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Sommaire du brevet 2157222 

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  • lorsque le brevet est émis (délivrance).
(12) Brevet: (11) CA 2157222
(54) Titre français: PLATE-FORME DE MAINTIEN AERIENNE A CINQ AXES DE MOUVEMENT
(54) Titre anglais: AERIAL SUPPORT PLATFORM MECHANISM WITH FIVE AXES OF MOTION
Statut: Périmé et au-delà du délai pour l’annulation
Données bibliographiques
Abrégés

Abrégé français

Cette invention concerne une plate-forme aérienne suspendue sous et entre une paire de câbles parallèles longeant respectivement un de deux murs opposés d'un studio. Un chariot circule sur chacun des câbles parallèles et une autre paire de câbles relient ces deux chariots l'un à l'autre. Un troisième chariot circule sur cette deuxième paire de câbles et supporte la plate-forme au moyen d'autres câbles verticaux. La paire de chariots circulant le long des deux murs opposés du studio se déplacent ensemble et le troisième chariot se déplace entre eux. La plate-forme peut également être élevée ou abaissée par rapport au troisième chariot; elle a donc trois degrés de liberté linéaire. Elle possède deux autres degrés de liberté, soit la rotation autour d'un axe vertical et la rotation autour d'un axe horizontal. La plate-forme est conçue pour recevoir du matériel cinématographique dont l'orientation peut être déterminé à distance à l'aide d'un ordinateur.


Abrégé anglais


An aerial support platform is supported to extend
below, and intermediate of, a pair of parallel cables
mounted along respective opposite walls of a studio. A
carriage rides on each of the parallel cables, and
another pair of cables extends to connect the pair of
carriages. A third carriage sits on the other pair of
cables, and a series of further cables extend vertically
from that carriage to the platform. The pair of
carriages positioned on the opposite walls of the studio
are controlled to move in tandem, and the third carriage
has controlled movement between those carriages. The
platform may be raised or lowered relative to the third
carriage, and thus has three linear axes of motion. The
platform has two additional axes of motion, both
rotational. One is around a vertical axis and another is
around an axis normal to the vertical axis.
Cinematographic equipment may be fixed to the platform,
which can then be oriented using a computer at a remote
location.

Revendications

Note : Les revendications sont présentées dans la langue officielle dans laquelle elles ont été soumises.


CLAIMS:
1. An aerial support mechanism for providing five
independently addressable degrees of axial freedom for a
camera, said mechanism comprising:
a pair of spaced parallel first cables supported at
both ends and supporting a pair of first carriages
therefrom, first movement means for movement of each of
said first carriages along said respective first cables;
a pair of transverse second cables extending between
and affixed to said pair of first carriages, for providing
laterally-directed tension to said first pair of cables by
way of said first carriages, said second cables terminating
at one of said first carriages and tensionably terminating
at the other first carriage;
a second carriage, said second carriage depending from
said second cables and having second movement means for
movement along said second cables;
a platform member, said platform member depending from
a set of third cables fixed to and extending from said
second carriage and terminating in third movement means
disposed on said platform member, said third movement means
for effecting movement of said platform member vertically
with respect to said second carriage;
said platform member further comprising a rotatably
mounted jointed means with a platform depending therefrom
for supporting a camera, said jointed means rotatable about
a horizontal axis by means of respective fourth movement
means, and said jointed means including a fifth movement
means to effect rotation of said platform about a vertical
axis; and
control means for remotely and independently
controlling the movement of each of the respective first,
second, third, fourth and fifth movement means.
2. A mechanism as in claim 1, wherein said second
platform is rotatably connected to said first platform by a
support element for rotation around a vertical first axis,

and wherein said support element is adapted to provide
rotation about an axis generally normal to said first axis.
3. A mechanism as in claim 1, wherein each first carriage
has wheel means riding on a respective first cable and
wherein said respective first movement means comprises a
first cable loop disposed generally parallel to said first
cables and extending between a first driven pulley and a
second pulley, said first pulley and said second pulley
located at opposite ends of said first cables, the first
cable loop starting from said first carriage and ending
thereat.
4. A mechanism as in claim 1, wherein said second
carriage has wheel means riding on a respective cable of
said pair of second cables, and wherein said second
movement means comprises a second cable loop disposed
generally parallel to said second cables and extending
between, a first driven pulley depending from a respective
first carriage and a second pulley depending from the other
first carriage, the second cable loop starting from said
second carriage and ending thereat.
5. A mechanism as in claim 1, wherein said set of third
cables is a plurality of independent cables depending from
said second carriage at one end and extensibly affixed to
respective movement means at the other end, and wherein
said respective movement means are mounted on said platform
member and are reversible motors.
6. An aerial support mechanism for providing five
independently addressable degrees of axial freedom to
multiple cameras, said mechanism comprising:
a plurality of vertically spaced pairs of parallel
first cables supported at both ends and supporting a
respective pair of first carriages therefrom, said
respective pair of first carriages having respective first
movement means for movement along said respective first

11
cables;
a plurality of pairs of transverse second cables
extending between and affixed to respective pairs of said
first carriages, for providing laterally-directed tension
to said respective first pairs of cables by way of a
respective one of said-first carriages, each pair of said
second cables terminating at a respective one of said first
carriages and adjustably terminating at the respective
other first carriage;
a plurality of second carriages, one each of said
second carriages depending from a respective pair of said
second cables and each of said second carriages having
independent second movement means for movement along a
respective pair of said second cables;
a plurality of platform members, each one of said
platform members depending from a set of third cables fixed
to and depending from a respective second carriage and
terminating in third movement means disposed on said
platform member for effecting movement of each of said
platform members vertically with respect to said respective
second carriage;
each of said platform members further comprising
rotatably mounted jointed means with a platform depending
therefrom for supporting a respective camera, said
articulating means rotatable about a horizontal axis by
means of respective fourth movement means, and said
articulating means including a fifth movement means to
effect rotation of said platform about a vertical axis; and
control means for remotely and independently
controlling individually the movement of each of the
respective first, second, third, fourth and fifth movement
means.
7. An aerial support mechanism for providing five
independently addressable degrees of axial freedom to
multiple cameras, said mechanism comprising:
a pair of spaced parallel first cables supported at
both ends and supporting a plurality of respective pairs of

12
first carriages therefrom, said respective pairs of first
carriages having respective first movement means for
movement along said first cables;
said pairs of first carriages further providing a pair
of respective transverse second cables extending between
and tensionably affixed thereto for providing
laterally-directed tension to said first pair of cables;
a plurality of second carriages one each of said
second carriages depending from a respective pair of said
second cables, and having respective second movement means
for movement along a respective second cable;
a plurality of platform members, each one of said
platform members depending from a set of third cables fixed
to and depending from a respective second carriage and
terminating in third movement means disposed on said
platform member for effecting movement of each of said
platform members vertically with respect to said respective
second carriage; and
control means for remotely and independently
controlling individually the movement of each of the
respective first, second, third, fourth and fifth movement
means.
8. An aerial support platform mechanism comprising:
a first pair of support cables each affixed at each
end to support means;
a pair of first carriages each moving along a
respective one of said first pair of support cables;
a drive cable for reciprocating each carriage of said
first pair along its respective support cable, each said
drive cable connected at one end to its respective
carriage, passing around a resiliently mounted pulley
adjacent one end of the support cable, around a reversible
drive means for reciprocating said drive cable adjacent an
opposite end of the support cable and connected at an
opposite end to said respective carriage;
a second pair of support cables each terminating at
one end to one of said pair of first carriages and

13
adjustably terminating at the other end to the other one of
said pair of first carriages, said second pair of support
cables acting through said pair of first carriages to
tension said first pair of support cables;
a drive cable for reciprocating a second carriage
along said second support cables, said drive cable
connected at one end to said second carriage, passing
around a pulley disposed on one of said first pair of
carriages, around a reversible drive means for
reciprocating said drive cable disposed on the other one of
said pair of first carriages and connected at an opposite
end to said second carriage;
a set of third support cables depending from said
second carriage, each one of said third set of cables
attached at one end to said second carriage and attached at
the other end to a respective reversible drive means, said
respective drive means mounted on a platform;
a support arm rotatably depending from said platform
and adapted to be rotated about a vertical first axis by a
first rotatable drive means, said support arm adapted to
provide rotation to a second platform depending therefrom
about an axis generally normal to said first axis by a
second rotatable drive means; and
control means for remotely and independently
controlling the movement of each of said reversible drive
means and said first and second rotatable drive means.

Description

Note : Les descriptions sont présentées dans la langue officielle dans laquelle elles ont été soumises.


' 2157222
FIELD OF THE INVENTION
The invention relates to an aerial support platform
mechanism for cinematographic and similar uses, more parti-
cularly to a mechanism having a platform supported to ex-
tend below and intermediate of a pair of parallel guidemembers, and having three linear axes of motion and two
rotational axes of motion.
BACKGROUND OF THE INVENTION
Various suspension systems for supporting equipment in
aerial locations are known. Such systems are particularly
important in the making of motion pictures, where cinemato-
graphic equipment has to be suspended at high elevations to
capture panoramic views. A boom mounted on a vehicle may
give the necessary height, or it may be possible to use the
roof of a nearby building. However, systems which are not
ground-based are increasingly being used, i.e. systems that
use cables or similar means for suspension. U. S. Patent
No. 4,710,819, granted to Garrett W. Brown on Dec. 1, 1987,
discloses one such system. It uses at least three flexible
members, such as cables, to suspend an equipment support
member inside of a support structure. Each of the flexible
members extends around a pulley on the support structure,
and has one end connected to the equipment support member
and the other end connected to a motor assembly controlled
by a computer. The relative movement of the flexible mem-
bers is synchronized by the computer, and this arrangement
allows a computer operator to control the position of the
support member within the support structure. A somewhat
similar concept for directing an underwater exploration de-
vice is disclosed in U.S. Patent No. 3,324,239, granted toI. C. Jacobson on June 6, 1967.
Numerous difficulties have been found to exist with
the suspension system of Brown. A major problem is stress
on the cables; because of the angles involved, supporting

~157222
an item weighing several hundred pounds may create a ten-
sion in the cables many times higher; the cables have been
known to break under such stress. Brown's three-cable and
four-cable systems incorporate no redundancy; if a cable
breaks, the supported item freely falls. Known problems
with prior art systems are the stress placed on the motor
assemblies to which the cables connect, the motors are
under continual pressure to maintain tension on the cables,
which leads to their frequent burn out, and the creation of
wave motion in the cables; this results in serious prob-
lems for cinematographers and others who require a highly
stable camera platform with smooth movement.
The aerial support platform mechanism of the subject
invention has a redundancy built into its cable system; if
a support cable should break, a parallel drive cable takes
on the support cable load and prevents the supported item
from falling. Because the vertical cables in the subject
invention only have to carry the weight of the supported
item and are not part of the overall suspension system as
in the Brown system, those cables can be made considerably
thinner than is possible with Brown's system. That allows
the vertical cables supporting a camera on a first platform
member of the invention to be invisible to a second camera
on a second platform member, even if the separation between
the two is only a few feet. Because the motors of the sub-
ject platform mechanism only act to move carriages and not
to support cables as in Brown, the motors have little or no
burn out. The cables of the subject platform mechanism ex-
perience negligible wave motion because the start/stop por-
tion of the software that controls movement has a built-in
inertia compensation, similar to that found in modern ele-
vator control systems.
Two further prior art systems are found in U.S. Patent
5,113,768 (Brown) and U.S.Ptaent 5,225,863 (Weir-Jones).
These systems are directed solely to linear traveling and
does not permit substantive lateral or vertical
displacement of the camera system.

3 ~ ~ ~72~2
SUMMARY OF THE INVENTION
The invention is an aerial support platform mechanism
having a pair of parallel first guide means, transverse
second guide means, and vertical third guide means. It
also has a pair of first carriages, each supported on a
respective one of the first guide means and having a first
movement means for moving it along the respective first
guide means. The transverse guide means extends between
the pair of first carriages, and supports a second carriage
and a second movement means for moving that carriage along
the second guide means. The vertical guide means extends
downward from the second carriage, and supports a platform
member and a third movement means for moving the platform
member relative to the third guide means. The platform
member has a frame connected to the third guide means, and
also has a platform connected to the frame. The platform
is rotatable around two axes relative to the frame by means
of a fourth and a fifth movement means. The mechanism also
has a control means for controlling movement of the first,
second, third, fourth and fifth movement means.
Each first guide means may be a cable, and each first
carriage may have a wheel means riding on the respective
cable. The second guide means may be a cable that extends
between the pair of first carriages, and the second
carriage may have a wheel means riding on that cable. The
third guide means may be a series of cables that extend
between the second carriage and the frame of the platform
member.
The platform of the platform member may be connected
to the frame for rotation around a vertical first axis and
around a second axis extending generally normal to the
first axis. A disk member may be rotatably connected to
the frame for rotation around a vertical first axis, and
the platform may be rotatably connected to the disk member
for rotation around an axis extending generally normal to
the first axis.
Each first movement means may comprise a first cable

~ 2157222
loop that extends between a first driven pulley and a se-
cond pulley, and connects to a respective first carriage at
a point intermediate the first and second pulleys. The
second movement means may comprise a second cable loop that
extends between a third driven pulley and a fourth pulley,
and connects to the second carriage at a point intermediate
the third and fourth pulleys. The third pulley may be se-
cured to one first carriage, and the fourth pulley may be
secured to the other first carriage. Alternatively or ad-
ditionally, the third and fourth pulleys may be secured torespective opposite ends of the second guide means.
An extended aerial support platform mechanism may com-
prise a series of the basic platform mechanisms described
above, each of the basic mechanisms having a single common
first guide means.
SHORT DESCRIPTION OF THE DRAWINGS
The platform mechanism of the invention will next be
further described by means of a preferred embodiment, uti-
lizing the accompanying drawings, in which:
Figure 1 is a perspective view of the aerial support
platform mechanism of the invention;
Figure 2 is a perspective view of three of the aerial
support platform mechanisms situated in close proximity;
Figure 3 is a side view of the aerial support platform
mechanism of Figure l;
Figure 4 is a top view of the aerial support platform
mechanism of Figure l;
Figure 5 is an enlarged view of a segment of the top
view of Figure 4;
Figure 6 is a perspective view of a first carriage and
the first and second guide means;
Figure 7 is a side view of the two first carriages,
the second carriage, and the second guide means for moving
the second carriage;
Figure 8 is an enlarged view of a first carriage, the

~ 2157222
second carriage, and a motor for moving the second carriage
on the second guide means;
Figure 9 is a top view of the two first carriages, the
second carriage, and the second guide means of Figure 7;
Figure 10 is a perspective view of the second carri-
age, the third guide means and the platform member;
Figure 11 is an end view of the second carriage, the
third guide means and the platform member of Figure 10;
Figure 12 is a schematic diagram of the control system
utilized to operate the three aerial support platforms of
Figure 2; and,
Figure 13 is a perspective view of the platform mech-
anism built into a truss hoistable by a pair of cranes.
DESCRIPTION OF A PREFERRED EMBODIMENT
A form of the aerial support platform mechanism that
is used to support a camera in a studio is shown in Figure
1. A pair of guide cables 14 and 16 each extend across a
respective one of a pair of facing side walls 18 and 20 of
the studio. One end of guide cable 14 is fixed to a first
end wall 21 by a bracket 22. The other end of cable 14 is
connected to a first end of a turnbuckle 24, the other end
of which is fixed by a bracket 25 to a second end wall 26.
The guide cable 16 is similarly supported on the other side
wall 20. In this embodiment the guide cables 14 and 16 are
each approximately fifty feet in length.
Riding on guide cable 14 is a carriage generally de-
signated 30; a similar carriage 31 rides on guide cable 16.
As illustrated in Figures 5 and 6, the carriages 30 and 31
are each formed by a pair of generally rectangular plates
32 with a pair of angled corners. Plates 32 are held in
parallel spaced relation by a series of spacers 34 mounted
between them; each spacer 34 is secured to each plate 32 by
a screw 36. Rotatably mounted between the plates 32 are a
pair of large pulleys 38 and a pair of small pulleys 40. A
series of holes 42 are positioned around the periphery of

each plate 32.
A pair of cables 44 extend between the two carriages
30 and 31. Each end of each cable 44 terminates in a loop
45 that extends around one of the spacers 34 mounted
between the pair of plates 32. Each cable 44 is connected
to a turnbuckle 46 which, when rotated, increases the
tension on the cable. As illustrated in Figure 9, a
carriage assembly 48 formed by a pair of carriages 50 each
of similar construction to the carriages 30 and 31, rides
on the pair of cables 44. The two carriages 50 are held in
parallel, spaced relation by a series of struts 52.
Each of the carriages 30 and 31, and the carriage
assembly 48, moves by means of a respective cable loop,
held between a pulley and a motor shaft, as shown in
Figures 3 and 4. With respect to the carriages 30 and 31,
a cable 56 connects to one side of each carriage, extends
around a pulley (not shown) on a shaft of a motor 58,
around a pulley 60, and then connects to the other side of
the respective carriage. The motor 58 is mounted on the
end wall 21 by a bracket 62. The pulley 60 is connected
through a spring member 64 to a turnbuckle 66, which is
secured to the end wall 26 by a bracket 68. A clamp 69 on
the top of motor 58 secures the guide cable 14 to the
motor. If the cable 14 breaks, the cable 56 prevents the
carriage 30 from falling and supports that carriage until
repairs are made.
A cable 70 connects to one of the struts 52 between
the pair of carriages 50, extends around a pulley (not
shown) on the shaft of a motor 72, extends around a pulley
74, and then connects to the another of the struts 52. As
seen in Figs. 6, 7 and 8, the motor 72 is secured to the
carriage 30 by a pair of struts 76, and is secured to the
cables 44 by a bar 77. The pulley 74 is secured to a
spring member 78, which in turn is secured to the carriage
31. Since the position of motor 72 changes as it moves
across wall 18, a helical power line 80 is used to connect
motor 72 to a ceiling power connection.
A platform member generally designated 84 is suspended

7 ~ 7 ~ ~ 2
by four cables 86 from the carriage assembly 50, two of the
cables 86 extending from each carriage 50. As seen in
Figs. 9 and 10, within an upper housing 88 of the platform
member 84 are four motors 90. A lower part of each cable
86 enters the housing 88 through a respective opening 92 on
the upper surface of housing 88, and is wound around a
rotor spindle 94 on a respective one of the four motors 90.
The four motors 90 are actuated simultaneously to either
raise or lower the platform member 84. A helical power
line 96 extends between platform member 84 and one of the
carriages 50, and another connecting helical power line 98
extends between the carriage 50 and a ceiling power connec-
tion. This arrangement provides power to the motors 90 at
all lateral positions of carriage assembly 48 and all vert-
ical positions of the platform member 84.
Rotatably mounted under the housing 88 for rotationaround a vertical axis is a disk 100. A motor (not shown)
inside the housing 88 is adapted to rotate disk 100. Con-
nected to the disk 100, and extending downwardly from the
periphery thereof, is a strut 102. To a lower end of the
strut 102 a powered joint 104 is connected. A second strut
106 is connected to joint 104, and extends downwardly of
that joint to support a connected platform 108. A motor
(not shown) within the joint 104 is adapted to rotate
second strut 106 relative to strut 102, and thereby rotate
platform 108 relative to housing 88. The power to actuate
the motors which rotate the disk 100 and the platform 108
is provided through the helical power lines 96 and 98.
As shown in Figures 1 and 2, the platform 108 may be
used to support a camera generally designated as 110 in a
studio. With respect to the studio configuration in Figure
2, the integrated control system of Figure 12 is used to
control five degrees of motion for each of three support
platforms 114, 116 and 118. One person controls the X, Y
and Z directional degrees of motion for each of the three
platforms 114, 116 and 118 using monitor 120 and joystick
122, while a second person controls the two rotational
degrees of motion for each of the platforms using monitor
A

21a7222
124 and joystick 126.
Where no vertical members exist for supporting the
aerial support platform of the invention, a rigid truss is
used. Depending on its size, a truss may be hoisted by a
single crane, or by a crane positioned on each side, or by
a crane positioned at each corner. In Figure 13, a pair of
cranes 128 and 129 each connects to a respective opposite
side of a truss 130. The truss 130 supports two cables 132
and 134 in a manner similar to that in which the cables 14
and 16 are supported in Figure 1. Three carriages 136 ride
on cable 132, and three carriages 138 ride on cable 134. A
transverse cable 140 connects each carriage 136 with a res-
pective carriage 138, and on each cable 140 sits a carriage
142. This configuration differs from the Figure 2 embodi-
ment in that movement of the three aerial support platformsis dependent on each other. In Figure 2, there is a suffi-
cient vertical distance between each of the three support
cables 150, 152 and 154 on each side wall that each of the
associated support platforms is movable to any position in
the studio.

Dessin représentatif
Une figure unique qui représente un dessin illustrant l'invention.
États administratifs

2024-08-01 : Dans le cadre de la transition vers les Brevets de nouvelle génération (BNG), la base de données sur les brevets canadiens (BDBC) contient désormais un Historique d'événement plus détaillé, qui reproduit le Journal des événements de notre nouvelle solution interne.

Veuillez noter que les événements débutant par « Inactive : » se réfèrent à des événements qui ne sont plus utilisés dans notre nouvelle solution interne.

Pour une meilleure compréhension de l'état de la demande ou brevet qui figure sur cette page, la rubrique Mise en garde , et les descriptions de Brevet , Historique d'événement , Taxes périodiques et Historique des paiements devraient être consultées.

Historique d'événement

Description Date
Le délai pour l'annulation est expiré 2000-08-30
Lettre envoyée 1999-08-30
Accordé par délivrance 1999-03-23
Inactive : Taxe finale reçue 1998-12-08
Préoctroi 1998-12-08
Un avis d'acceptation est envoyé 1998-06-09
Un avis d'acceptation est envoyé 1998-06-09
Lettre envoyée 1998-06-09
Inactive : Renseign. sur l'état - Complets dès date d'ent. journ. 1998-06-05
Inactive : Dem. traitée sur TS dès date d'ent. journal 1998-06-05
Inactive : Approuvée aux fins d'acceptation (AFA) 1998-05-08
Demande publiée (accessible au public) 1997-03-01
Exigences pour une requête d'examen - jugée conforme 1995-08-30
Toutes les exigences pour l'examen - jugée conforme 1995-08-30

Historique d'abandonnement

Il n'y a pas d'historique d'abandonnement

Taxes périodiques

Le dernier paiement a été reçu le 1998-08-31

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  • taxe additionnelle pour le renversement d'une péremption réputée.

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Historique des taxes

Type de taxes Anniversaire Échéance Date payée
TM (demande, 2e anniv.) - petite 02 1997-09-02 1997-09-02
TM (demande, 3e anniv.) - petite 03 1998-08-31 1998-08-31
Taxe finale - petite 1998-12-08
Titulaires au dossier

Les titulaires actuels et antérieures au dossier sont affichés en ordre alphabétique.

Titulaires actuels au dossier
PAUL KNELLER
Titulaires antérieures au dossier
S.O.
Les propriétaires antérieurs qui ne figurent pas dans la liste des « Propriétaires au dossier » apparaîtront dans d'autres documents au dossier.
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Description du
Document 
Date
(aaaa-mm-jj) 
Nombre de pages   Taille de l'image (Ko) 
Page couverture 1996-10-24 1 16
Abrégé 1996-10-24 1 26
Description 1996-10-24 8 378
Revendications 1996-10-24 5 217
Dessins 1996-10-24 12 287
Description 1998-04-22 8 390
Revendications 1998-04-22 5 240
Page couverture 1999-03-17 1 55
Dessin représentatif 1999-03-17 1 7
Dessin représentatif 1998-03-27 1 18
Avis du commissaire - Demande jugée acceptable 1998-06-09 1 164
Avis concernant la taxe de maintien 1999-09-27 1 179
Avis concernant la taxe de maintien 1999-09-27 1 179
Correspondance 1998-12-08 2 52
Taxes 1998-08-31 1 42
Taxes 1997-09-02 1 33
Demande de l'examinateur 1997-08-29 2 59
Correspondance de la poursuite 1998-02-13 3 82
Correspondance de la poursuite 1998-02-13 3 148
Correspondance de la poursuite 1995-08-30 10 527