EP2630335B1 - Hydraulic device for changing the pitch of a propeller - Google Patents
Hydraulic device for changing the pitch of a propeller Download PDFInfo
- Publication number
- EP2630335B1 EP2630335B1 EP11779773.8A EP11779773A EP2630335B1 EP 2630335 B1 EP2630335 B1 EP 2630335B1 EP 11779773 A EP11779773 A EP 11779773A EP 2630335 B1 EP2630335 B1 EP 2630335B1
- Authority
- EP
- European Patent Office
- Prior art keywords
- changing
- hydraulic device
- propeller pitch
- nut
- propeller
- 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.)
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Links
- 239000002184 metal Substances 0.000 claims description 41
- 230000000903 blocking effect Effects 0.000 claims description 3
- 239000012530 fluid Substances 0.000 claims description 3
- 230000005540 biological transmission Effects 0.000 claims description 2
- BASFCYQUMIYNBI-UHFFFAOYSA-N platinum Chemical compound [Pt] BASFCYQUMIYNBI-UHFFFAOYSA-N 0.000 description 5
- 238000006073 displacement reaction Methods 0.000 description 3
- 238000004519 manufacturing process Methods 0.000 description 3
- 239000000463 material Substances 0.000 description 3
- 238000002788 crimping Methods 0.000 description 2
- 238000012423 maintenance Methods 0.000 description 2
- 230000000295 complement effect Effects 0.000 description 1
Images
Classifications
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- 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
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- 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
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- 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
- F04D29/40—Casings; Connections of working fluid
- F04D29/52—Casings; Connections of working fluid for axial pumps
- F04D29/54—Fluid-guiding means, e.g. diffusers
- F04D29/56—Fluid-guiding means, e.g. diffusers adjustable
- F04D29/563—Fluid-guiding means, e.g. diffusers adjustable specially adapted for elastic fluid pumps
-
- 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
- F05D2220/00—Application
- F05D2220/30—Application in turbines
- F05D2220/36—Application in turbines specially adapted for the fan of turbofan engines
-
- 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
- F05D2260/50—Kinematic linkage, i.e. transmission of position
-
- 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
Definitions
- the present invention relates to a hydraulic device of a propeller pitch change control device.
- the field of the invention is that of systems provided with a propeller, such as a wind turbine, an industrial fan, but also turbomachines and turbojet engines provided with a fan comprising a plurality of blades or blades at angles of variable setting.
- a propeller such as a wind turbine, an industrial fan
- turbomachines and turbojet engines provided with a fan comprising a plurality of blades or blades at angles of variable setting.
- a turbomachine comprises one or more stages of variable pitch vanes which are mounted between rotor wheels of a compressor. These variable-pitch vanes are carried by the stator of the turbomachine and are adjustable in position about their axis to optimize the flow of gas in the engine of the turbomachine.
- the variation of the setting of the blades makes it possible to increase the performances and to improve the efficiency of the engine of a turbomachine during all the phases of its operation, from the take-off to the landing.
- This variable setting also makes it possible to vary the speed of the propeller or the blower to obtain the desired thrust, without modifying that of the turbine, which is generally calibrated at its maximum continuous speed, or even, during landing, to reverse this thrust thus replacing conventional heavy and complex reverse thrust systems.
- Propeller or fan pitch control devices are hydraulic actuators (jacks driving each of the blade roots) which provide the force necessary to orient the blades in the desired position.
- Such a control device is for example described in the document FR2928979 .
- Each variable-pitch blade has a cylindrical pivot at each of its ends, these pivots defining the axis of rotation of the blade.
- the radially outer pivot of the blade is engaged in a chimney cylindrical outer annular casing which is connected by means of a rod to a control ring mounted around the annular housing.
- the control ring is connected by a lever to a control shaft actuated by a hydraulic cylinder.
- the control shaft extends parallel to the axis of the housing and can be connected to one or more rings so as to control one or more stages of blades with a single cylinder.
- the hydraulic cylinder rod is connected to the control shaft by a radial arm integral with the control shaft causing, by linear displacement of the cylinder rod, the rotation of each of the rings around the housing.
- the rotation of a control ring is transmitted by the corresponding billets to the outer pivots of the blades of a stage rotating them about their axes.
- the rod of the jack has at its end a yoke for ensuring a connection with a ball joint forming the end of the radial arm integral with the control shaft.
- the connection between the yoke and the ball joint is ensured by means of a screw-nut connection.
- the operator is in the need to dismantle different neighboring parts in order to free a space large enough for the operator to access the nut of the screw-nut connection and thus be able to handle and dismount it easily.
- the invention aims to solve the problems mentioned above, by proposing a hydraulic blade pitch change device to ensure rapid assembly and / or disassembly of the device, for example during a maintenance operation, while avoiding the dismantling of other neighboring rooms.
- the invention proposes a hydraulic device for changing the pitch of a helix comprising a piston rod actuated by a hydraulic fluid, said piston rod comprising at its end a clevis adapted to provide a connection for the transmission of the movements of said piston rod for a pitch change of at least one helix, said hydraulic device being characterized in that it comprises a threaded nut held in position on said yoke of said piston rod by shaped holding means by the cooperation of a metal plate secured to said threaded nut and a metal ring integral with said yoke comprising elastic means able to receive and hold said metal plate in position by clipping, said nut being able to cooperate with a threaded rod to make a connection.
- the disassembly of the hydraulic cylinder for example during a handling operation, is achieved quickly by simply unscrewing the threaded rod to separate the hydraulic cylinder from the control shaft. Disassembly of the cylinder is achieved without disassembly of other neighboring parts despite a complex architecture does not allow access to the clamping nut of the screw-nut connection.
- the invention also relates to a propeller pitch change control device comprising a hydraulic step change device according to the invention.
- the figure 1 is a perspective view of a piston rod of a hydraulic variable pitch pitch changing device according to a first embodiment of the invention.
- the hydraulic jack 100 is formed by a body 10 and a piston rod 20 actuated by the pressure of a hydraulic fluid circulating inside the body 10 of the jack 100.
- the piston rod 20 comprises at its free end a substantially U-shaped yoke 30 which is intended to be connected to the control shaft via a radial arm secured to the control shaft causing, by linear displacement of the rod 20 of the cylinder, the indirect rotation of the blades of the blowers.
- the yoke 30 comprises two coaxial orifices 32 crossing on either side the branches of the U of the yoke 30.
- the space 33 formed between the two branches of the U is intended to receive the end of a radial arm 50 of the yoke. control shaft, called a ball joint, as shown in FIG. figure 2 .
- the yoke 30 comprises a threaded nut 41 held in position by holding means 40.
- the threaded nut is adapted to cooperate with a threaded rod (not shown) inserted through the orifice 32 of the lower branch of the U.
- the threaded nut 41 is a self-locking nut.
- the metal ring 43 has a substantially perpendicular base 47 having an orifice adapted to receive a crimping ring 46.
- the elastic means 44 are arranged in projections relative to the base 47, and at the edge thereof, forming elastic tabs in which notches 48 are arranged to perform a clipping or stapling function.
- the metal ring 43 is secured to the U-shaped yoke for example by shrinking the crimping ring 46 in the hole 32 of the upper branch of the U of the yoke 30.
- the yoke comprises a face 34 serving as a support for the metal ring 43 is thus performing a function of anti-rotation of the metal ring 43.
- This bearing surface 34 is obtained by making a flat on the yoke 30 adapted to form a flat support for the metal ring 43.
- the metal plate 42 is formed from a flat metal sheet of substantially rectangular shape having two openings, for example of rectangular shape and arranged in parallel manner.
- the nut 41 comprises a threaded upper part and a base on which two tabs 45 project radially with respect to the axis of rotation of the nut 41, the shape of the tabs 45 being complementary to the shape of the openings of the metal plate. 42.
- the metal plate 42 is made integral with the nut 41 by folding the lateral edges of the metal sheet on either side of the nut and so that the tabs 45 protruding through the two openings of the metal plate 42.
- the metal plate 42 is integral with movements of the threaded nut 41.
- the metal plate 42 also comprises protuberances 49 able to cooperate with the elastic tabs 44 of the metal ring and more precisely with the notches 48 of the elastic tabs 44.
- the subassembly formed by the nut 41 and the plate 42 is inserted into the metal ring 43, integral with the yoke, until the introduction of the protuberances of the metal plate 42 in the notches 48 of the elastic tabs 44 .
- the protuberances 49 of the metal plate 42 and the corresponding notches 48 may be of different sizes and shapes from the moment they perform a clipping or stapling function between the plate 42 and the ring 43.
- the platen-nut subassembly can be detached from the metal ring 43, and more particularly from the elastic tabs 44, by means of a specific tool allowing the elastic tabs 44 to be sufficiently spaced apart to disengage the protuberances 49 from the notches. 48.
- the nut 41 is made captive, held in position on the yoke 30 while ensuring a certain clearance of operation between the subassembly and the metal ring 43.
- the operating clearance thus allows the nut 41 to be precisely positioned. by self-centering, depending on the position of the threaded rod and thus be able to perform the screwing function between the nut and the threaded rod.
- the threaded rod is a calibrated rod which eliminates the play in the orifices 32 of the yoke 30.
- the orifice 32 of the lower branch of the U comprises a ring 31 whose diameter is also calibrated to receive the calibrated threaded rod (not shown).
- the figure 4 is a perspective view of a piston rod of a hydraulic variable pitch pitch change device according to a second embodiment.
- the anti-rotation function of the metal ring 143 relative to the yoke 30 is achieved by the particular geometry of the metal ring 143.
- the metal ring 143 has an outgrowth of material at its base 147 so as to protrude from the bearing face of the yoke 30.
- the metal ring 143 has a protrusion 150 protruding and directed towards the inside of the yoke 30 adapted to block any displacement by rotation of the metal ring 143 relative to the yoke 30.
- the invention has been mainly described for a hydraulic device for changing the pitch of blades with variable turbine engine fan timing; however, the invention is also applicable to any system with propellers such as wind turbines, industrial fans or turbojets.
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- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Transmission Devices (AREA)
Description
La présente invention concerne un dispositif hydraulique d'un dispositif de commande de changement de pas d'hélice.The present invention relates to a hydraulic device of a propeller pitch change control device.
Le domaine de l'invention est celui des systèmes munis d'une hélice, tel qu'une éolienne, un ventilateur industriel, mais aussi les turbomachines et les turboréacteurs munis d'une soufflante comprenant une pluralité d'aubes ou de pales à angles de calage variable.The field of the invention is that of systems provided with a propeller, such as a wind turbine, an industrial fan, but also turbomachines and turbojet engines provided with a fan comprising a plurality of blades or blades at angles of variable setting.
D'une façon connue, une turbomachine comporte un ou plusieurs étages d'aubes à calage variable qui sont montés entre des roues de rotor d'un compresseur. Ces aubes à calage variable sont portées par le stator de la turbomachine et sont réglables en position autour de leur axe pour optimiser l'écoulement des gaz dans le moteur de la turbomachine. Ainsi, la variation du calage des aubes permet d'augmenter les performances et d'améliorer le rendement du moteur d'une turbomachine durant toutes les phases de son fonctionnement, du décollage à l'atterrissage.In a known manner, a turbomachine comprises one or more stages of variable pitch vanes which are mounted between rotor wheels of a compressor. These variable-pitch vanes are carried by the stator of the turbomachine and are adjustable in position about their axis to optimize the flow of gas in the engine of the turbomachine. Thus, the variation of the setting of the blades makes it possible to increase the performances and to improve the efficiency of the engine of a turbomachine during all the phases of its operation, from the take-off to the landing.
Ce calage variable permet en outre de faire varier le régime de l'hélice ou de la soufflante pour obtenir la poussée désirée, sans modifier celui de la turbine qui est en général calé à son régime maximum continu, voire, lors de l'atterrissage, d'inverser cette poussée remplaçant ainsi les systèmes conventionnels lourds et complexes d'inversion de poussée.This variable setting also makes it possible to vary the speed of the propeller or the blower to obtain the desired thrust, without modifying that of the turbine, which is generally calibrated at its maximum continuous speed, or even, during landing, to reverse this thrust thus replacing conventional heavy and complex reverse thrust systems.
Les dispositifs de commande de variation de pas d'hélice ou de soufflante sont des actionneurs hydrauliques (vérins entraînant chacun des pieds d'aubes) qui procurent la force nécessaire pour orienter les aubes dans la position désirée. Un tel dispositif de commande est par exemple décrit dans le document
Chaque aube à calage variable comporte un pivot cylindrique à chacune de ses extrémités, ces pivots définissant l'axe de rotation de l'aube.Each variable-pitch blade has a cylindrical pivot at each of its ends, these pivots defining the axis of rotation of the blade.
Le pivot radialement externe de l'aube est engagé dans une cheminée cylindrique d'un carter annulaire externe qui est relié au moyen d'une biellette à un anneau de commande monté autour du carter annulaire. L'anneau de commande est quant à lui relié par un levier à un arbre de commande actionné par un vérin hydraulique. De façon générale, l'arbre de commande s'étend parallèlement à l'axe du carter et peut être relié à un ou plusieurs anneaux de façon à commander un ou plusieurs étages d'aubes avec un seul vérin.The radially outer pivot of the blade is engaged in a chimney cylindrical outer annular casing which is connected by means of a rod to a control ring mounted around the annular housing. The control ring is connected by a lever to a control shaft actuated by a hydraulic cylinder. In general, the control shaft extends parallel to the axis of the housing and can be connected to one or more rings so as to control one or more stages of blades with a single cylinder.
La tige du vérin hydraulique est reliée à l'arbre de commande par un bras radial solidaire de l'arbre de commande provoquant, par déplacement linéaire de la tige du vérin, la rotation de chacun des anneaux autour du carter. La rotation d'un anneau de commande est transmise par les billettes correspondantes aux pivots externes des aubes d'un étage les faisant tourner autour de leurs axes.The hydraulic cylinder rod is connected to the control shaft by a radial arm integral with the control shaft causing, by linear displacement of the cylinder rod, the rotation of each of the rings around the housing. The rotation of a control ring is transmitted by the corresponding billets to the outer pivots of the blades of a stage rotating them about their axes.
La tige du vérin comporte à son extrémité une chape permettant d'assurer une liaison avec une rotule formant l'extrémité du bras radial solidaire de l'arbre de commande. La liaison entre la chape et la rotule est assurée au moyen d'une liaison vis-écrou.The rod of the jack has at its end a yoke for ensuring a connection with a ball joint forming the end of the radial arm integral with the control shaft. The connection between the yoke and the ball joint is ensured by means of a screw-nut connection.
En fonction des contraintes de volume et d'architecture de la soufflante, il arrive que l'environnement proche du vérin hydraulique n'offre que le volume nécessaire à l'écrou ainsi qu'à sa cinématique lors du fonctionnement du vérin hydraulique. Ce volume n'est par conséquent pas suffisant pour pouvoir installer, positionner, ou encore maintenir correctement l'écrou lors des opérations de montage ou démontage du vérin hydraulique par exemple lors des opérations de maintenance.Depending on the constraints of volume and architecture of the fan, it happens that the environment close to the hydraulic cylinder offers only the volume required for the nut and its kinematics during operation of the hydraulic cylinder. This volume is therefore not sufficient to install, position, or maintain the nut correctly during assembly or disassembly of the hydraulic cylinder for example during maintenance operations.
Ainsi, durant les opérations de manutention du vérin hydraulique, l'opérateur se trouve dans la nécessité de démonter différentes pièces avoisinantes afin de libérer un espace suffisamment important pour que l'opérateur puisse accéder à l'écrou de la liaison vis-écrou et ainsi pouvoir le manipuler et le démonter aisément.Thus, during the handling operations of the hydraulic cylinder, the operator is in the need to dismantle different neighboring parts in order to free a space large enough for the operator to access the nut of the screw-nut connection and thus be able to handle and dismount it easily.
Dans ce contexte, l'invention vise à résoudre les problèmes mentionnés ci-dessus, en proposant un dispositif hydraulique de changement de pas d'aubes permettant d'assurer un montage et/ou un démontage rapide du dispositif, par exemple lors d'une opération de maintenance, tout en s'affranchissant du démontage d'autres pièces avoisinantes.In this context, the invention aims to solve the problems mentioned above, by proposing a hydraulic blade pitch change device to ensure rapid assembly and / or disassembly of the device, for example during a maintenance operation, while avoiding the dismantling of other neighboring rooms.
A cette fin, l'invention propose un dispositif hydraulique de changement de pas d'hélice comportant une tige de piston actionnée par un fluide hydraulique, ladite tige de piston comportant à son extrémité une chape apte à assurer une liaison pour la transmission des mouvements de ladite tige de piston en vue d'un changement de pas d'au moins une hélice, ledit dispositif hydraulique étant caractérisé en ce qu'il comporte un écrou fileté maintenu en position sur ladite chape de ladite tige de piston par des moyens de maintien formés par la coopération d'une platine métallique solidaire dudit écrou fileté et d'une bague métallique solidaire de ladite chape comportant des moyens élastiques aptes à recevoir et à maintenir en position ladite platine métallique par clipsage, ledit écrou étant apte à coopérer avec une tige filetée pour réaliser une liaison.To this end, the invention proposes a hydraulic device for changing the pitch of a helix comprising a piston rod actuated by a hydraulic fluid, said piston rod comprising at its end a clevis adapted to provide a connection for the transmission of the movements of said piston rod for a pitch change of at least one helix, said hydraulic device being characterized in that it comprises a threaded nut held in position on said yoke of said piston rod by shaped holding means by the cooperation of a metal plate secured to said threaded nut and a metal ring integral with said yoke comprising elastic means able to receive and hold said metal plate in position by clipping, said nut being able to cooperate with a threaded rod to make a connection.
Grâce à l'invention, le démontage du vérin hydraulique, par exemple lors d'une opération de manutention, est réalisé rapidement par simple dévissage de la tige filetée permettant de désolidariser le vérin hydraulique de l'arbre de commande. Le démontage du vérin est réalisé sans démontage d'autres pièces avoisinantes malgré une architecture complexe n'autorisant pas un accès à l'écrou de serrage de la liaison vis-écrou.Thanks to the invention, the disassembly of the hydraulic cylinder, for example during a handling operation, is achieved quickly by simply unscrewing the threaded rod to separate the hydraulic cylinder from the control shaft. Disassembly of the cylinder is achieved without disassembly of other neighboring parts despite a complex architecture does not allow access to the clamping nut of the screw-nut connection.
Le dispositif hydraulique de changement de pas d'hélice selon l'invention peut également présenter une ou plusieurs des caractéristiques ci-dessous, considérées individuellement ou selon toutes les combinaisons techniquement possibles
- ledit écrou fileté est un écrou auto-freinant ;
- ladite bague métallique est une bague à encoches ;
- lesdits moyens élastiques sont formés par des pattes élastiques comportant chacune au moins une encoche ;
- ladite platine métallique comporte des protubérances aptes à coopérer avec lesdites encoches desdites pattes élastiques par clipsage ou par agrafage ;
- ledit dispositif comporte des moyens pour bloquer la rotation de ladite bague à encoches par rapport à ladite chape ;
- ledit écrou fileté comporte deux pattes faisant saillies radialement par rapport à l'axe de rotation dudit écrou fileté aptes à coopérer avec deux ouvertures agencées dans ladite platine métallique ;
- ledit sous-ensemble formé par ladite platine métallique et par ledit écrou fileté comporte des moyens pour bloquer la rotation dudit sous-ensemble par rapport à ladite bague à encoches ;
- ledit dispositif hydraulique est apte au changement de pas d'aubes à calage variable de soufflante de turbomachine.
- said threaded nut is a self-braking nut;
- said metal ring is a ring with notches;
- said elastic means are formed by resilient tabs each having at least one notch;
- said metal plate has protuberances adapted to cooperate with said notches of said elastic tabs by clipping or stapling;
- said device comprises means for blocking the rotation of said notched ring with respect to said yoke;
- said threaded nut comprises two tabs projecting radially with respect to the axis of rotation of said threaded nut adapted to cooperate with two openings arranged in said metal plate;
- said subassembly formed by said metal plate and said threaded nut comprises means for locking the rotation of said subassembly with respect to said notched ring;
- said hydraulic device is adapted to changing the pitch of variable-speed turbine engine fan blades.
L'invention a également pour objet un dispositif de commande de changement de pas d'hélice comportant un dispositif hydraulique de changement de pas selon l'invention.The invention also relates to a propeller pitch change control device comprising a hydraulic step change device according to the invention.
D'autres caractéristiques et avantages de l'invention ressortiront plus clairement de la description qui en est donnée ci-dessous, à titre indicatif et nullement limitatif, en référence aux figures annexées, parmi lesquelles :
- la
figure 1 est une vue en perspective d'une tige d'un dispositif hydraulique de changement de pas d'aubes à calage variable selon un premier exemple de réalisation de l'invention ; - la
figure 2 est une vue en perspective de la tige de piston illustrée à lafigure 1 solidarisée à un arbre de commande d'un dispositif de commande ; - la
figure 3 est une vue éclatée d'un écrou prisonnier solidarisée sur la tige de piston illustrée à lafigure 1 : - la
figure 4 est une vue en perspective d'une tige de piston d'un dispositif hydraulique de changement de pas d'aubes à calage variable selon un deuxième exemple de réalisation.
- the
figure 1 is a perspective view of a rod of a hydraulic variable pitch pitch changing device according to a first embodiment of the invention; - the
figure 2 is a perspective view of the piston rod illustrated in FIG.figure 1 secured to a control shaft of a control device; - the
figure 3 is an exploded view of a prisoner nut secured to the piston rod shown in thefigure 1 : - the
figure 4 is a perspective view of a piston rod of a hydraulic variable pitch pitch change device according to a second embodiment.
Dans toutes les figures, les éléments communs portent les mêmes numéros de référence sauf précision contraire.In all the figures, the common elements bear the same reference numbers unless otherwise specified.
La
De façon connue, le vérin hydraulique 100 est formé par un corps 10 et par une tige de piston 20 actionnée par la pression d'un fluide hydraulique circulant à l'intérieur du corps 10 du vérin 100.In known manner, the
La tige de piston 20 comporte à son extrémité libre une chape 30 sensiblement en forme de U qui est destinée à être reliée à l'arbre de commande via un bras radial solidaire de l'arbre de commande provoquant, par déplacement linéaire de la tige 20 du vérin, la rotation indirecte des aubes de la soufflantes.The
La chape 30 comporte deux orifices 32 coaxiaux traversant de part et d'autre les branches du U de la chape 30. L'espace 33 formé entre les deux branches du U est destiné à recevoir l'extrémité d'un bras radial 50 de l'arbre de commande, appelé rotule, tel qu'illustré à la
Sur la face extérieure de la branche supérieure du U illustrée à la
Les moyens de maintien 40 sont formés par :
- une platine métallique 42 formée à partir d'une tôle métallique et rendu solidaire à l'écrou fileté 41 par pliage ;
- une bague métallique 43 comportant des moyens élastiques 44 aptes à maintenir en position la platine métallique 42 par agrafage ou par clipsage.
- a
metal plate 42 formed from a metal sheet and secured to the threadednut 41 by folding; - a
metal ring 43 comprising elastic means 44 able to hold themetal plate 42 in position by stapling or clipping.
Tel qu'illustré à la
La bague métallique 43 est solidarisée sur la chape en forme de U par exemple par frettage de la bague de sertissage 46 dans l'orifice 32 de la branche supérieure du U de la chape 30.The
Selon le premier mode de réalisation de l'invention illustré à la
La platine métallique 42 est formée à partir d'une tôle métallique plane de forme sensiblement rectangulaire comportant deux ouvertures, par exemple de forme rectangulaire et disposées de façon parallèle.The
L'écrou 41 comporte un partie supérieure filetée et une base sur laquelle deux pattes 45 font saillies radialement par rapport à l'axe de rotation de l'écrou 41, la forme des pattes 45 étant complémentaires de la forme des ouvertures de la platine métallique 42.The
La platine métallique 42 est rendue solidaire de l'écrou 41 par pliage des bords latéraux de la tôle métallique de part et d'autre de l'écrou et de sorte que les pattes 45 faisant saillies traversent les deux ouvertures de la platine métallique 42. Ainsi, la platine métallique 42 est solidaire des mouvements de l'écrou fileté 41.The
La platine métallique 42 comporte également des protubérances 49 aptes à coopérer avec les pattes élastiques 44 de la bague métallique et plus précisément avec les encoches 48 des pattes élastiques 44.The
Ainsi, le sous-ensemble formé par l'écrou 41 et la platine 42 est inséré dans la bague métallique 43, solidaire de la chape, jusqu'à l'introduction des protubérances de la platine métallique 42 dans les encoches 48 des pattes élastiques 44.Thus, the subassembly formed by the
Les protubérances 49 de la platine métallique 42 et les encoches 48 correspondantes peuvent être de tailles et de formes différentes à partir du moment où elles réalisent une fonction de clipsage ou d'agrafage entre la platine 42 et la bague 43.The
Bien entendu, le sous-ensemble platine-écrou peut être désolidarisé de la bague métallique 43, et plus particulièrement des pattes élastiques 44, au moyen d'un outil spécifique permettant d'écarter suffisamment les pattes élastiques 44 pour désengager les protubérances 49 des encoches 48.Of course, the platen-nut subassembly can be detached from the
Ainsi, l'écrou 41 est rendu imperdable, maintenu en position sur la chape 30 tout en garantissant un certain jeu de fonctionnement entre le sous-ensemble et la bague métallique 43. Le jeu de fonctionnement permet ainsi de placer précisément l'écrou 41, par auto-centrage, en fonction de la position de la tige filetée et ainsi pouvoir réaliser la fonction de vissage entre l'écrou et la tige filetée. En effet, la tige filetée est une tige calibrée qui permet de supprimer les jeux dans les orifices 32 de la chape 30.Thus, the
A cet effet, l'orifice 32 de la branche inférieure du U comporte une bague 31 dont le diamètre est également calibré pour recevoir la tige filetée calibrée (non représentée).For this purpose, the
Une fonction supplémentaire d'anti-rotation est assurée entre le sous-ensemble platine-écrou et la bague métallique 43 par positionnement entre deux pattes élastiques 44 de la bague métallique 43 les pattes 45 faisant saillies. Ainsi la rotation du sous-ensemble platine-écrou est bloquée d'une part par les moyens élastiques et d'autre part par l'espacement des pattes élastiques 44 autorisant le passage des pattes 45 faisant saillies et formant des butées latérales.An additional function of anti-rotation is provided between the platen-nut subassembly and the
La
Dans ce deuxième exemple de réalisation, la fonction anti-rotation de la bague métallique 143 par rapport à la chape 30 est réalisée par la géométrie particulière de la bague métallique 143.In this second embodiment, the anti-rotation function of the
A cet effet, la bague métallique 143 comporte une excroissance de matière au niveau de sa base 147 de façon à déborder de la face d'appui de la chape 30. Au niveau de cette excroissance de matière, la bague métallique 143 comporte une protubérance 150 faisant saillie et dirigée vers l'intérieur de la chape 30 apte à bloquer tout déplacement par rotation de la bague métallique 143 par rapport à la chape 30.For this purpose, the
L'invention a été principalement décrite pour un dispositif hydraulique de changement de pas d'aubes à calage variable de soufflante de turbomachine ; toutefois, l'invention est également applicable à tout système muni d'hélices tel que les éoliennes, les ventilateurs industriels ou encore les turboréacteurs.The invention has been mainly described for a hydraulic device for changing the pitch of blades with variable turbine engine fan timing; however, the invention is also applicable to any system with propellers such as wind turbines, industrial fans or turbojets.
Les autres avantages de l'invention sont notamment les suivants :
- réduction des coûts de réalisation ;
- réduction du temps de réalisation ;
- simplification de la gamme de fabrication ;
- réduction des coûts des outillages ;
- réduction des coûts matière.
- reduction of implementation costs;
- reduction of the production time;
- simplification of the manufacturing range;
- reduction of tooling costs;
- material cost reduction.
Claims (10)
- Hydraulic device (100) for changing a propeller pitch comprising a piston rod (20) actuated by a hydraulic fluid, said piston rod (20) comprising a clevis (30) at its end to form a connection for the transmission of movements of said piston rod (20) in order to change the pitch of at least one propeller, said hydraulic device being characterised in that it comprises a threaded nut (41) held in position on said clevis (30) of said piston rod (20) by retaining means (40) formed by the cooperation of a metal plate (42) fixed to said threaded nut (41) and a metal ring (43) fixed to said clevis (30) comprising elastic means (44) that can hold and retain said metallic plate (42) in place by clip fitting, said threated nut (41) being designed to cooperate with a threaded rod to make a connection.
- Hydraulic device (100) for changing a propeller pitch according to claim 1, characterised in that said threaded nut (41) is a self-locking nut.
- Hydraulic device (100) for changing a propeller pitch according to either claim 1 or 2, characterised in that the metal ring (43) is a notched ring (48).
- Hydraulic device (100) for changing a propeller pitch according to one of claims 1 to 3, characterised in that said elastic means are formed from elastic tabs (44) each comprising a notch (48).
- Hydraulic device (100) for changing a propeller pitch according to claim 4, characterised in that said metallic plate (42) comprises protuberances (49) capable of cooperating with said notches (48) of said elastic tabs (44) by clip fitting.
- Hydraulic device (100) for changing a propeller pitch according to one of claims 1 to 5, characterised in that it comprises means (34,150) for blocking the rotation of said notched ring (43) relative to said clevis (30).
- Hydraulic device (100) for changing a propeller pitch according to one of claims 1 to 6, characterised in that said threaded nut (41) comprises two tabs (45) projecting radially from the rotation centre-line of said threaded nut (41) and capable of cooperating with two openings formed in said metal plate (42).
- Hydraulic device (100) for changing a propeller pitch according to one of claims 1 to 7, characterised in that the sub-assembly formed by said metallic plate (42) and by said threaded nut (41) comprises means (45) for blocking rotation of said sub-assembly relative to said notched ring (43).
- Hydraulic device (100) for changing a propeller pitch according to one of claims 1 to 8, characterised in that said hydraulic device (100) is capable of changing the pitch of variable-pitch blades in a turbomachine fan.
- Control device for changing a propeller pitch, characterised in that it comprises a hydraulic device (100) according to one of claims 1 to 9.
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1058594A FR2966426B1 (en) | 2010-10-21 | 2010-10-21 | HYDRAULIC DEVICE FOR CHANGING PROPELLER PITCH |
PCT/FR2011/052290 WO2012052649A1 (en) | 2010-10-21 | 2011-09-30 | Hydraulic device for changing the pitch of a propeller |
Publications (2)
Publication Number | Publication Date |
---|---|
EP2630335A1 EP2630335A1 (en) | 2013-08-28 |
EP2630335B1 true EP2630335B1 (en) | 2017-01-04 |
Family
ID=44080263
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP11779773.8A Active EP2630335B1 (en) | 2010-10-21 | 2011-09-30 | Hydraulic device for changing the pitch of a propeller |
Country Status (8)
Country | Link |
---|---|
US (1) | US9879552B2 (en) |
EP (1) | EP2630335B1 (en) |
CN (1) | CN103210183B (en) |
BR (1) | BR112013009848A2 (en) |
CA (1) | CA2815337A1 (en) |
FR (1) | FR2966426B1 (en) |
RU (1) | RU2013123058A (en) |
WO (1) | WO2012052649A1 (en) |
Families Citing this family (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2992696B1 (en) * | 2012-06-28 | 2015-04-10 | Eurocopter France | HYDRAULIC DISPENSER, DEVICE FOR ADJUSTING BLADE PITCH, AIRCRAFT PROVIDED WITH SUCH A HYDRAULIC DISPENSER |
FR3046408B1 (en) * | 2016-01-05 | 2018-02-09 | Safran Aircraft Engines | DEVICE FOR LOCKING THE FLAGS AND FLOWING BLADES OF REGULATLY ORIENTED BLOWER BLADES OF A TURBOMACHINE PROPELLER |
CN106938695B (en) * | 2017-01-19 | 2023-08-15 | 飞灵智控(北京)科技有限公司 | Rotor hub and unmanned helicopter |
CN114962328B (en) * | 2022-07-25 | 2023-01-06 | 沈阳鼓风机集团股份有限公司 | Axial-flow type main driving compressor for continuous wind tunnel device |
Family Cites Families (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4790701A (en) * | 1987-05-08 | 1988-12-13 | Jacobson Mfg. Co., Inc. | Floating fastener retainer assembly with removable fasteners |
FR2794801B1 (en) * | 1999-06-10 | 2001-07-06 | Snecma | PROTECTIVE DEVICE FOR THE CONTROL MECHANISM OF THE SHUTTERS OF A TURBOEACTOR INPUT STEERING WHEEL |
US6692177B2 (en) * | 2001-02-26 | 2004-02-17 | The Torrington Company | Steering shaft retaining clip |
AU2003903902A0 (en) * | 2003-07-25 | 2003-08-07 | Aimbridge Pty Ltd | Marine propulsion system |
FR2911644B1 (en) * | 2007-01-23 | 2012-06-01 | Snecma | TURBOPROPULSEUR COMPRISING A PROPELLED PROPELLER OF BLADES WITH ADJUSTABLE ORIENTATION. |
FR2928979B1 (en) * | 2008-03-19 | 2015-05-01 | Snecma | DEVICE FOR CONTROLLING AUBES WITH VARIABLE TIMING IN A TURBOMACHINE. |
CA2667849A1 (en) * | 2008-06-10 | 2009-12-10 | Mitsubishi Heavy Industries, Ltd. | Blade pitch-angle control apparatus and wind turbine generator |
FR2937678B1 (en) * | 2008-10-23 | 2013-11-22 | Snecma | DEVICE FOR CONTROLLING THE ORIENTATION OF BLOWER BLADES OF A TURBOPROPULSEUR |
-
2010
- 2010-10-21 FR FR1058594A patent/FR2966426B1/en active Active
-
2011
- 2011-09-30 WO PCT/FR2011/052290 patent/WO2012052649A1/en active Application Filing
- 2011-09-30 CN CN201180055101.3A patent/CN103210183B/en active Active
- 2011-09-30 RU RU2013123058/06A patent/RU2013123058A/en not_active Application Discontinuation
- 2011-09-30 US US13/880,621 patent/US9879552B2/en active Active
- 2011-09-30 BR BR112013009848A patent/BR112013009848A2/en not_active IP Right Cessation
- 2011-09-30 EP EP11779773.8A patent/EP2630335B1/en active Active
- 2011-09-30 CA CA2815337A patent/CA2815337A1/en not_active Abandoned
Non-Patent Citations (1)
Title |
---|
None * |
Also Published As
Publication number | Publication date |
---|---|
FR2966426B1 (en) | 2012-12-07 |
EP2630335A1 (en) | 2013-08-28 |
CA2815337A1 (en) | 2012-04-26 |
RU2013123058A (en) | 2014-11-27 |
US20130199167A1 (en) | 2013-08-08 |
WO2012052649A1 (en) | 2012-04-26 |
CN103210183B (en) | 2015-11-25 |
US9879552B2 (en) | 2018-01-30 |
FR2966426A1 (en) | 2012-04-27 |
CN103210183A (en) | 2013-07-17 |
BR112013009848A2 (en) | 2016-07-26 |
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