NZ713668A - A system, method of use and Self Retracting Lifeline (SRL) apparatus - Google Patents
A system, method of use and Self Retracting Lifeline (SRL) apparatus Download PDFInfo
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- NZ713668A NZ713668A NZ713668A NZ71366814A NZ713668A NZ 713668 A NZ713668 A NZ 713668A NZ 713668 A NZ713668 A NZ 713668A NZ 71366814 A NZ71366814 A NZ 71366814A NZ 713668 A NZ713668 A NZ 713668A
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- 238000005859 coupling reaction Methods 0.000 claims description 47
- 230000001133 acceleration Effects 0.000 claims description 21
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- 230000009471 action Effects 0.000 claims description 18
- 230000036461 convulsion Effects 0.000 claims description 15
- 238000006073 displacement reaction Methods 0.000 claims description 12
- 230000001360 synchronised effect Effects 0.000 claims description 9
- 230000003534 oscillatory effect Effects 0.000 claims description 4
- 238000006243 chemical reaction Methods 0.000 claims description 2
- 230000007246 mechanism Effects 0.000 abstract description 10
- 230000003993 interaction Effects 0.000 abstract description 8
- 230000008901 benefit Effects 0.000 abstract description 4
- 230000008859 change Effects 0.000 description 11
- 230000010355 oscillation Effects 0.000 description 4
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- 239000006096 absorbing agent Substances 0.000 description 2
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- 238000001514 detection method Methods 0.000 description 2
- 230000005484 gravity Effects 0.000 description 2
- 238000000926 separation method Methods 0.000 description 2
- 230000003213 activating effect Effects 0.000 description 1
- 230000004913 activation Effects 0.000 description 1
- 238000007792 addition Methods 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
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Abstract
Described herein is a system, method of use and Self Retracting Lifeline (SRL) apparatus using the system that govern a dynamic response between members causing a halt in relative motion between the members. Magnetic interactions, eddy current drag forces and centrifugal and/or inertial forces may provide various mechanisms of governing movement. The invention relates to a coupler configured to selectively couple a spool to an external member, where the coupler includes a pawl linked to the spool. The spool is rotatable within an external member and when the spool rotates below a speed threshold, the pawl oscillates and the coupler does not couple to spool to the external member. When the spool rotates above a speed threshold, the pawl of the coupler moves to a deployed position such that the pawl couples the spool to the external member. The advantage of the invention is that it achieves movement control beyond the reliance on centrifugal and/or eddy current forces alone.
Description
LATCH ACTIVATION BETWEEN ELEMENTS
TECHNICAL FIELD
Described herein is a system, method of use and Self Retracting Lifeline (SRL) apparatus using the
system to control relative speed between members.
BACKGROUND ART
The applicant’s co-pending and granted patents in the field of eddy current related devices include US
8,851,235, US 8,490,751, NZ619034, NZ627617, NZ627619, NZ627633, NZ627630 and other equivalents
all incorporated herein by reference. NZ627617 in particular, describes a method of achieving a latch
operation between elements the contents of which are incorporated herein by reference. While the
devices described in NZ627617 may be useful, other methods of controlling relative movement and/or
braking may also be achieved or at least provide the public with a choice.
Further aspects and advantages of the system, method of use and Self Retracting Lifeline (SRL)
apparatus should become apparent from the ensuing description that is given by way of example only.
SUMMARY
Described herein is a system, method of use and Self Retracting Lifeline (SRL) apparatus using the
system that govern a dynamic response between members causing a halt in relative motion between
the members. Magnetic interactions, eddy current drag forces and centrifugal and/or inertial forces
may provide various mechanisms of governing movement.
In a first aspect, there is provided a system with at least two members in a kinematic relationship, the
system comprising a means of coupling a first member to at least one further member and in doing so
causing synchronised relative motion between the members, wherein coupling occurs in response to a
prescribed system dynamic response, the dynamic response selected from at least one of:
(a) a particular velocity action of one or more of the members;
(b) a particular acceleration action of one or more of the elements;
(c) a particular jerk action of one or more of the elements.
In a second aspect, there is provided a method of governing relative movement between members by
the steps of:
(a) selecting the system substantially as described herein;
(b) applying a motive force on the system causing movement of at least one member in the system;
(c) causing coupling between the members when the prescribed system dynamic response occurs.
In a third aspect, there is provided a Self Retracting Lifeline (SRL) incorporating the system substantially
as described herein.
The system, method of use and SRL device described offer the advantage of providing alternative ways
of achieving movement control or at least provide the public with a choice.
BRIEF DESCRIPTION OF THE DRAWINGS
Further aspects of the system, method of use and SRL device will become apparent from the following
description that is given by way of example only and with reference to the accompanying drawings in
which:
Figure 1 illustrates a simplified elevation view of one embodiment of incorporating a magnetic
interaction between a braking and moving element;
Figure 2 illustrates a simplified elevation view of an alternative bi-stable embodiment;
Figure 3 illustrates a graph showing the magnetic force interaction for the above bi-stable
embodiment;
Figure 4 illustrates a perspective view and elevation view of an alternative embodiment
employing a cogging torque approach;
Figure 5 illustrates two graphs showing the velocity dependent result from the cogging torque
approach;
Figure 6 illustrates a simplified elevation view of a cogging torque approach of a barking and
moving element;
Figure 7 illustrates a simplified elevation view of an alternative embodiment utilising a
rotational degree of freedom;
Figure 8 illustrates elevation views of alternative cam path embodiments;
Figure 9 illustrates elevation views of alternative cam path embodiments;
Figure 10 illustrates perspective views of alternative cam path embodiments;
Figure 11 illustrates a simplified perspective view of an alternative cam path embodiment;
Figure 12 illustrates simplified perspective and elevation views of an alternative cam path
embodiment;
Figure 13 illustrates a simplified elevation view of an alternative cam path embodiment;
Figure 14 illustrates various elevation views of an alternative embodiment using a combination
of a cam, geometry, inertial response and eddy current;
Figure 15 illustrates a simplified elevation view of an art velocity sensitive device using pawls;
Figure 16 illustrates a simplified elevation view of an art acceleration sensitive device using
pawls;
Figure 17 illustrates a simplified elevation view of a jerk sensitive device;
Figure 18 illustrates a simplified elevation view of the jerk sensitive device of Figure 17 in a
varying alignment;
Figure 19 illustrates a simplified elevation views of the magnetic interaction from the
embodiment of Figures 17 and 18; and
Figure 20 illustrates a simplified elevation view of an alternative jerk sensitive device.
DETAILED DESCRIPTION
As noted above, described herein is a system, method of use and Self Retracting Lifeline (SRL) apparatus
using the system that govern a dynamic response between members causing a halt in relative motion
between the members. Magnetic interactions, eddy current drag forces and centrifugal and/or inertial
forces may provide various mechanisms of governing movement.
For the purposes of this specification, the term ‘about’ or ‘approximately’ and grammatical variations
thereof mean a quantity, level, degree, value, number, frequency, percentage, dimension, size, amount,
weight or length that varies by as much as 30, 25, 20, 15, 10, 9, 8, 7, 6, 5, 4, 3, 2, or 1% to a reference
quantity, level, degree, value, number, frequency, percentage, dimension, size, amount, weight or
length.
The term ‘substantially’ or grammatical variations thereof refers to at least about 50%, for example 75%,
85%, 95% or 98%.
The term 'comprise' and grammatical variations thereof shall have an inclusive meaning - i.e. that it will
be taken to mean an inclusion of not only the listed components it directly references, but also other
non-specified components or elements.
The term ‘jerk’ or grammatical variations thereof refers to a change in acceleration, typically a rapid and
sudden change in acceleration compared to normal operating parameters.
In a first aspect, there is provided a system with at least two members in a kinematic relationship, the
system comprising a means of coupling a first member to at least one further member and in doing so
causing synchronised relative motion between the members, wherein coupling occurs in response to a
prescribed system dynamic response, the dynamic response selected from at least one of:
(a) a particular velocity action of one or more of the members;
(b) a particular acceleration action of one or more of the elements;
(c) a particular jerk action of one or more of the elements.
The inventors have in effect produced a system relating to coupling members together based on the
system dynamic response. The aim is to bring the members into synchronised motion under
predetermined conditions.
Coupling between the members may be achieved:
(a) mechanically;
(b) magnetically;
(c) a combination of mechanically and magnetically.
Coupling may occur passively and once coupled the members may be remain coupled or may be
releasably coupled. Coupling may instead be achieved via an active means.
The synchronised motion may be a zero absolute velocity or halting effect. This effect for example may
be useful where all motion needs to stop, for example in a fall safety apparatus.
Coupling may also be based on, or at least influenced by, eddy current induced drag. This is not essential
in the inventors experience but may be useful to further tune the dynamic response characteristics.
In one specific embodiment, coupling between the members may be achieved via mechanical coupling
between at least one pawl linked to the first member, the pawl having an oscillatory movement action,
and at least one latch member on, or being, the at least one further member, coupling occurring at a
speed threshold according to the prescribed system dynamic response.
A bias relationship may exist between the pawl and the latch member, the bias being achieved through
use of at least one magnet arranged for attraction, repulsion, or alternating attraction and repulsion, of
the pawl.
At least one magnetic element may be located on both the pawl and first member and when rotation of
the pawl and first member occurs, a varying bias results and hence oscillatory pawl movement occurs.
The pawl may be axially mounted on the first member and the pawl centre of gravity may be off set
from the pawl axis of rotation thereby further influencing the oscillation effect.
As may be appreciated, the degree of oscillation of the pawl may be varied depending for example on
the relative rates of motion of the first member and pawl (or first member and at least one further
member.
The pawl dynamic response may be further tuned by varying the inertia of the pawl. As noted above,
the centre of mass of the pawl may be off set from the pawl axis of rotation assuming the pawl is
connected in this manner to the first member. A part or parts of the pawl may be weighted so as to
tune the inertia of the pawl to movement thereby tuning the dynamic response of the system.
The system may act as follows:
(a) at a predetermined speed, coupling may occur when the pawl moves to a deployed position for
a sufficient time period such that it couples with the latch member; and
(b) at speeds below the predetermined speed, the pawl may not couple.
Coupling may be avoided by having the pawl skip over the latch member – that is the pawl may not be
sufficiently deployed to interfere with the latch member. Skipping over may continue until the inertial
effects of the pawl are overcome and the pawl deploys sufficiently far to couple with the latch member.
The system may further act so that:
(a) the pawl may remain coupled when the speed of motion is insufficient to overcome the inertial
effects of the pawl; and
(b) decoupling may occur when the speed of motion is sufficient to overcome the inertial effects of
the pawl.
The degree of bias noted above causing oscillation may be configured to provide the desired dynamic
response behaviour of the pawl.
In an alternative specific embodiment, coupling between the members may be achieved by a mechanical
cam system based on the reaction effects of inertial forces and/or applied drag forces according to the
prescribed system dynamic response.
In the above system, the first and at least one further member may be aligned together and the cam
feature may be located between the first and at least one further member. In effect, the system has at
least two independent but moving members.
The at least one further member may be configured with either or both of inertial characteristics and/or
retarding drag due to motion such that it is subject to a slowed motion with respect to the first member
when a motive force is applied on the system.
Relative velocity between the first and at least one further member may provide a displacement
between the members and may urge the members to separate due to the cam profile prescribed
movement path. Separation refers to the members moving apart with respect to each other.
Movement of the at least one further member may cause coupling with a latch member on or about the
first member, coupling at least one anchor on the at least one further member to the latch member.
As may be appreciated, coupling of the further member to the latch member also results in coupling
indirectly between the first and further member.
Coupling may be achieved via:
(a) a geometric latching interface;
(b) attraction of magnetic poles; or
(c) a combination of a geometric latching interface and attraction of magnetic poles.
In a further specific embodiment, coupling may rely on magnetic forces between the members wherein
the magnetic forces between the members are configured to achieve an attraction force between the
members, the attraction force being sufficient to slow and halt relative motion between the members
resulting in synchronised relative motion according to the prescribed system dynamic response.
The magnetic forces may be imposed by magnetic pole elements acting between the members. For the
purposes of this specification, magnetic pole action is termed ‘cogging’. The cogging system may be
designed in consideration of the dynamic behaviour of the connected system and any peripheral energy
absorbing means such that the system achieves a stop and hold action under the intended conditions.
The magnetic pole elements may be configured to be ineffective or inactive under predetermined
conditions. Variation in magnetic pole action may for example be achieved by varying the separation
distance between members or parts thereof containing the magnet or magnets thereby reducing the
magnetic interaction forces.
The system above may be a continuously coupled system where an externally applied motive force
results in initial movement of the members, but a slow and halt action takes effect immediately
between the members provided the motive force is sufficient to induce the prescribed system dynamic
response.
As may be appreciated, in the first aspect above and the specific embodiments described, the members
may move in a substantially linear kinematic relationship. Alternatively, the members may move in a
substantially rotational kinematic relationship. Both actions may be possible and appropriate depending
on the device in which the system may be used. Examples given or used herein are described in the
rotational embodiment. Linear equivalent embodiments will be obvious to someone skilled in the art.
In a yet further specific embodiment, the members may be in a substantially rotational kinematic
relationship and coupling between the members may be achieved via a centrifugal based system
designed so that, on application of a motive force of a predetermined magnitude, the members couple
together according to the prescribed system dynamic response.
The centrifugal forces acting on the members may be influenced by use of at least one weight or
weighted element or part thereof.
The first and at least one further member may be aligned together and the centrifugal feature or
features may be located between the first and at least one further member.
Velocity of the members may urge a displacement of the centrifugal feature or features which in turn
urges the members to separate due to the centrifugal force imposed on the at least one further
member.
Movement of the at least one further member may cause coupling with a latch member on or about the
first member, coupling at least one anchor of the at least one further member to the latch member. As
may be appreciated, coupling of the further member to the latch member also results in coupling
indirectly between the first and further member.
Coupling may be achieved via:
(a) a geometric latching interface;
(b) attraction of magnetic poles; or
(c) a combination of a geometric latching interface and attraction of magnetic poles.
As noted above, the dynamic response may be in one of three ways. In more detail, specific examples of
how the three actions might take place may be as follows:
- A velocity sensitive device may be configured using pawls that are activated by centripetal
forces acting against the constraint of a biasing element;
- An acceleration sensitive device may make use of the inertial behaviour of a pawl causing
rotation of the pawl about its pivot in response to acceleration of the pawl mounting plate;
- A jerk sensitive device may be configured by making use of the non-linear shear force capacity
that exists between a pair of magnetic poles.
As should be appreciated, the configuration may be varied and the above options should be seen as
non-limiting examples only.
In a second aspect, there is provided a method of governing relative movement between members by
the steps of:
(a) selecting the system substantially as described herein;
(b) applying a motive force on the system causing movement of at least one member in the system;
(c) causing coupling between the members when the prescribed system dynamic response occurs.
In a third aspect, there is provided a Self Retracting Lifeline (SRL) incorporating the system substantially
as described herein.
As noted above, the devices described may be used in SRL devices. The ability to detect and activate a
braking element is important for SRL apparatus.
Detection of a fall event is commonly triggered by a mechanism that responds to a change in state of
the line. Mechanisms can potentially be triggered by the displacement, velocity, acceleration or jerk
(rate of change of acceleration) of the line, or by a combination of these signals.
Existing SRLs commonly make use of velocity or acceleration mechanisms, typically using a ratchet and
pawl arrangement to couple the spool to a brake. Either the ratchet plate or the pawl set can be
attached to the rotating spool.
A linear configuration may comprise a means of sensing a change in acceleration (jerk) of a carrier
(moving element). The carrier may be attached to a rider (braking element) of known mass with a given
inertia. When a contact force is applied to the carrier the rider and carrier remain coupled and aligned.
A change in the applied force to the carrier (jerk) causes the rider to slip relative to the carrier due to the
inertial effects. The inertial effects may then be tracked through displacement between the rider and
carrier. When the carrier acceleration changes, the relative displacement between the rider and carrier
also changes.
The same principle may be used in a rotational sense. The rider may be free to rotate with the carrier.
A change in angular acceleration applied to the carrier may be resolved as a relative angular
displacement between the carrier and rider.
Besides SRL applications, the devices and methods may be used for a variety of other applications, non-
limiting examples including speed control or load control of:
An autobelay device;
A rotor in a rotary turbine;
Exercise equipment e.g. rowing machines, epicyclic trainers, weight training equipment;
Roller-coasters and other amusement rides;
Elevator and escalator systems;
Evacuation descenders and fire escape devices;
Conveyer systems:
Rotary drives in factory production facilities;
Materials handling devices such as conveyer belts or a braking device in a chute;
Roadside safety systems e.g. the energy absorber may be connected in a system to provide
crash attenuation though the dissipation of energy via the energy absorber;
Seat belts in vehicles;
Zip lines;
Braking mechanisms for trolleys and carriages;
Bumpstops in transport applications;
Bumpstops in crane applications;
Torque or force limiting devices in mechanical drive train;
Structural overload protection in wind turbines;
Load limiting and energy dissipation in structures, buildings and bridges.
The system, method of use and SRL device described above offer the advantage of providing alternative
ways of achieving movement control beyond for example reliance on centrifugal and/or eddy current
forces alone. In addition, the relationship between the parts and the rate at which movement control
occurs may also be influenced using the embodiments described herein.
The embodiments described above may also be said broadly to consist in the parts, elements and
features referred to or indicated in the specification of the application, individually or collectively, and
any or all combinations of any two or more said parts, elements or features, and where specific integers
are mentioned herein which have known equivalents in the art to which the embodiments relate, such
known equivalents are deemed to be incorporated herein as of individually set forth.
Where specific integers are mentioned herein which have known equivalents in the art to which this
invention relates, such known equivalents are deemed to be incorporated herein as if individually set
forth.
WORKING EXAMPLES
The above described system, method of use and examples of Self Retracting Lifeline (SRL) apparatus
using the devices are now described by reference to specific examples.
EXAMPLE 1
General examples are provided below of magnetic latching caused by movement of a braking element.
Figure 1 illustrates an example of magnetic latching caused by movement of a pawl. Direct attractive
forces exerted by permanent magnets 10 may be used to either augment or replace eddy current drag
forces (if eddy current forces are used) as a means of activating a pawl 11 between the spool 12 (the
first member) and a concentric external element 13 (the further member). When the pawl 11 is latched
with the concentric external element 13, movement between the spool 12 and concentric external
element 13 is synchronised.
EXAMPLE 2
A bi-stable arrangement can be used in conjunction with a tube and cylinder (plunger) approach
described in the applicants co-pending application NZ619034. In this example, as illustrated in Figure 2,
a plunger 50 eddy current brake configuration is shown as a means of delaying the initial relative motion
between the active brake element/plunger 50 and the lead screw 51 and/or to latch and lock the brake
50 at the end of the plunger axial travel stroke 52, 53. The output in terms of force/movement
interaction is graphed in Figure 3 showing how the force at either end of the plunger stroke 52, 53 is
high and subsequently drops through the travel phase of the plunger stroke 52, 53 noting that the term
force refers to the force required to translate the plunger sideways and movement is the lateral
movement of the plunger.
EXAMPLE 3
In a further embodiment, a cogging example is illustrated in Figure 4. A cogging torque results from
magnetic poles rotating with respect to each other generally indicated by arrow 60. This results in a
speed-dependent torque relationship best seen in the graphs shown in Figure 5 where F refers to the
force/degree of oscillation and o refers to the movement path that can enable low-speed lock-off of a
brake that relies on eddy current braking (the highest latching force occurs at low speed).
Figure 6 shows how the magnets 60 align at low speed thereby halting further movement. This
embodiment allows a complete halt in relative movement between the parts but without part
interference or friction – that is braking is frictionless.
Figure 6 also illustrates a centrifugal embodiment. One of the members includes weighted balls that
move along a defined path. At maximum rotation force, the balls move to alter the centre of gravity
thereby changing the dynamic response of the system.
EXAMPLE 4
Magnetic latching of a braking element can also be configured about a rotational degree of freedom
normal to the primary drive axis, in this example being the rotation axis 70 of the braking element 71
relative to the moving element 72 (a rotor). Figure 7 illustrates three embodiments of this type of
system. Also shown in the Figure 7 embodiments is the use of a bias (magnets and/or springs) that
further tune the dynamic response of the system.
EXAMPLE 5
Relative rotation between the moving and braking elements may also be further influenced by use of
inertial or centrifugal forces resulting in differential velocity between the elements. In one
embodiment, a differential velocity may be used to drive an axial displacement via a cam path 100 as
illustrated in Figures 8 to 13. Different profiles can be used to control ball movement and thus alter the
centrifugal force acting on the parts and their movement characteristics.
The axial load required to maintain contact between the two halves in the embodiments shown in
Figures 8 to 13 may be generated by a spring force, a magnetic repulsive force or as a result of eddy
current drag torque acting through the cam 100 angle. Additional detail on this force generation is
shown in Figures 12 and 13.
EXAMPLE 6
Another arrangement that exploits the combination of cam geometry, inertial response and the eddy
current drag force-speed relationship is shown in Figure 14.
EXAMPLE 7
As noted above, the ability to detect and activate a braking element is important for SRL apparatus.
Detection of a fall event is commonly triggered by a mechanism that responds to a change in state of
the line. Mechanisms can potentially be triggered by the displacement, velocity, acceleration or jerk
(rate of change of acceleration) of the line, or by a combination of these signals.
Existing SRLs commonly make use of velocity or acceleration mechanisms, typically using a ratchet and
pawl arrangement to couple the spool to a brake. Either the ratchet plate or the pawl set can be
attached to the rotating spool.
An art velocity sensitive device can be configured using pawls (braking elements) 110 that are activated
by centripetal forces acting against the constraint of a biasing element (spring) 111 as illustrated in
Figure 15.
An art acceleration sensitive device can make use of the inertial behaviour of the pawl 112 causing
rotation of the pawl 112 about its pivot 113 in response to acceleration of the pawl 112 mounting plate.
This approach is illustrated in Figure 16.
EXAMPLE 8
A jerk sensitive device can be configured by making use of the non-linear shear force capacity that exists
between a pair of magnetic poles.
A linear configuration is illustrated in Figures 17 to 19. The configuration shows a means of sensing the
change in acceleration (jerk) of a carrier. The carrier 120 is attached to a rider 130 of known mass with a
given inertia. When a contact force is applied to the carrier 120 the rider 130 and carrier 120 remain
coupled and aligned. A change in the applied force to the carrier 120 (jerk) causes the rider 130 to slip
relative to the carrier 120 due to the inertial effects. The inertial effects may then be tracked through
displacement ‘d’. When the carrier 120 acceleration changes, the relative displacement between the
rider 130 and carrier 120 changes.
Aspects of the system, method of use and Self Retracting Lifeline (SRL) apparatus using the system have
been described by way of example only and it should be appreciated that modifications and additions
may be made thereto without departing from the scope of the claims herein.
WHAT WE
Claims (28)
1. A system with at least two members in a kinematic relationship, the system comprising a means of coupling a first member to at least one further member and in doing so causing synchronised relative motion between the members, wherein coupling occurs in response to a prescribed system dynamic response, the dynamic response selected from at least one of: (a) a particular velocity action of one or more of the members; (b) a particular acceleration action of one or more of the elements; (c) a particular jerk action of one or more of the elements.
2. The system as claimed in claim 1 wherein coupling between the members is achieved: (a) mechanically; (b) magnetically; (c) a combination of mechanically and magnetically.
3. The system as claimed in any one of the above claims wherein the synchronised motion is a zero absolute velocity or halting effect.
4. The system as claimed in any one of the above claims wherein coupling is also based on, or at least influenced by, eddy current induced drag.
5. The system as claimed in any one of the above claims wherein coupling between the members is achieved via mechanical coupling between at least one pawl linked to the first member, the pawl having an oscillatory movement action, and at least one latch member on, or being, the at least one further member, coupling occurring at a speed threshold according to the prescribed system dynamic response.
6. The system as claimed in claim 5 wherein a bias relationship exists between the pawl and the latch member the bias being achieved through use of at least one magnet arranged for attraction, repulsion, or alternating attraction and repulsion, of the pawl.
7. The system as claimed in claim 6 wherein at least one magnetic element is located on both the pawl and first member and when rotation of the pawl and first member occurs, a varying bias results and hence oscillatory pawl movement occurs.
8. The system as claimed in any one of claims 5 to 7 wherein the pawl dynamic response is further tuned by varying the inertia of the pawl.
9. The system as claimed in any one of claims 5 to 8 wherein: (a) at a predetermined speed, coupling occurs when the pawl moves to a deployed position for a sufficient time period such that it couples with the latch member; and (b) at speeds below the predetermined speed, the pawl does not couple. 10. The system as claimed in any one of claims 5 to 8 wherein: (a) the pawl remains coupled when the speed of motion is insufficient to overcome the inertial effects of the pawl; and (b) decoupling occurs when the speed of motion is sufficient to overcome the inertial effects of the pawl.
10. The system as claimed in any one of claims 1 to 4 wherein coupling between the members is achieved by a mechanical cam system based on the reaction effects of inertial forces and/or applied drag forces according to the prescribed system dynamic response.
11. The system as claimed in claim 10 wherein the first and at least one further member are aligned together and the cam feature is located between the first and at least one further member.
12. The system as claimed in claim 10 or claim 11 wherein relative velocity between the first and at least one further member provides a displacement between the members and urges the members to separate due to the cam profile prescribed movement path.
13. The system as claimed in any one of claims 10 to 12 wherein movement of the at least one further member causes coupling with a latch member on or about the first member, coupling at least one anchor on the at least one further member to the latch member.
14. The system as claimed in claim 13 wherein coupling is achieved via: (a) a geometric latching interface; (b) attraction of magnetic poles; or (c) a combination of a geometric latching interface and attraction of magnetic poles.
15. The device as claimed in any one of claims 1 to 4 wherein coupling relies on magnetic forces between the members wherein the magnetic forces between the members are configured to achieve an attraction force between the members, the attraction force being sufficient to slow and halt relative motion between the members resulting in synchronised relative motion according to the prescribed system dynamic response.
16. The system as claimed in claim 15 wherein the magnetic forces are imposed by magnetic pole elements acting between the members.
17. The system as claimed in claim 16 wherein the magnetic pole elements are configured to be ineffective or inactive under predetermined conditions.
18. The system as claimed in any one of claims 15 to 17 wherein the system is a continuously coupled system where an externally applied motive force results in initial movement of the members, but a slow and halt action takes effect immediately between the members provided the motive force is sufficient to induce the prescribed system dynamic response.
19. The system as claimed in any one of the above claims wherein the members move in a substantially linear kinematic relationship.
20. The system as claimed in any one of claims 1 to 18 wherein the members move in a substantially rotational kinematic relationship.
21. The device as claimed in any one of claims 1 to 4 wherein the members are in a substantially rotational kinematic relationship and coupling between the members is achieved via a centrifugal based system designed so that, on application of a motive force of a predetermined magnitude, the members couple together according to the prescribed system dynamic response.
22. The device as claimed in claim 21 wherein the centrifugal forces acting on the members are influenced by use of at least one weight or weighted element or part thereof.
23. The system as claimed in claim 21 or claim 22 wherein first and at least one further member are aligned together and the centrifugal feature or features are located between the first and at least one further member.
24. The system as claimed in any one of claims 21 to 23 wherein velocity of the members urge a displacement of the centrifugal feature or features which in turn urges the members to separate due to the centrifugal force imposed on the at least one further member.
25. The system as claimed in any one of claims 21 to 24 wherein movement of the at least one further member causes coupling with a latch member on or about the first member, coupling at least one mooring of the at least one further member to the latch member.
26. The system as claimed in claim 25 wherein coupling is achieved via: (a) a geometric latching interface; (b) attraction of magnetic poles; or (c) a combination of a geometric latching interface and attraction of magnetic poles.
27. A Self Retracting Lifeline (SRL) incorporating the system as claimed in any one of the above claims.
28. A method of governing relative movement between members by the steps of: (a) selecting the system as claimed in any one of claims 1 to 26 (b) applying a motive force on the system causing movement of at least one member in the system; (c) causing coupling between the members when the prescribed system dynamic response occurs.
Priority Applications (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
NZ770580A NZ770580A (en) | 2014-12-04 | 2014-12-04 | A method of controlling a self-retracting lifeline |
NZ713668A NZ713668A (en) | 2014-12-04 | 2014-12-04 | A system, method of use and Self Retracting Lifeline (SRL) apparatus |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
NZ713668A NZ713668A (en) | 2014-12-04 | 2014-12-04 | A system, method of use and Self Retracting Lifeline (SRL) apparatus |
Publications (1)
Publication Number | Publication Date |
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NZ713668A true NZ713668A (en) | 2022-10-28 |
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Family Applications (2)
Application Number | Title | Priority Date | Filing Date |
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NZ770580A NZ770580A (en) | 2014-12-04 | 2014-12-04 | A method of controlling a self-retracting lifeline |
NZ713668A NZ713668A (en) | 2014-12-04 | 2014-12-04 | A system, method of use and Self Retracting Lifeline (SRL) apparatus |
Family Applications Before (1)
Application Number | Title | Priority Date | Filing Date |
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NZ770580A NZ770580A (en) | 2014-12-04 | 2014-12-04 | A method of controlling a self-retracting lifeline |
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NZ (2) | NZ770580A (en) |
Families Citing this family (1)
Publication number | Priority date | Publication date | Assignee | Title |
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WO2024157284A1 (en) * | 2023-01-25 | 2024-08-02 | Pn International Private Limited | Wire brush assembly and method of replacing wire brush from self retracting lifeline |
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2014
- 2014-12-04 NZ NZ770580A patent/NZ770580A/en unknown
- 2014-12-04 NZ NZ713668A patent/NZ713668A/en unknown
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NZ770580A (en) | 2022-10-28 |
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Free format text: THE FILED DATE HAS BEEN CORRECTED TO 04/12/2014 Effective date: 20151209 |
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PSEA | Patent sealed | ||
RENW | Renewal (renewal fees accepted) |
Free format text: PATENT RENEWED FOR 1 YEAR UNTIL 04 DEC 2024 BY HOLMES SOLUTIONS LIMITED PARTNERSHIP Effective date: 20230908 |