WO2013124617A1 - Ensemble amortisseur - Google Patents
Ensemble amortisseur Download PDFInfo
- Publication number
- WO2013124617A1 WO2013124617A1 PCT/GB2013/050262 GB2013050262W WO2013124617A1 WO 2013124617 A1 WO2013124617 A1 WO 2013124617A1 GB 2013050262 W GB2013050262 W GB 2013050262W WO 2013124617 A1 WO2013124617 A1 WO 2013124617A1
- Authority
- WO
- WIPO (PCT)
- Prior art keywords
- damper
- damper assembly
- assembly according
- impact surface
- mass
- 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.)
- Ceased
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16F—SPRINGS; SHOCK-ABSORBERS; MEANS FOR DAMPING VIBRATION
- F16F7/00—Vibration-dampers; Shock-absorbers
- F16F7/10—Vibration-dampers; Shock-absorbers using inertia effect
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16F—SPRINGS; SHOCK-ABSORBERS; MEANS FOR DAMPING VIBRATION
- F16F7/00—Vibration-dampers; Shock-absorbers
- F16F7/10—Vibration-dampers; Shock-absorbers using inertia effect
- F16F7/104—Vibration-dampers; Shock-absorbers using inertia effect the inertia member being resiliently mounted
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16F—SPRINGS; SHOCK-ABSORBERS; MEANS FOR DAMPING VIBRATION
- F16F7/00—Vibration-dampers; Shock-absorbers
- F16F7/10—Vibration-dampers; Shock-absorbers using inertia effect
- F16F7/104—Vibration-dampers; Shock-absorbers using inertia effect the inertia member being resiliently mounted
- F16F7/116—Vibration-dampers; Shock-absorbers using inertia effect the inertia member being resiliently mounted on metal springs
Definitions
- the present invention relates to a damper assembly for reducing the kinetic energy of a moving body, to apparatus including such an assembly and to a method of using such a damper assembly.
- the damper assembly may be used progressively to
- Such an assembly may form part of reciprocating apparatus, such as, for example, high speed linear or rotary action actuators.
- the damper assembly may also be used progressively to accelerate a second body via the progressive deceleration of the first body .
- the operating stresses imparted on the components controlled by the actuators due to the rapid accelerations and decelerations as a result of initiation of movement, or arrest of movement, especially where the latter are by travel limiting stops, may reduce longevity, or, may produce undesirable rebound.
- the present invention provides a damper assembly
- the assembly comprising an impact surface, and at least one damper mass for damping the motion of a body, wherein the assembly is configured such that, in use, when a body approaches the impact surface it collides with the at least one damper mass in an initial position to cause the at least one damper mass to bounce back and forth between the impact surface and the body undergoing a series of collisions with the moving body that decelerate the body.
- the damper assembly may include as part of the mechanism a body configured to approach the impact surface.
- series of collisions it is meant at least two collisions with the moving body that progressively reduce its kinetic energy.
- the collisions may involve a single damper mass bouncing back and forth between the impact surface and the approaching body, or, may involve a plurality of damper masses moving back and forth between the impact surface and the approaching body; in the latter case, one mass may only travel a short distance and may only collide with other masses, for example, but the combined effect will again be successive momentum transfer between the approaching body and the impact surface.
- the plurality of damper masses may be configured (for example, constrained) to move in a co- ordinated fashion, or to move in a random fashion or to move in parallel, or, in series (i.e. colliding with one another successively so as to transfer the momentum across from the moving body to the impact surface) , or any combination thereof, providing that they undergo the required series of collisions.
- deceleration occurs in stages as a result of the series of collisions of the body with the at least one damper mass, rather than in one single abrupt deceleration.
- sufficient strain energy must be imparted to the damper mass by impact with the body to result in separation of the body and the damper mass.
- the damper mass will then travel ahead of the body towards the impact surface where strain energy will again be stored in the damper mass as a result of the collision with the impact surface.
- Some strain energy is also imparted to the impact surface and is attenuated through the supporting structure.
- the present damper assembly may be implemented in
- the damping mechanism is illustrated in a graph in
- Body B is accelerated towards the stop by an external force.
- Body B undergoes a first collision at point Ci, after which damper mass D moves towards the impact surface faster than body B, whose momentum has now been reduced.
- Damper mass D collides with the impact surface at and the stored strain energy is then released causing it to reverse its direction, moving back towards the body B where it collides again with it at point C 2 .
- the body B is thus decelerated relative to the impact surface by successive momentum transfer to the damper mass D.
- the damper mass transfers this momentum to the impact surface and, although the total momentum of the body, the body of which the impact surface is a part and the damper mass is maintained, the relative momentum of the body to the impact surface is reduced by dissipation through multiple damper mass
- the impact surface may be configured to remain
- stationary during the damping, and may be provided upon a second body that is stationary (e.g. static or fixed), or that is free to move (in which case it may gradually
- the assembly is configured such that the series of collisions involve a single damper mass.
- This may be a baton, ball, puck or any suitable robust, smooth, preferably outwardly curved object likely to provide a good rebound (i.e. required dynamic hardness), and could be suspended or anchored or tethered or the like; it could also be an elongate self-supporting (e.g. pivotally hung) element, e.g. a rod, cylinder or resilient cantilever.
- the assembly is configured such that the series of collisions involve multiple damper masses bouncing back and forth (e.g. partially or fully) between the impact surface and the moving body.
- the multiple damper masses may be arranged to act in series and/or in parallel.
- the multiple dampers may comprise a plurality of rounded damper masses
- such multiple dampers may be a series of successively aligned, closely spaced damper masses disposed between the body and impact surface and capable of
- the masses may comprise individual damper masses arranged and constrained to move in a line or in an arc, for linear or rotary damping, respectively.
- the damper masses may be freely movable or may be anchored (e.g. to restrain their respective paths of movement) to respective anchor points, or to a common anchor point, or may be anchored to one another, and the anchoring connections may be resilient or rigid and may be single or paired connections.
- the multiple dampers may comprise masses constrained for movement in a line via elements such as rigid or resilient or flexible, usually elongate, elements, which may be anchored as above.
- the multiple dampers may also comprise masses constrained for movement in an arc via attachments to the ends of such elements (e.g. leaf springs) including being suspended from such elements (e.g. inelastic cable, wires or the like) .
- the multiple dampers may comprise a series of adjacent cantilevers pivotally hinged at a common hinge point (e.g. moving in an arc like leaves of a book) .
- Such dampers may employ both percussive damping and gas damping, whereby gas is forced out of the leaves as they rotate relative to one another, providing an additional damping effect.
- the damper assembly may be used in applications where a moving body needs to be brought to a temporary (e.g.
- the damper assembly is a one-shot device.
- the damper assembly may be installed as a protective one-off device in vehicles to assist in
- the damper assembly may also be used to accelerate a second body (via the deceleration of the first moving body) , and this may be as a one-off device to assist in launching a vulnerable projectile or, for example, an aircraft ejector seat.
- the damper assembly is a re-usable (i.e. multi-shot) device.
- the damper assembly includes a reset mechanism configured to reposition the at least one damper mass in the initial position for re ⁇ use. This mechanism may or may not include additional
- the mechanism may enable the at least one damper to damp the same body or a further body.
- the at least one damper mass may be moving or stationary when the moving body collides with it in the initial position (at a selected proximity to the impact surface) .
- the at least one damper mass may be a free body, for example, one dropped into, or launched as a
- the damper assembly is configured such that the movement of the at least one damper mass is constrained to follow a selected path, which may be a linear or rotary path.
- the damper mass may be constrained by virtue of one or more (e.g. a matched pair of) restraints, which may be a resilient restraint or flexible restraint or a rigid but movable restraint; a resilient restraint may be capable of flexing, stretching or otherwise deforming out of its equilibrium position and subsequently returning to that position.
- the restraint may also act as the reset mechanism.
- the restraint may be anchored to a fixed or movable body, which may include, for example, another damper (that could for example be acting in a corresponding matched (e.g. symmetrical) role.
- a damper may be supported upon one end of a resilient restraint (e.g. leaf spring), or a pair of matched dampers may be attached to either end of the restraint, where the latter is, for example, confined within a channel, groove, bore, ring, or similar partly or fully encircling device.
- the action (e.g. flexing) of the restraint needs to be sufficiently light as to allow the damper mass to undergo the required energy damping collisions, the purpose of the restraint (e.g. spring or cantilever) being primarily an anchoring or confining function so as to ensure the damper mass remains positioned between the body and surface.
- the restraint e.g. spring or cantilever
- the damper assembly is configured such that the damper is reset in the initial position by virtue of its motion being constrained with respect to the moving body.
- the damper may be carried by the body and/or may at least partially or fully encircle the body or otherwise be constrained with respect to the body.
- the damper assembly will usually be configured to operate in air or other gaseous environment.
- the damper assembly will tolerate variations in gas pressure, although extremely high gas pressures may lead to some viscous damping which may lead to reduced percussive damping.
- the moving body will form part of apparatus in which the body is forced to undergo controlled movements, including rapid accelerations from rest, or rapid
- the damper assembly may form part of robotic apparatus, machining apparatus, valve-controlled apparatus or other apparatus involving repetitive (and often fast) controlled movements of controlled components, usually in combination with an actuator or similar assembly. It is especially beneficial for use in unlubricated actuated machinery (i.e. where lubrication is undesirable) , such as, for example, unlubricated weaving apparatus or food production apparatus.
- the present damper assembly has the advantage that this percussive mechanism can react within fast time frames, as opposed to some alternative damper mechanisms, for example, certain viscose dampers, which operate in too slow a time frame for use in these applications. Furthermore, the present damper assembly is remarkably tolerant of speed variations. During tests, it was found that even when the speed of the moving body is changed quite significantly, roughly the same number of collisions will still occur, but they will merely happen in a shorter or longer time frame (i.e. if the body speed is doubled, the form of the damping curve of Fig 5 above remains the same, but damping takes place in a shorter time frame) .
- the present damper assembly may also be
- bearings for example, can be self-lubricating
- the damper assembly may form part of, or be operatively linked to, an actuator assembly e.g. a reciprocating linear or rotary actuator.
- the moving body may be part of an actuator assembly e.g. a reciprocating linear or rotary actuator.
- actuator arm where its motion requires damping, or more usually a component carried by the actuator, for example, a framework supporting an object which is the subject of the desired actuated movement (e.g. a movable valve plate), or a component carried by or connected to the object, in
- the present damper assembly is of especial application where a component carried by the actuator is delicate and should be protected from rapid accelerations or decelerations.
- Applicant's earlier application WO2009/074800 describes a valve including a flexible valve plate whose movement may be controlled by an actuator and in which apparatus the valve plate kick-off's and/or halts may be damped by incorporation of the present damper assembly.
- the moving body forms part of
- the damper assembly may be provided in apparatus as a single action damper that only damps the deceleration of a moving body when it moves in one direction i.e. at one extent of its motion.
- a door that is opened and closed may only require a single action damper to damp the closing action.
- a further example would be pivotally connected arms, where the pivot joint itself requires damping to slow the closing of the arms to subtend the smallest angle.
- the damper assembly could be used to assist in initiating the opening of such a joint, where the pivot joint is a second body gradually accelerated by the gradual deceleration of a first moving body. More usually, a fast moving body will be undergoing a back and forth motion that requires damping at both extents of its motion.
- This may be linear or rotary reciprocating movement (e.g. a valve such as a linear or rotary (slide) valve or plate valve) .
- the moving body may form part of apparatus in which the body follows a reciprocating path, and the damper assembly may be a double action damper assembly so configured as to provide damping at each end of the
- a separate respective damper and separate respective impact surface may be provided at each end of the stroke, or a common damper and/or a common impact surface may be provided for both ends.
- the damper may be disposed inwardly of the impact surface.
- the damper assembly comprises a common damper mass. This may be carried by the moving body and so configured as to damp the motion of the moving body at each end of its reciprocating stroke.
- the common damper mass may be a collar loosely fitted around the moving body. The collar may be held within the plane of motion of the body; it may comprise inwardly disposed (facing), forward and rear striking surfaces against which the element collides during its forward and rearward reciprocating movement,
- the striking surfaces are preferably convex and preferably made of a material with the required rebound (or dynamic) hardness (i.e. requisite elastic stiffness) .
- the damper assembly comprises a pivotally supported damper provided with two damper arms, optionally pivotally supported at, or near to (for example, hung from), its centre of percussion.
- the centre of percussion of a pin-supported object is a point on it where a perpendicular impact at a location remote from that point will produce no reaction force at the pivot point, hence causing the least wear and tear at the pivot point.
- the damper assembly is preferably configured so that a collision of the at least one damper with the body and/or a collision of the at least one damper with the impact surface involves at least one convex surface. This may conveniently be achieved using a damper mass having an outwardly curved surface or surfaces; normally, the impact surface will be flat. Preferably, none of the collisions involve the collision of two flat surfaces.
- the number of collisions of the at least one damper mass with the approaching body is at least 2, and may be at least 3, at least 5, or at least 10, or in the range of at least 3 to 6, or in the range of at least 7 to 10.
- the damper mass may be configured to store the strain energy remotely from the impact points.
- the assembly may be selectively configured so that the
- the assembly can be adjusted to operate in different time frames depending on the required responsivity and may be employed to provide effective damping in very short time frames.
- the number of collisions may be limited by a further mechanism; this may involve the use of an intermediate stop surface.
- the damper assembly may further
- intermediate stop surface may be arranged outwardly of the line of movement of the at least one damper mass.
- the intermediate stop surface may comprise a continuous flat surface with an inset cavity having an end wall at the far end of the cavity comprising the impact surface against which the damper mass impacts; in this case, the cavity may be an elongate cavity and the damper mass an elongate rod, wherein the rod is not as long as the cavity.
- the length of the rod (and hence cavity) may be selected to secure sufficient damping; a longer rod is better at storing strain energy and will give a more vigorous bounce.
- the impact surface may comprise a continuous flat surface, while the intermediate stop surface comprises one or a plurality of bodies partially or fully encircling the path of the oscillating damper mass and disposed in the path of the approaching body.
- the damper assembly comprises a secondary damping mechanism. This can attenuate energy within the damper mass and hence reduce bounce.
- Such a secondary damping mechanism may comprise a single impact damper (e.g. a ball bearing loosely mounted in a cavity) or a plurality of impact dampers, and these may be incorporated within or attached to the body of the at least one damper.
- a single impact damper e.g. a ball bearing loosely mounted in a cavity
- a plurality of impact dampers e.g. a ball bearing loosely mounted in a cavity
- the damping mechanism may comprise a gas damping mechanism.
- a multiple damper arrangement may comprise a set of adjacent cantilevers capable of both impacting one another for percussive damping, where gas damping between the leaves attenuates the energy of the multiple damper to reduce bounce.
- the properties and arrangement of the components in the assembly should be selectively configured, that is, they should be intentionally selected so as to ensure that at least two collisions occur, thereby progressively damping the motion of the moving body.
- the factors are of course
- the mass of the damper relative to that of the moving body is not more than 1:2, preferably, not more than 1:4, or 1:10.
- the momentum (mass x velocity) exchange during the collision will ensure the damper will move away quickly enough to bounce off the impact surface and return for at least one further momentum exchanging collision.
- the damper assembly may be employed in applications where the impact surface is movable e.g. provided upon a body that is free to move.
- the impact surface may be part of a second body and the collisions of the one or more dampers with the impact surface may result, via the deceleration of the first moving body, in the progressive acceleration of the second body away from the moving body, as opposed to a single abrupt initiation.
- the above damper assembly configured gradually to accelerate a second body, usually at rest, away from a first moving body.
- the assembly could comprise a first moving body in the form of a
- controlled striking device i.e. just initially controlled until the first impact or fully controlled
- Such an arrangement may be re-usable, and may for example initiate movement of a second body that is, for example, itself undergoing reciprocating movement. More usually, such a progressive acceleration application will be in a one-off device, for example, to assist in launching a projectile or, for example, an aircraft ejector seat, where reduced ejection forces can mitigate spinal column trauma .
- the present invention further provides apparatus
- damper assembly comprising a damper assembly as above
- apparatus may comprise robotic apparatus, machining apparatus, valve- controlling apparatus or other apparatus involving singular or repetitive, single action or double action, controlled movements of components, and may optionally comprise an actuator assembly.
- the present invention further provides a method of decelerating a body using at least one damper mass and an impact surface together configured in a damper assembly, the method comprising: -
- the present invention also provides a damper assembly comprising an impact surface, a body configured to approach the impact surface, and at least one damper mass for damping the motion of the body, wherein the assembly is configured such that as the body approaches the impact surface it collides with the at least one damper mass in an initial position to cause the at least one damper mass to bounce back and forth between the impact surface and the approaching body undergoing a series of collisions with the body that
- a damper assembly to damp the motion of a moving body as it approaches an impact surface
- the damper assembly comprises the impact surface and at least one damper mass
- the damper assembly is configured such that as the body approaches the impact surface it collides with the at least one damper mass in an initial position to cause the at least one damper mass to bounce back and forth between the impact surface and the approaching body undergoing a series of collisions with the body that
- the use of the present damper assembly progressively to decelerate and/or halt a moving body, or, progressively to accelerate a second body on which the impact surface is disposed.
- the use may be in apparatus in which the moving body is undergoing
- the present invention further provides any novel and inventive combination of the above mentioned features which the skilled person would understand as being capable to being combined.
- any feature disclosed in respect of a single action damper may usually also be employed for a double action or multiple action damper.
- Fig.l is a schematic plan view of a single action damper assembly according to the invention.
- Figs. 2a and 2b are, respectively, schematic perspective and side views of a double action damper assembly according to the invention.
- Fig. 3 is a schematic plan view of a double action, multiple damper assembly according to the invention.
- Figure 4 is a schematic perspective view of a further double action, multiple damper assembly according to the invention.
- Figure 5 is a graph showing the separation distances x of the body and damper mass from the impact surface of the damper assembly of Figure 1, respectively, as they undergo the multiple collisions;
- Figure 6 is a perspective schematic view of a further double action, damper assembly according to the invention.
- FIG. 7 illustrates Steps 1 to 10 showing the operation of the damper assembly according to Figure 6;
- Figure 8 is a schematic side view of a single action damper assembly configured gradually to accelerate a second body away from a first moving body;
- Figure 9 shows, as Steps 1 to 3, the operation of a single action damper in which the maximum number of
- Figure 10 is a graph similar to that of Figure 5 showing the separation distances x of the body and damper mass from the impact surface in the damper assembly of Figure 9 as they undergo the multiple collisions;
- Figures 11a and lib are, respectively, a front view and transverse sectional view of a double action damper assembly according to the invention with a secondary damper mechanism, while Figure 11c is a front view of a similar double action damper assembly; and,
- Figures 12a to d show schematic side views of various damper assemblies with different arrangements of damper masses .
- one factor for progressive damping to occur is that the body needs to approach the impact surface with sufficient kinetic energy to trigger the series of collisions of the at least one damper back and forth between the moving body and the impact surface (i.e. too slow an approach will not result in multiple collisions), that is to say, a body of a particular mass should have a selected minimum velocity, if all factors remain unchanged.
- Another factor which may be important for damping to occur is that, at the moment of the initial collision, the at least one damper should be disposed in a selected position
- FIG. 1 shows a plan view of a damping mechanism according to the invention for damping the arrest of a door 3 against a wall 5.
- the mechanism 1
- a damper mass 7 in the form of a hard rubber ball 7 resiliently supported on the end of a leaf spring 15 attached to the wall 5, the ball being selectively positioned across the entrance to a cavity 11 inset into the wall.
- the end wall of the cavity is provided with an impact surface in the form of a striker block 9, and the door 3 with a similar striker block 13.
- this percussive damping mechanism acts to dampen the arrest of the door body in a controlled and progressive manner reducing the wear and noise as compared with an uncontrolled impact.
- the anchoring allows the ball to be reset in its initial position after use.
- the configuration of the damper mechanism and choice of components should be appropriately selected.
- the material of the ball and the blocks should be selected to have a suitable co-efficient of restitution (i.e. springiness or stiffness)
- the ball should be sufficiently light in mass to accelerate away and ahead of the door
- the ball should be appropriately anchored in a position suitably spaced close to the wall and the leaf spring or other similar resilient anchoring member should not significantly impede the ball but rather allow it to move and collide relatively freely.
- Reciprocating arm 22 forms part of a structure that supports the slide valve (not shown) and has twin forks 26 provided with opposed striking surfaces 24 which would normally impact against objects such as static stops to halt the arm's movement. In this case, however, the stops have been replaced by a double action damper mechanism to achieve a gradual deceleration.
- the damper mechanism comprises a single, common damper mass in the form of a hard, solid, cylindrical puck 28. This is constrained by a leaf spring 30 to travel in an arc bouncing back and forth between impact surfaces 32a-32d of fixed common curved bracket assembly 34 and the moving twin forks 26.
- the bracket assembly has upper arms 36 and lower arms 38 and the cylindrical puck damper 28 extends beyond the upper and lower arms in length, as may be seen in Fig. 2b, so that when the damper bounces off the upper and lower arms on one side of the bracket 34, it receives balanced angular forces about its centre of mass 40 (point of attachment) .
- the reciprocating arm 22 reciprocates linearly back and forth within a plane of motion between the upper and lower arms, as may also be seen in Fig.
- the damper puck 28 will be bouncing back and forth between impact surfaces 32a/32b and one fork 26' reducing the kinetic energy of the arm, and at the other end of the arm' s stroke between impact surfaces 32c/32d and the other fork 26.
- Figure 3 shows a schematic plan view of a double action, multiple damper assembly 50 intended to damp the rotary reciprocations of a controlled actuator arm 52.
- damping is achieved using a separate multi-puck
- Figure 4 is a schematic perspective view of a further double action, multiple damper assembly 60.
- Arm 62 is part of an actuator frame and undergoes rapid reciprocations more or less linearly to the left and right.
- the end of the arm is secured to a common damper in the form of a resilient cantilever 64, whose length and resilience allows the arm freely to reciprocate.
- damper 64 impacts against respective multidamper arrangements 66 and 66, each comprising shorter multi- cantilevered arms 68.
- two damping mechanisms slow the arm 62 which is particularly effective.
- the arm is decelerated by successive impacts of the adjacent flexing leaves of the shorter multi-cantilevered arms 68, and there is secondary gas damping as gas is forced out from the adjacent leaves thereby attenuating the energy in those leaves.
- Figure 6 is a further double action damper assembly 70 forming part of an actuator assembly that is supporting a slide valve (not shown) .
- Moving actuator frame 72 reciprocates linearly to and fro and includes arm 74 extending perpendicular to the line of motion which extends through a rectangular aperture 76 in slideway 78.
- arm 74 extending perpendicular to the line of motion which extends through a rectangular aperture 76 in slideway 78.
- rectangular collar 80 mounted upon the arm 74 is rectangular collar 80, which acts as a common damper for both ends of the reciprocating strokes, sliding along the slideway 78 in a plane of motion perpendicular to the arm 74 and colliding with the separate impact surfaces of static abutments 82, 82' and arm 74 so as to decelerate the arm, as described in more detail with respect to Figure 7 below.
- the 8 respective striking surfaces involved in the decelerating collisions are as follows:
- Steps 1 to 10 illustrate the operation as follows :- 1 - Actuator Arm 74 (Moving body) is pressed against Collar 80 (Common Damper) which is pressed against abutment 82', both at a temporary halt;
- Collar 80 collides in 2nd Impact C 2 at its internal striking surface F with strike surface E of Arm 74 and the exchange of momentum causes Collar 80 to reverse its
- Figure 8 is an example of a single action, one-shot damper assembly configured gradually to accelerate a second body away from a first moving body.
- Assembly 90 is an ejector assembly for an aircraft ejector seat and propellant or rocket device or charge 92 acts as the moving body.
- a damper mass 94 is centrally suspended in a selected initial stationary position directly above the charge 92 by means of a plurality of radially extending, sacrificial tethers 96 designed to snap easily upon rapid movement of the damper mass 94.
- the releasable ejector seat 96 is disposed directly above the damper mass 94 and includes a reinforced impact surface 100 on its underside .
- Activation of the charge 92 causes it to be propelled towards the damper mass 94, which immediately snaps its tethers upon the collision and accelerates towards the impact surface 100.
- the damper mass 94 then bounces back and forth between the impact surface 100 and the still approaching charge 92 undergoing multiple collisions that result in successive momentum transfer from the charge 92 to the ejector seat 96 before the charge itself impacts the ejector seat 96 in a softened impact.
- the progressive acceleration of the ejector seat 96 due to the damping mechanism mitigates the effect of the main impact, thereby minimising the risk of a spinal column trauma n the passenger.
- Figure 9 shows Steps 1 to 3 of the operation of a single action, one-shot damper assembly in which the number of collisions is limited, or rather, the action of the damper assembly per se is restricted.
- the assembly comprises moving body B, damper mass comprising a metal rod D and an elongate cavity C extending within and perpendicular to surface S. Cavity C is longer in length than rod D and is provided at its far end with impact surface I.
- Such an assembly could be part of a protective device for damping the deceleration of vehicle component B before it impacts surface S during a vehicle accident.
- Step 1 Moving body B collides in collision Ci with end A of damper rod D causing momentum transfer to the rod which bounces away towards inset cavity C where its other end Z collides with the inset impact surface I.
- Step 2 - The assembly is configured such that the rod D bounces back out of the cavity C to undergo a second
- Step 3 Damper rod D enters the cavity
- Figure 10 is a graph similar to that of Figure 5 showing the separation distances x of the body B and end A of damper mass D from the impact surface as they undergo the multiple collisions of Steps 1 to 3.
- Figure 11a depicts a further double action damper assembly according to the invention, with additional damper mechanisms to attenuate the energy within the damper mass.
- Damper assembly 110 comprises a common damper 111 comprising a pivotally hung, fork shaped body 111 having two respective damper arms 112 and 112'.
- the moving body comprises moving actuator arm 114 supported (not shown) for rotary (or linear) reciprocation back and forth between impact surfaces of stops 116 and 116' .
- the fork shaped body 111 is pivotally hung at, or close to, its centre of percussion 120 so as to minimise wear and tear at the pivot point.
- the pivot bearing is also a self- lubricating, graphite bearing, with the result that the fork shaped body 111 is tuned to swing very freely. This is ideal for longevity but can lead to an excessive number of
- the fork shaped body 111 incorporates a single impact damper 118 offset from the pivot point, in this case, directly above the pivot point; this may be a ball bearing confined in a cavity against which it strikes during reciprocation to dissipate some of the kinetic energy in the body 111.
- the ends of the damper arms 112, 112' are receivable within slightly larger cavities (Fig. lib) that curtail damping by limiting the number of collisions, so that actuator arm 114 eventually collides with stops 116, 116'.
- Fig. 11c shows a slightly modified arrangement, where multiple impact dampers 118 are provided above the pivot point 120 for more aggressive attenuation of the kinetic energy.
- the stiffness (springiness) of the damper limbs may be adjusted by changing the necking 122 of the limbs, as shown in Fig. 11c, for even further fine tuning. (In this way, more energy may be stored in a single collision for subsequent attenuation by the ball dampers.)
- Figures 12a and b respectively show multiple dampers D arranged in series and parallel prior to undergoing damping collisions between moving body B and impact surface I. They could be individually tethered or tethered to each other, and, if initially stationary, could be configured for simple linear movement in parallel lines of motion.
- Figure 12c shows multiple dampers D arranged randomly prior to undergoing damping collisions between moving body B and impact surface I. They could be individually tethered or tethered to each other (e.g. by 2D or 3D net), and, if initially stationary, could be configured for simple linear movement in parallel lines of motion.
- Figure 12d shows a single damper arrangement whereby a free damper mass D is used, and is projected into the space between the moving body B and impact surface I in order to provide damping, its resulting zigzagging motion after collisions being unpredictable and random.
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Vibration Dampers (AREA)
- Manipulator (AREA)
- Chutes (AREA)
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB1203070.6 | 2012-02-22 | ||
| GB1203070.6A GB2499621A (en) | 2012-02-22 | 2012-02-22 | A damper assembly |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| WO2013124617A1 true WO2013124617A1 (fr) | 2013-08-29 |
Family
ID=45940033
Family Applications (2)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| PCT/GB2013/050264 Ceased WO2013124619A1 (fr) | 2012-02-22 | 2013-02-05 | Ensemble à dispositifs d'amortissement multiples |
| PCT/GB2013/050262 Ceased WO2013124617A1 (fr) | 2012-02-22 | 2013-02-05 | Ensemble amortisseur |
Family Applications Before (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| PCT/GB2013/050264 Ceased WO2013124619A1 (fr) | 2012-02-22 | 2013-02-05 | Ensemble à dispositifs d'amortissement multiples |
Country Status (2)
| Country | Link |
|---|---|
| GB (2) | GB2499621A (fr) |
| WO (2) | WO2013124619A1 (fr) |
Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2520937A (en) * | 1949-05-19 | 1950-09-05 | Jr Dwight C Kennard | Spring and vibration damper therefor |
| GB2163233A (en) * | 1984-08-13 | 1986-02-19 | Westinghouse Electric Corp | Multiple-impact shock absorbing means for circuit interrupter and other apparatus |
| US4698470A (en) * | 1986-05-22 | 1987-10-06 | Westinghouse Electric Corp. | Multiple-impact shock-absorbing assembly for circuit interrupter and other apparatus |
| WO2009074800A1 (fr) | 2007-12-11 | 2009-06-18 | Isentropic Limited | Vanne |
Family Cites Families (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP4421851B2 (ja) * | 2003-08-20 | 2010-02-24 | 本田技研工業株式会社 | ダイナミックダンパ |
| JP2008281141A (ja) * | 2007-05-11 | 2008-11-20 | Shinko Electric Co Ltd | 電磁ブレーキ及び電磁クラッチ |
| FR2948431B1 (fr) * | 2009-07-21 | 2011-06-24 | Eurocopter France | Revetement isolant a masse amplifiee |
-
2012
- 2012-02-22 GB GB1203070.6A patent/GB2499621A/en not_active Withdrawn
-
2013
- 2013-02-05 GB GB1414209.5A patent/GB2517840A/en not_active Withdrawn
- 2013-02-05 WO PCT/GB2013/050264 patent/WO2013124619A1/fr not_active Ceased
- 2013-02-05 WO PCT/GB2013/050262 patent/WO2013124617A1/fr not_active Ceased
Patent Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2520937A (en) * | 1949-05-19 | 1950-09-05 | Jr Dwight C Kennard | Spring and vibration damper therefor |
| GB2163233A (en) * | 1984-08-13 | 1986-02-19 | Westinghouse Electric Corp | Multiple-impact shock absorbing means for circuit interrupter and other apparatus |
| US4698470A (en) * | 1986-05-22 | 1987-10-06 | Westinghouse Electric Corp. | Multiple-impact shock-absorbing assembly for circuit interrupter and other apparatus |
| WO2009074800A1 (fr) | 2007-12-11 | 2009-06-18 | Isentropic Limited | Vanne |
Also Published As
| Publication number | Publication date |
|---|---|
| WO2013124619A1 (fr) | 2013-08-29 |
| GB201203070D0 (en) | 2012-04-04 |
| GB2517840A (en) | 2015-03-04 |
| GB2499621A (en) | 2013-08-28 |
| GB201414209D0 (en) | 2014-09-24 |
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