The present invention relates to a system for transporting people and/or freight. This includes in particular the transport of people and/or freight to floating objects and/or objects fixed to the bottom of the sea and or standing on the bottom of the sea, such as platforms used for the production of oil, gas or electricity.
A known method makes use of a helicopter for transporting in particular personnel to and fro. The use of a vessel is part of another method. However, due to the sometimes strong wave motion, the creating and maintaining of a safe footbridge between the vessel and a respective landing place is not without danger. In practice, there is a need for a system enabling the safe transport of people and/or freight.
It is an object of the present invention to provide a system enabling quick and safe transport of people and/or freight from or to a vessel or an object standing on the bottom of the sea, such as a drilling platform.
To achieve this, the system for transporting people and/or freight according to the invention has the characteristics described in claim 1.
An advantage of the system according to the invention resides in that the shuttle to be lifted, whether or not accommodating people and/or freight, can be transported by a crane present at the site from a vessel to a fixed or floating object, or conversely. The shuttle can be used as a hoistable transport means and the first catch member thereof can be lowered on to the second catch member of the respective landing station. In this position the complementary catch members are connected to each other. Subsequently, the catch members and the shuttle are stabilised in position on the landing site by the activated stabilisation members, after which the shuttle is detached from the hoisting cable by the subsequently activated detachable means intended for this purpose. As a result, the shuttle is in the proper stable position, which is maintained to enable the crew to safely leave or board the shuttle. Conversely, after catching the shuttle and attaching it to the hoisting cable, the stabilisation members are deactivated, after which the shuttle can be lifted safely.
In a possible embodiment of the system according to the invention, the first catch member on the lower side of the shuttle tapers off to the bottom. The second catch member present on the landing station is complementary to the first catch member, said second catch member having a cavity which tapers off to the bottom. Said first catch member, for example, terminates in a point which enters into the complementary cavity on the landing station. The cavity which accommodates the pointed end of the shuttle may be a simple recessed part, which may be provided, for example, on the deck of a vessel, the quay or a platform at sea. After the catch members have been caught and coupled to each other, the stabilisation members are activated, causing the shuttle to remain in a stable position on the landing station. After activation of the stabilisation members, a command is directed at the detachable means connected to said stabilisation members, causing the hoisting cable to become automatically detached from the stably positioned shuttle.
Another possible embodiment of the system according to the invention is the reverse, as it were, of the abovementioned embodiment. Thus, in this embodiment, the first catch member situated on the bottom side of the shuttle is a cavity which tapers off to the top. And the second catch member situated on the landing station tapers off to the top, for example like a cone or a hemisphere. In this embodiment, the first catch member on the shuttle is in the shape of, for example, a conical cavity in which fits, for example, the spherical second catch member which terminates in a point and which is situated on the landing station. Said cavity has a recessed portion in which said point on the cone or hemisphere, which may or may not be springy in transverse direction, is caught. In this embodiment, the landing station can be fastened, preferably detachably, to the deck of the transport vessel, the quay or a platform. Also in this embodiment, after the catch members have been caught and coupled to each other, the stabilisation members are activated, causing the shuttle on the landing station to remain in a stable position.
In general, as regards the embodiments explained hereinabove, the hoist connection comprising a ball-locking mechanism situated on the top side of the shuttle and forming part of the detachable means is disconnected. Subsequently, the crew can safely board and disembark. To lift the shuttle from its position on the landing station, the crane operator is instructed to restore the connection with the shuttle by means of the ball which is located at the end of the hoisting cable and which is then lifted or inserted into the funnel situated on top of the shuttle. Next, the ball is secured in the locking mechanism, thereby restoring the connection between the hoisting cable and the shuttle. Immediately after said connection has been established, the stabilisation members are automatically deactivated. In order to carry out the abovementioned automatic processes and to give and process mutual instructions, the activable stabilisation members and the detachable means are connected to each other.
In both embodiments, the locking members can be provided at possible and/or desired locations on the shuttle, the landing station or both the shuttle and the landing station in an advantageous manner.
Further detailed, possible embodiments, which are set forth in the remaining claims, are mentioned together with the associated advantages in the following description.
The system according to the present invention will now be explained in greater detail with reference to the figures mentioned below, in which corresponding parts are indicated by means of the same reference numerals. In the Figures:
On the bottom side, the shuttle 2 is provided with a first catch member 7-1, which is shaped so as to be complementary to a second catch member 7-2. In the embodiment shown in
In terms of shape, both catch members 7-1, 7-2 fit together, at least partly, in both embodiments, which helps in catching and coupling both members without the need of manpower, so that both members can be easily coupled and uncoupled.
The shuttle 2 and the landing station 8 are secured or stabilised in position and their relative position is maintained by activation of stabilisation members 9-1, 9-2. These activable members are provided, according to the requirements, on the shuttle 2 (
Next, by providing a footbridge 10, 11, which is often extendable, the crew can safely walk from or to the compartment 3.
A catching basket 12 which flares out to the top makes it easier to catch a weight or ball 13 attached to the hoisting cable 5. In the case shown here, said catching basket 12 is housed in the top side of the shuttle 2. The crane operator must subsequently lower the ball 13 into the catching basket 12, and the ball, as a result of its shape, then moves to the center of the catching basket 12, where it is retained by the activable means 14 such that the shuttle 2, after the subsequent retraction of the pins 9-1, can be lifted from its position, in this case the landing station 8, by the crane operator. The shuttle 2 comprises a hydraulic system 16 which, in order to carry out said operation, is connected to the movable pins 9-1 and to the means 14.
In this embodiment, the first catch member, which is situated on the lower side of the shuttle 2, is a cavity 7-1 which tapers off to the top. The second catch member 7-2, which is a kind of hemisphere, is situated on the landing station 8 and tapers off to the top so as terminate in a point or cone 15. As the arrows diagrammatically show, the cone 15 may be springy in transverse direction in order to cushion any shocks when the two catch members 7-1, 7-2 approach and engage one another. In the case shown here, stabilisation members in the form of extendable pins 9-1 are provided in the shuttle 2 and stabilisation members in the form of a suitable cavity and/or groove 9-2 are provided on the landing station 8. The reverse or a combination with the foregoing is also possible of course, that is to say, pins 9-1 on the landing station 8 and the groove 9-2 in the cavity 7-1 of the shuttle 2. When use is made of a circumferential groove 9-2 extending along the outer circumference of said cone or hemisphere 7-2, the shuttle can be lowered, in any required rotational position, on to the landing station 8, after which the hydraulic system 16 is used to secure the one or more pins 9-1 in the circumferential groove 9-2, and next the means 14 connected to the system 16 and/or to the one or more pins 9-1 are operated to uncouple the shuttle 2 from the hoisting cable 5.
Number | Date | Country | Kind |
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2017388 | Aug 2016 | NL | national |