may be tuned to be responsive to different frequencies.
Claims (14)
- An axial air movement fan comprising a hub (1) with a plurality of elongate fan blades (3) extending generally radially outwardly therefrom, wherein each fan blade (3) is at least partially hollow and at least one damping mass (11) is located within the hollow part, the mass (11) being at least partially provided by a resilient plate (12), one edge (14) of which is secured to the fan blade (3) to form a cantilever, and being secured to the fan blade (3) in such a way as to oscillate relative to the fan blade (3) in response to oscillatory flexing of the fan blade in a first plane, thereby to damp the flexing of the fan blade (3), characterised in that,
the end (16) of the plate (12) remote from said secured end being held in a guide device (17) to constrain its movement in a controlled manner when the plate (12) is oscillating, and wherein a further guide device (23) is located between the secured end (14) of the plate (12) and the first guide device (17) and engages the plate in such a way as to enable the natural frequency of oscillation of the mass to be adjusted to match the natural frequency of the fan blade (3). - A fan as claimed in claim 1, wherein the location at which the further guide device (23) engages the plate (12) is adjustable relative to the end (!4) of the plate secured to the fan blade.
- A fan as clamed in claim 1 or 2, wherein the plate (12) is secured to the radially outermost face of the hollow space.
- A fan as claimed in claim 1 or 2, wherein the plate (12) is secured at its radially innermost edge to the fan blade (3).
- A fan as claimed in claim 1 wherein the guide device (17) comprises two members between faces of which said outermost end (16) is clamped so as to be constrained against lateral movement but is able to pivot relative to the members.
- A fan according to any one of the preceding claims wherein the further guide device comprises two members (18, 19) between faces of which an intermediate part of the plate (12) is clamped so as to be constrained against lateral movement but is able to pivot relative to the members (18, 19).
- A fan as claimed in claim 5 or 6, wherein said faces are curved so that the contact between the members (18, 19) and the plate (12) is a line contact.
- A fan as claimed in claim 5 or 6 wherein a resilient damping mass is located between each of the two members (18, 19) and the plate (12).
- A fan according to any one of the preceding claims wherein the further guide device (23) is located closer to the secured end (14) than the outermost end (17) of the plate (12).
- A fan according to any one of the preceding claims wherein a further damping means is located between the guide device (17) and the further guide device (23) comprising damping means to,limit and damp oscillatory movement of the plate.
- A fan according to claim 10, wherein tHe damping means comprise rubber or synthetic rubber bushes.
- A fan as claimed in any one of the preceding claims, wherein the cross-sectional area of the plate (12) varies along its length to give a desired form of flexure.
- A fan according to any one of the preceding claims wherein a plurality of said plates (12) are provided.
- A fan as claimed in any one of the preceding claims, including a further mass adapted to dampen a higher frequency harmonic by oscillatory movement about the longitudinal axis of the blade.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB1021349.4A GB2486470A (en) | 2010-12-16 | 2010-12-16 | Fan blade with oscillating damping mass |
Publications (3)
Publication Number | Publication Date |
---|---|
EP2466072A2 true EP2466072A2 (en) | 2012-06-20 |
EP2466072A3 EP2466072A3 (en) | 2016-12-21 |
EP2466072B1 EP2466072B1 (en) | 2018-07-04 |
Family
ID=43567308
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP11075270.6A Active EP2466072B1 (en) | 2010-12-16 | 2011-12-14 | Axial air movement fans |
Country Status (2)
Country | Link |
---|---|
EP (1) | EP2466072B1 (en) |
GB (2) | GB2486470A (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2015112891A1 (en) | 2014-01-24 | 2015-07-30 | United Technologies Corporation | Additive manufacturing process grown integrated torsional damper mechanism in gas turbine engine blade |
Family Cites Families (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2689107A (en) * | 1949-08-13 | 1954-09-14 | United Aircraft Corp | Vibration damper for blades and vanes |
US2828941A (en) * | 1952-12-24 | 1958-04-01 | United Aircraft Corp | Blade damping means |
US2920868A (en) * | 1955-10-05 | 1960-01-12 | Westinghouse Electric Corp | Dampened blade structure |
GB2093126B (en) * | 1981-02-12 | 1984-05-16 | Rolls Royce | Rotor blade for a gas turbine engine |
US5232344A (en) * | 1992-01-17 | 1993-08-03 | United Technologies Corporation | Internally damped blades |
DE29522190U1 (en) * | 1994-02-07 | 2000-12-14 | Lm Glasfiber As Lunderskov | Windmill blade |
US6155789A (en) * | 1999-04-06 | 2000-12-05 | General Electric Company | Gas turbine engine airfoil damper and method for production |
US7993113B2 (en) * | 2004-10-15 | 2011-08-09 | Boc Edwards Japan Limited | Damper and vacuum pump |
EP1754886B1 (en) * | 2005-08-17 | 2012-10-10 | General Electric Company | Rotor blade for a wind energy turbine |
US7270517B2 (en) * | 2005-10-06 | 2007-09-18 | Siemens Power Generation, Inc. | Turbine blade with vibration damper |
FR2933068B1 (en) * | 2008-06-27 | 2011-02-25 | Eurocopter France | BLADE FOR REDUCING MOVEMENTS IN TRAINING OF SAID BLADE AND METHOD FOR REDUCING SUCH MOVEMENT IN TRAINEE. |
-
2010
- 2010-12-16 GB GB1021349.4A patent/GB2486470A/en not_active Withdrawn
-
2011
- 2011-12-14 GB GB1121432.7A patent/GB2486557B/en active Active
- 2011-12-14 EP EP11075270.6A patent/EP2466072B1/en active Active
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2015112891A1 (en) | 2014-01-24 | 2015-07-30 | United Technologies Corporation | Additive manufacturing process grown integrated torsional damper mechanism in gas turbine engine blade |
EP3097268A4 (en) * | 2014-01-24 | 2017-03-15 | United Technologies Corporation | Additive manufacturing process grown integrated torsional damper mechanism in gas turbine engine blade |
US10914320B2 (en) | 2014-01-24 | 2021-02-09 | Raytheon Technologies Corporation | Additive manufacturing process grown integrated torsional damper mechanism in gas turbine engine blade |
Also Published As
Publication number | Publication date |
---|---|
EP2466072A3 (en) | 2016-12-21 |
GB201021349D0 (en) | 2011-01-26 |
GB2486557A (en) | 2012-06-20 |
EP2466072B1 (en) | 2018-07-04 |
GB2486557B (en) | 2017-02-08 |
GB2486470A (en) | 2012-06-20 |
GB201121432D0 (en) | 2012-01-25 |
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