KR101711429B1 - Helideck - Google Patents
Helideck Download PDFInfo
- Publication number
- KR101711429B1 KR101711429B1 KR1020150050601A KR20150050601A KR101711429B1 KR 101711429 B1 KR101711429 B1 KR 101711429B1 KR 1020150050601 A KR1020150050601 A KR 1020150050601A KR 20150050601 A KR20150050601 A KR 20150050601A KR 101711429 B1 KR101711429 B1 KR 101711429B1
- Authority
- KR
- South Korea
- Prior art keywords
- deck
- base
- base deck
- extension
- helideck
- Prior art date
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Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B63—SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
- B63B—SHIPS OR OTHER WATERBORNE VESSELS; EQUIPMENT FOR SHIPPING
- B63B35/00—Vessels or similar floating structures specially adapted for specific purposes and not otherwise provided for
- B63B35/50—Vessels or floating structures for aircraft
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B63—SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
- B63B—SHIPS OR OTHER WATERBORNE VESSELS; EQUIPMENT FOR SHIPPING
- B63B15/00—Superstructures, deckhouses, wheelhouses or the like; Arrangements or adaptations of masts or spars, e.g. bowsprits
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
- B64F1/00—Ground or aircraft-carrier-deck installations
- B64F1/007—Helicopter portable landing pads
-
- E—FIXED CONSTRUCTIONS
- E01—CONSTRUCTION OF ROADS, RAILWAYS, OR BRIDGES
- E01F—ADDITIONAL WORK, SUCH AS EQUIPPING ROADS OR THE CONSTRUCTION OF PLATFORMS, HELICOPTER LANDING STAGES, SIGNS, SNOW FENCES, OR THE LIKE
- E01F3/00—Landing stages for helicopters, e.g. located above buildings
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F15—FLUID-PRESSURE ACTUATORS; HYDRAULICS OR PNEUMATICS IN GENERAL
- F15B—SYSTEMS ACTING BY MEANS OF FLUIDS IN GENERAL; FLUID-PRESSURE ACTUATORS, e.g. SERVOMOTORS; DETAILS OF FLUID-PRESSURE SYSTEMS, NOT OTHERWISE PROVIDED FOR
- F15B15/00—Fluid-actuated devices for displacing a member from one position to another; Gearing associated therewith
- F15B15/08—Characterised by the construction of the motor unit
- F15B15/14—Characterised by the construction of the motor unit of the straight-cylinder type
- F15B15/16—Characterised by the construction of the motor unit of the straight-cylinder type of the telescopic type
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- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Aviation & Aerospace Engineering (AREA)
- Combustion & Propulsion (AREA)
- Ocean & Marine Engineering (AREA)
- Fluid Mechanics (AREA)
- General Engineering & Computer Science (AREA)
- Architecture (AREA)
- Civil Engineering (AREA)
- Structural Engineering (AREA)
- Physics & Mathematics (AREA)
- Bridges Or Land Bridges (AREA)
- Wind Motors (AREA)
Abstract
A helideck is initiated. A helideh according to an embodiment of the present invention includes: a base deck disposed in front of a structure installed on an upper surface of a ship; And an extension deck disposed on both sides of the base deck and inclined relative to the base deck, the base deck being adapted to maintain a horizontal position to provide a landing surface at which the helicopter can land and take off, And can be inclined downwardly forward of the structure to reduce wind load.
Description
The present invention relates to a helideck, and more particularly, to a helideck installed on a ship.
Most large ships and offshore structures, such as drillships, are equipped with Helideck, which provides landing surfaces for helicopters to land and land for emergency and, if necessary, transport of life and materials. The helideck is generally installed in the upper area of a structure such as a deckhouse.
These heli-decks are often not used during a voyage or during off-shore operations where helicopter landings and landings are not required during sea voyage.
In addition, during the voyage of the ship or offshore structure, wind load caused by the wind blowing toward the structure acts on the structure where the helideck is installed. Because of such wind loads, the resistance of ships or offshore structures increases, resulting in energy losses.
An embodiment of the present invention is to provide a helideck that reduces the wind load acting on a structure installed on the upper surface of a ship while a ship or the like is navigating.
According to an aspect of the present invention, there is provided a hull comprising: a base deck disposed in front of a structure installed on an upper surface of a hull; And an extension deck disposed on both sides of the base deck and inclined relative to the base deck, the base deck being adapted to maintain a horizontal position to provide a landing surface at which the helicopter can land and take off, A helideck may be provided, which is operated to tilt down the front of the structure to reduce wind loads.
The heli deck may further include a base driving unit that provides a driving force to operate the base deck in a horizontal or inclined manner.
The rear end of the base deck may be hinged to all of the structure, and the base driving unit may include a hydraulic cylinder extending and retracting to rotate the base deck.
The base driving unit includes a first actuator for moving the front end of the base deck up and down; And a second actuator for moving the rear end of the base deck upward and downward.
The helideck may be rotatably coupled to the base deck.
The helideck may further include an elongated driving part for providing a driving force to rotate the extension deck relative to the base deck.
The inclined angle formed by the extension deck and the base deck may be adjusted corresponding to an inclination angle of the base deck with respect to the horizontal plane when the base deck is inclined downwardly of the structure.
According to an embodiment of the present invention, a helicopter can provide a landing surface from which a helicopter can take off and land, and can be arranged to be inclined downwardly forward of the structure when it is not necessary to provide a landing surface during navigation, It is effective to reduce the wind load and improve the propulsion efficiency of the hull.
1 is a view illustrating an installation of a helideck according to an embodiment of the present invention.
FIG. 2 is a top view of the helideck shown in FIG. 1; FIG.
3 is a cross-sectional view taken along the line AA in Fig.
4 is a diagram illustrating a base driving unit of a helideck according to an embodiment of the present invention.
FIG. 5 is a view showing the helideck of FIG.
Fig. 6 is an enlarged perspective view of the helideck shown in Fig. 5;
FIG. 7 is a view showing a modification of the base driving unit shown in FIG.
8 is a view showing a state in which the base driver of FIG. 7 operates to tilt the base deck.
9 is a view showing a modification of the coupling structure of the base deck and the extension deck of Fig.
BRIEF DESCRIPTION OF THE DRAWINGS The present invention is capable of various modifications and various embodiments, and specific embodiments are illustrated in the drawings and described in detail in the detailed description. It is to be understood, however, that the invention is not to be limited to the specific embodiments, but includes all modifications, equivalents, and alternatives falling within the spirit and scope of the invention. DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS Hereinafter, the present invention will be described in detail with reference to the accompanying drawings.
DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENT Hereinafter, embodiments of the present invention will be described in detail with reference to the accompanying drawings. Referring to the accompanying drawings, the same or corresponding components are denoted by the same reference numerals, do.
FIG. 1 is a view showing an installation of a helideck according to an embodiment of the present invention. FIG. 2 is a top view of the helideck shown in FIG. 1, and FIG. 3 is a cross- to be. For reference, Fig. 1 shows the bow portion of the hull, and in Figs. 1 and 2, the left direction shows the bow direction.
1 to 3, the
The
The
For example, the rear end of the
The
The
The
The
In one example, the
Alternatively, the
4 is a diagram illustrating a base driving unit of a helideck according to an embodiment of the present invention. For reference, the extension deck (200 in Fig. 1) is omitted in Fig.
Referring to FIG. 4, the
For example, the
The
FIG. 5 is a view showing a helideck of FIG. 1 operating in an inclined manner forward and downward, and FIG. 6 is an enlarged perspective view of the helideck of FIG.
Hereinafter, the operation of the
1, the
In this case, the
The size of the
Referring to Figures 5 and 6, when the
In this case, the
At this time, the
The
More specifically, when the
In this case, the
Therefore, the resistance of the
The angle formed between the
FIG. 7 is a view showing a modified example of the base driving unit shown in FIG. 4, and FIG. 8 is a view showing a state in which the base driving unit of FIG. 7 operates so as to tilt the base deck. For reference, the extension deck (200 in Fig. 1) is omitted in Fig. 7 and Fig.
7 and 8, the base driving unit 300 'according to the present modification includes a
For example, although the
7, the
In this case, the
On the other hand, the
For example, when the height of the
On the other hand, the
9 is a view showing a modification of the coupling structure of the base deck and the extension deck of Fig.
Referring to FIG. 9, the
In this case, the
For example, the
It goes without saying that various devices for providing the driving force for rotating the
When the
When the
For example, when the rear end of the
In this case, the
As mentioned above, the helideck 10 according to the present embodiment can provide a landing surface on which a helicopter (not shown) can take off and land, So that it is possible to reduce the wind load acting on the
While the present invention has been particularly shown and described with reference to exemplary embodiments thereof, many modifications and changes may be made by those skilled in the art without departing from the spirit and scope of the invention as defined in the appended claims. The present invention can be variously modified and changed by those skilled in the art, and it is also within the scope of the present invention.
1: Ship 10: Helideck
20: Hull 30: Structure
100: Base deck 200: Extension deck
210: Hinge shaft 220:
221: Hydraulic cylinder 222: Support member
300, 300 ': Base drive unit 310: Hinge shaft
320: Hydraulic cylinder 331: First actuator
332: second actuator
Claims (7)
An extension deck disposed on both sides of the base deck and inclined relative to the base deck,
The base deck comprises:
Keep the helicopter horizontal to provide a landing surface for take-off and landing,
Operating in an inclined downward forward direction of the structure to reduce wind loads acting on the structure,
The extension deck is rotatably coupled to the base deck,
Wherein the inclination angle formed by the extension deck and the base deck is adjusted corresponding to an inclination angle of the base deck with respect to the horizontal plane when the base deck is inclined downward forward of the structure.
Further comprising: a base driver for providing a driving force for the base deck to operate in a horizontal or inclined manner.
The rear end of the base deck is hinged to all of the structure,
Wherein the base drive includes a hydraulic cylinder extending and retracting to rotate the base deck.
The base drive unit includes:
A first actuator for moving the front end of the base deck upward and downward; And
And a second actuator for moving the rear end portion of the base deck upward and downward.
Further comprising an elongated driver for providing a driving force to rotate the extension deck relative to the base deck.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
KR1020150050601A KR101711429B1 (en) | 2015-04-10 | 2015-04-10 | Helideck |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
KR1020150050601A KR101711429B1 (en) | 2015-04-10 | 2015-04-10 | Helideck |
Publications (2)
Publication Number | Publication Date |
---|---|
KR20160121098A KR20160121098A (en) | 2016-10-19 |
KR101711429B1 true KR101711429B1 (en) | 2017-03-02 |
Family
ID=57250827
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
KR1020150050601A KR101711429B1 (en) | 2015-04-10 | 2015-04-10 | Helideck |
Country Status (1)
Country | Link |
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KR (1) | KR101711429B1 (en) |
Families Citing this family (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN207775740U (en) * | 2017-05-08 | 2018-08-28 | 深圳市大疆创新科技有限公司 | Airplane parking area |
CN108945286A (en) * | 2018-07-04 | 2018-12-07 | 中国船舶工业集团公司第七0八研究所 | Active extendible helicopter platform device |
Family Cites Families (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
KR20130027672A (en) * | 2011-09-08 | 2013-03-18 | 삼성중공업 주식회사 | Helideck for offshore structure |
KR20130030027A (en) * | 2011-09-16 | 2013-03-26 | 안기주 | A ship with device for reducing air resistance |
KR20140043966A (en) * | 2012-10-02 | 2014-04-14 | 현대중공업 주식회사 | Heli deck apparatus |
KR101563663B1 (en) | 2013-09-24 | 2015-10-27 | 삼성중공업 주식회사 | Helicopter deck apparatus |
-
2015
- 2015-04-10 KR KR1020150050601A patent/KR101711429B1/en active IP Right Grant
Also Published As
Publication number | Publication date |
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KR20160121098A (en) | 2016-10-19 |
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