Watercraft
11377810 · 2022-07-05
Inventors
Cpc classification
B63B35/003
PERFORMING OPERATIONS; TRANSPORTING
E02D13/00
FIXED CONSTRUCTIONS
G01K11/00
PHYSICS
B63B35/44
PERFORMING OPERATIONS; TRANSPORTING
B63B21/50
PERFORMING OPERATIONS; TRANSPORTING
B63B7/00
PERFORMING OPERATIONS; TRANSPORTING
International classification
E02D13/00
FIXED CONSTRUCTIONS
B63B7/00
PERFORMING OPERATIONS; TRANSPORTING
B63B21/50
PERFORMING OPERATIONS; TRANSPORTING
B63B35/44
PERFORMING OPERATIONS; TRANSPORTING
Abstract
The invention relates to a watercraft having a hull (10), an introduction installation (20) for an object (70) to be anchored in the water, said introduction installation (20) being disposed on said hull (10), and at least one compressor (30) having at least one compressed-air line (40) which leads into the water and is coupled to at least one compressed-air distribution installation (45) which has a horizontal extent and for generating a bubble curtain (50) below the hull (10) has a multiplicity of mutually spaced apart outflow openings (46), characterized in that the hull (10) has at least two sub-hulls (11, 12) which are disposed so as to be mutually spaced apart and connected to one another, and a void (15) which is at least partially surrounded by the bubble curtain (50) is situated between the sub-hulls (11, 12).
Claims
1. A watercraft, comprising: a hull which comprises at least two sub-hulls which are disposed mutually spaced apart and connected to one another, and the hull at least partially encloses a void which is situated between the sub-hulls; an introduction installation for an object to be anchored in a bed of a body of water, said introduction installation being disposed on said hull; a first compressed-air distribution installation which comprises a multiplicity of mutually spaced apart outflow openings and is configured to be selectively lowered from the hull to the bed by holding elements and to extend, when on the bed, horizontally in a configuration that is circumferential about a location where the object has been or will be anchored, and; a second compressed-air distribution installation that comprises another multiplicity of mutually spaced apart outflow openings and is configured to be selectively lowered from the hull to the bed by other holding elements and to extending when on the bed, horizontally in a configuration about an external circumference of the hull; and at least one compressor which is configured to selectively pump compressed air into the first compressed-air distribution installation and the second compressed-air distribution installation, through at least one compressed-air line which is configured to extend to the first and the second compressed-air distribution installations on the bed, wherein the mutually spaced apart outflow openings of the first compressed-air distribution installation on the bed are configured to generate, when receiving the compressed air from the at least one compressor via the at least one compressed-air line, a first bubble curtain that rises from the mutually spaced apart outflow openings on the bed, vertically upward to an area of the hull which at least partially encloses the void and at least partially surrounds the introduction installation or the object to be anchored in the water, and the mutually spaced apart other outflow openings of the second compressed-air distribution installation on the bed are configured to generate when receiving compressed air from the at least one compressor, via the at least one of another compressed-air line, a second bubble curtain that rises from the mutually spaced apart other outflow openings of the second compressed-air distribution installation on the bed, vertically upward toward a surface of the water about the external circumference of the hull.
2. The watercraft as claimed in claim 1 wherein the first compressed-air distribution installation extends to form a closed circumference.
3. The watercraft as claimed in claim 1 wherein the first compressed-air distribution installation is configured as a tube or hose, and the multiplicity of mutually spaced apart outflow openings extend through a wall of the tube or wall of the hose.
4. The watercraft as claimed in claim 1 wherein the multiplicity of mutually spaced apart outflow openings are configured as mutually spaced apart with identical mutual spacings.
5. The watercraft as claimed in claim 1 further comprising ballast installations disposed on at least the first compressed-air distribution installation.
6. The watercraft as claimed in claim 1 wherein the at least two sub-hulls are configured to surround the void, or to partially surround the void in a configuration that provides at least one lateral access to the void.
7. The watercraft as claimed in claim 6 wherein the first compressed-air distribution installation is further configured to generate, in response to the compressed air, the first bubble curtain according to a further configuration that surrounds a circumference of the void, or is a circumferentially closed first bubble curtain that surrounds the void and bridges the at least one lateral access.
8. The watercraft as claimed in claim 1 further comprising at least one support element selected from the group consisting of a net, a tubular steel construction, plates and/or meshes, wherein the at least one support element is configured to laterally surround the object to be anchored below the hull.
9. The watercraft as claimed in claim 8 wherein the at least one support element comprises a plurality of support elements having dissimilar diameters or mutually corresponding internal and external dimensions, and are disposed in a telescoping manner to be displaceable from one another.
10. The watercraft as claimed in claim 8 further comprising gas-filled flexible damper elements fastened to one or more support elements of the at least one support element.
11. The watercraft as claimed in claim 8 wherein the first compressed-air distribution installation is further configured to generate the first bubble curtain to also surround surrounds the at least one support element and/or be surrounded by the at least one support element.
12. The watercraft as claimed in claim 8 wherein the at least one support element is fastened to a frame.
13. The watercraft as claimed in claim 8 wherein the first compressed-air distribution installation is mounted on or in a frame comprising or composed of a dimensionally stable material.
14. The watercraft as claimed in claim 13 wherein the frame has a U-profile, an H-profile, and/or a T-profile.
15. The watercraft as claimed in claim 13 wherein the frame is configured as foldable or collapsible.
16. The watercraft as claimed in claim 13 wherein the frame comprises interconnected segments that connect at respective connection points, wherein the connection points are configured to permit a mutual relative movement of the interconnected segments.
17. The watercraft as claimed in claim 15, further comprising a drive, coupled to the frame and configured to open and to close the frame.
18. The watercraft as claimed in claim 1 wherein the multiplicity of mutually spaced apart outflow openings of the first compressed-air distribution installation are oriented in dissimilar directions.
19. The watercraft as claimed in claim 1, further comprising another first compressed-air distribution installation, which is disposed in alignment with and at a height above the first of compressed-air distribution installation on the bed.
20. The watercraft as claimed in claim 19 wherein: the multiplicity of mutually spaced apart outflow openings of the first compressed-air distribution installation on the bed have opening sizes that are dissimilar to opening sizes of the multiplicity of mutually spaced apart other outflow openings of the other compressed-air distribution installation.
21. The watercraft as claimed in claim 19 wherein the first compressed-air distribution installation is configured to form an internal pressure, in response to the compressed air that is dissimilar to an internal pressure that the second compressed air distribution system forms in response to the compressed air.
22. A compressed-air distribution installation for fastening to and lowering from a watercraft on a body of water, the watercraft having a hull comprising two sub-hulls which are disposed as mutually spaced apart with a void situated between the two sub-hulls, and the lowering being to a bed of the body of water, said compressed air distribution installation comprising: a first multiplicity of spaced apart compressed air outflow openings that, when the compressed air installation is on the bed of the water of water, are located on the bed at first positions along a first pattern that extends horizontally and circumferentially surrounding the void; a second multiplicity of spaced apart compressed air outflow openings that, when the compressed air installation is on the bed of the water of water, are located on the bed at second positions along a second pattern that extends horizontally and circumferentially surrounding an external circumference of the hull, wherein: the first multiplicity of spaced apart compressed air outflow openings are configured to generate, in response to receiving a compressed air from a compressed air line, a first bubble curtain that rises from the bed below the hull, from the first positions along the first pattern, vertically upward to the hull circumferentially surrounding the void, and the second multiplicity of spaced apart compressed air outflow openings are configured to generate, in response to receiving another compressed air feed from the compressed air line or another compressed air line, a second bubble curtain that rises from the bed below the hull, from the second positions along the second pattern, vertically upward to a surface of the body of water which is circumferentially about the external circumference of the hull.
23. The compressed-air installation as claimed in claim 22 further comprising at least one frame which is configured as selectively buoyant and selectively lowerable.
Description
(1) Exemplary embodiments of the invention will be explained in more detail hereunder by means of the appended figures in which:
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(18) The post 70 in
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(20) Moreover, compressors by way of which the compressed air is directed through a compressed-air line to a compressed-air distribution installation are disposed on the hull 10 of the watercraft 1, said compressed-air distribution installation in one variant of the invention likewise being situated on or in the frame 80. A bubble curtain which for avoiding any further minimizing of the noise pollution on account of the object 70 being introduced extends around the object 70 to be anchored is thus generated during the introduction procedure of the post 70, for example by piling or drilling. The bubble curtain within and/or outside the support element can move upward to the water surface 2. The support element 60 is configured such that water can pass through the intermediate spaces in the support element which is in particular configured as a net or mesh. The damper elements can be situated within or outside the tubular support element 60 and also be fastened to the latter on both sides. The hydraulic acoustic damping installation can thus be designed and used with as well as without a bubble curtain.
(21) Upon anchoring of the object 70 in the bed of the body of water 3, the frame 80 conjointly with the damper elements, optionally the compressed-air distribution installation, as well as the support element 60, is pulled to the surface by way of the holding installations 47. This takes place by way of winches or the like which are disposed on the watercraft 1.
(22)
(23) It can be seen in
(24) The position resulting on account thereof, prior to the object being introduced into the bed of the body of water, is illustrated in
(25) Two variants of the hull shape are illustrated in
(26) The watercraft 1 having the two sub-hulls 11, 12 as well as the cross member 13 is schematically illustrated in
(27) A variant of the invention, in which the frame 80 is disposed at a larger spacing about the object 70 to be introduced is shown in
(28)
(29) The compressed-air lines 40 open into a compressed-air distribution installation 45 which in the exemplary embodiment illustrated is configured so as to fully encircle the frame 80. The compressed-air distribution installation 45 can be fastened in or to the frame 80, and in the case of a fully circumferential disposal distributes the compressed air about the object (not illustrated) to be anchored in the bed of the body of water 3.
(30) It can be seen in the left illustration of
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(32) A detailed view of the compressed-air distribution installation according to
(33) A weight or a ballast installation 90 which is configured as a T-support and by way of the transverse leg is fastened on the frame 30 so as to be oriented toward the base is disposed below the frame 80. Two compressed-air distribution installations 45 are disposed in the intermediate space between the base of the frame 80 and the T-support in the illustrated example, outflow openings 46 being configured in said compressed-air distribution installations 45. The compressed-air distribution installations 45 can be configured as pipes or hoses; the outflow openings 46 in the exemplary embodiment illustrated point in mutually opposite directions such that a bubble curtain 50 is created on both sides of the support element 60, thus on the internal side and on the external side in the case of a closed circumference of the support element. The outflow openings 46 can also be directed downward such that the compressed air is directed in the direction toward the bed of the body of water 3, so as to generate an ideally continuous bubble curtain 50 from the bed of the body of water 3 up to the surface of the body of water 2.
(34) A variant of the invention in which a total of three compressed-air distribution installations 45 are disposed at three different heights is shown in
(35) A third variant of the invention in which a compressed-air distribution installation 45 is disposed externally around the circumference of the watercraft 1 is shown in
(36)
(37) A further variant of the invention in which the externally encircling bubble curtain 50 is generated by way of three compressed-air distribution installations 45 which are disposed on dissimilar levels around the entire watercraft 1 is shown in
(38) All three components of the hydraulic acoustic damping are shown conjointly with the watercraft 1 in
(39) A second support element 60 is disposed so as to be somewhat further away therefrom, thus so as to be radially spaced apart from the first support element 60. This support element 60 on the base side is also mounted on a rectangular frame 80 and extends to the water surface 2. Damper elements 65 which can be composed of gas-filled hollow panels or foam-material elements are fastened to the second support element 60 which configures an angular cross-section and is disposed within the void 15 between the two sub-hulls 11, 12. Conjointly with said hydraulic acoustic damper elements 65 and a bubble curtain 50 which by way of a compressed-air distribution installation 45 on the frame 80 runs from the bed of the body of water 3 to the surface of the body of water 2, further damping of the noise pollution created on account of the piling of the post can be effected. A plurality of compressed-air distribution installations 45 which are disposed at dissimilar height levels can be provided. The compressed-air distribution installations 45 can have outflow openings 46 which are oriented in dissimilar directions so as to configure a bubble curtain 50 having double walls which are mutually spaced apart.
(40) The bubble curtain 50 which is configured externally about the watercraft 1 and which surrounds the hull 10 having the two sub-hulls 11, 12 and the void 15 situated therebetween forms the third damper component. Here too, a plurality of compressed-air distribution installations 45 can be disposed at dissimilar heights so as to achieve the desired characteristics of a bubble curtain 50 by way of dissimilar pressures or dissimilar outflow opening diameters.