KR101727800B1 - Device for heating hellideck - Google Patents
Device for heating hellideck Download PDFInfo
- Publication number
- KR101727800B1 KR101727800B1 KR1020150063268A KR20150063268A KR101727800B1 KR 101727800 B1 KR101727800 B1 KR 101727800B1 KR 1020150063268 A KR1020150063268 A KR 1020150063268A KR 20150063268 A KR20150063268 A KR 20150063268A KR 101727800 B1 KR101727800 B1 KR 101727800B1
- Authority
- KR
- South Korea
- Prior art keywords
- heater
- pancake
- cover
- concave groove
- groove
- Prior art date
Links
- 238000010438 heat treatment Methods 0.000 title description 4
- 235000012771 pancakes Nutrition 0.000 claims abstract description 58
- 239000000945 filler Substances 0.000 claims abstract description 10
- 239000007788 liquid Substances 0.000 claims abstract description 4
- 239000000843 powder Substances 0.000 claims abstract description 4
- 230000008014 freezing Effects 0.000 abstract description 9
- 238000007710 freezing Methods 0.000 abstract description 9
- 239000000463 material Substances 0.000 abstract description 5
- JEIPFZHSYJVQDO-UHFFFAOYSA-N iron(III) oxide Inorganic materials O=[Fe]O[Fe]=O JEIPFZHSYJVQDO-UHFFFAOYSA-N 0.000 abstract description 2
- 230000008018 melting Effects 0.000 abstract 2
- 238000002844 melting Methods 0.000 abstract 2
- 229910052782 aluminium Inorganic materials 0.000 description 4
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 4
- 238000001125 extrusion Methods 0.000 description 3
- 230000008878 coupling Effects 0.000 description 2
- 238000010168 coupling process Methods 0.000 description 2
- 238000005859 coupling reaction Methods 0.000 description 2
- 230000005611 electricity Effects 0.000 description 2
- 229910000831 Steel Inorganic materials 0.000 description 1
- 238000009825 accumulation Methods 0.000 description 1
- 230000002411 adverse Effects 0.000 description 1
- 239000004020 conductor Substances 0.000 description 1
- 238000007796 conventional method Methods 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 238000007667 floating Methods 0.000 description 1
- 238000005304 joining Methods 0.000 description 1
- 239000007791 liquid phase Substances 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 239000002923 metal particle Substances 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 239000002245 particle Substances 0.000 description 1
- 230000002265 prevention Effects 0.000 description 1
- 239000013535 sea water Substances 0.000 description 1
- 239000007787 solid Substances 0.000 description 1
- 238000005507 spraying Methods 0.000 description 1
- 239000010959 steel Substances 0.000 description 1
- 238000003860 storage Methods 0.000 description 1
- 239000011800 void material Substances 0.000 description 1
Images
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
-
- 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
-
- H—ELECTRICITY
- H05—ELECTRIC TECHNIQUES NOT OTHERWISE PROVIDED FOR
- H05B—ELECTRIC HEATING; ELECTRIC LIGHT SOURCES NOT OTHERWISE PROVIDED FOR; CIRCUIT ARRANGEMENTS FOR ELECTRIC LIGHT SOURCES, IN GENERAL
- H05B3/00—Ohmic-resistance heating
- H05B3/10—Heating elements characterised by the composition or nature of the materials or by the arrangement of the conductor
-
- H—ELECTRICITY
- H05—ELECTRIC TECHNIQUES NOT OTHERWISE PROVIDED FOR
- H05B—ELECTRIC HEATING; ELECTRIC LIGHT SOURCES NOT OTHERWISE PROVIDED FOR; CIRCUIT ARRANGEMENTS FOR ELECTRIC LIGHT SOURCES, IN GENERAL
- H05B2214/00—Aspects relating to resistive heating, induction heating and heating using microwaves, covered by groups H05B3/00, H05B6/00
- H05B2214/02—Heaters specially designed for de-icing or protection against icing
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- Ocean & Marine Engineering (AREA)
- Architecture (AREA)
- Civil Engineering (AREA)
- Structural Engineering (AREA)
- Resistance Heating (AREA)
Abstract
The present invention proposes a device for preventing freezing of frost on the top surface of a helideck or for melting snow. In the apparatus of the present invention, the concave grooves (12, 14) are formed along the longitudinal direction, and a heater receiving groove (16) corresponding to the upper outline of the heater is formed on the bottom surface of the concave groove (10); And a cover (20) housed in the concave groove of the pancake and having a heater receiving groove (26) corresponding to the lower outer shape of the heater formed on the bottom surface and an upper surface forming the same plane as the upper surface of the pancake. The heater accommodating groove of the cover and the heater accommodating groove of the pancake accommodate the heater 30 to generate heat by application of power, thereby preventing freezing or melting the rust. The gap between the heater, the cover and the upper surface portion of the pancake is filled with liquid or powder filler material having thermal conductivity to maximize heat conduction efficiency.
Description
The present invention relates to a helideck, and more particularly to a helideck which is filled with a filler having a high thermal conductivity around the heater while filling a heater for generating heat on the top surface of the helideck to prevent the occurrence of freezing, To an icemaker preventing device of a helideck configured to enable efficient heat conduction.
Generally, an offshore plant such as a drill ship, FPSO (Floating, Production, Storage and Offloading) or a ship staying in the sea for a long time is generally operated by a helicopter in order to make the movement of the personnel quick and smooth . In order to use the helicopter, the helicopter must be installed on the offshore structure or the ship so that the helicopter can take off and land.
The helideck is composed of a pancake having a deck floor on which a helicopter is taken off and landed, and a support for supporting the pancake. The pancakes are formed, for example, by connecting a plurality of flanks, which are aluminum extruded materials, to form a deck floor on which the helicopter is taken off and landed on the upper surface. The pancake supporting part supporting the pancake is generally composed of a combination of a plurality of aluminum H beams and steel H beams supporting the pancakes in the lower part.
It can be said that the helicopter taking off and landing using such a helideck is much affected by the weather. In particular, when an offshore structure or vessel equipped with a helideck is operated in the polar regions, ice accumulation occurs on the helideck or icing occurs due to moisture. As snow accumulates on the heli-deck and freezing occurs, it can adversely affect the take-off and landing of the helicopter, which can cause a dangerous situation especially for those who use the helicopter. Therefore, snow or ice on the top of the heli-deck must be effectively removed as soon as possible.
According to the conventional technique for heating the top surface of the helideck, a dedicated heater for generating heat by supplying electricity is provided on the bottom surface. However, since the heater is directly exposed to a low-temperature atmosphere, There was a drawback. Korean Patent Laid-Open Publication No. 10-2015-0026020 proposes a technique of removing icing by spraying seawater heated by a heating device on the top surface of a helideck using a nozzle. However, such conventional technology is expected to be difficult to commercialize because of various disadvantages due to enlargement of the apparatus.
It is an object of the present invention to provide a device for preventing freezing of ice on the heli-deck or for removing snow or preventing it in advance.
It is a more specific object of the present invention to provide an effective anti-icing device by using a heater that generates heat by supplying electric power and sufficiently securing thermal conductivity.
According to an aspect of the present invention, there is provided an apparatus for preventing freezing of a heli-deck, comprising: a concave groove formed along a longitudinal direction of the helix; and a heater receiving groove corresponding to an upper outline of the heater is formed on a bottom surface of the concave groove A pancake having an upper surface portion; A cover accommodated in the concave groove of the pancake and having a heater receiving groove corresponding to a lower outer shape of the heater formed on the bottom surface and having an upper surface forming the same plane as the upper surface of the pancake; And a heater accommodated in the heater receiving groove of the cover and the heater receiving groove of the pancake and generating heat by application of power.
According to the embodiment of the present invention, the concave groove is constituted by a first concave groove formed concavely in the upper surface portion and a second concave groove formed partially concave on the bottom surface of the first concave groove. The cover is composed of a flange portion accommodated in the first concave groove and a protrusion portion protruding from the bottom surface of the flange portion and accommodated in the second concave groove.
According to another embodiment of the present invention, the gap formed between the heater, the cover and the upper surface portion of the pancake is filled with filler in a liquid or powder state having thermal conductivity, thereby maximizing the efficiency of heat conduction.
According to another embodiment of the present invention, the cover is fixed to the pancake by a screw-engaging member, and the lower end of the screw-engaging member is screwed to the pancake without protruding to the lower end of the pancake.
According to the present invention having such a technical structure, it is possible to minimize the heat loss due to conduction of heat to the pancake other than the pancake by filling the heater at a certain depth on the upper surface of the pancake. This means that the heat generated by the heater is effectively conducted in the lateral direction from the upper portion of the pancake.
In the present invention, it can be seen that the empty space around the heater embedded at a certain depth from the upper part of the pancake formed by extrusion of aluminum is filled with the filler having high thermal conductivity. Thus, it can be seen that a sufficient amount of heat is conducted to the upper surface of the pancake through substantially efficient heat conduction while substantially preventing heat loss through the void space.
The structure for embedding the heater according to the present invention and the structure for increasing the thermal conductivity by filling the space around the buried heater with a material having high thermal conductivity can quickly and effectively remove rust or ice accumulated in the deck floor formed on the upper surface of the pancake In addition, it is possible to expect an effect of sufficiently preventing the occurrence of such freezing by preheating.
BRIEF DESCRIPTION OF THE DRAWINGS Fig. 1 is an exemplary diagram showing an exploded view of an inventive pancake. Fig.
2 is a cross-sectional exemplary view of a pancake of the present invention.
Hereinafter, the present invention will be described in more detail based on the embodiments illustrated in FIGS. 1 and 2. FIG. 1 and 2, in the helideck freezing prevention apparatus according to the present invention, a
The
When the
In the illustrated embodiment, the second
A
The
When the
The lower part of the
Therefore, even when the
As described above, when the
Therefore, the gap between the
Accordingly, in the present invention, a filler is injected between the
Therefore, it is preferable that such a filler is formed of a thermally conductive material, and it is possible to use a gel state or a liquid state, or to use solid particles in the same state as a powder. Alternatively, it is also possible to use metal particles having high thermal conductivity mixed with a filler of a certain liquid phase.
For example, it is considered that the filler material should be filled around the
As described above, according to the present invention, the main technical theme is to maximize the heat conduction efficiency by embedding the heat ray for preventing freezing of the helideck at a predetermined depth from the upper part of the pancake. In order to improve heat conduction efficiency or ensure structural stability, a structure between the
It will be understood by those skilled in the art that various changes in form and details may be made therein without departing from the spirit and scope of the invention as defined by the appended claims.
10 ..... Pancakes
11 ..... upper part
12 ..... first concave groove
14 ..... second concave groove
16 ..... Heater accommodating groove
20 ..... cover
22 ..... flange section
24 ..... protrusion
26 ..... Heater accommodating groove
30 ..... Heater
Claims (4)
A cover accommodated in the concave groove of the pancake and having a heater receiving groove corresponding to an upper outer shape of the heater formed on the bottom surface and having an upper surface forming the same plane as the upper surface of the pancake; And
A heater accommodated in the heater receiving groove of the cover and the heater receiving groove of the pancake and generating heat by application of power;
/ RTI >
Wherein the concave groove is composed of a first concave groove formed concavely in an upper surface portion and a second concave groove formed partially concave on a bottom surface of the first concave groove,
Wherein the cover comprises a flange portion accommodated in the first concave groove and a protruding portion protruding from the bottom surface of the flange portion and received in the second concave groove.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
KR1020150063268A KR101727800B1 (en) | 2015-05-06 | 2015-05-06 | Device for heating hellideck |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
KR1020150063268A KR101727800B1 (en) | 2015-05-06 | 2015-05-06 | Device for heating hellideck |
Publications (2)
Publication Number | Publication Date |
---|---|
KR20160131279A KR20160131279A (en) | 2016-11-16 |
KR101727800B1 true KR101727800B1 (en) | 2017-04-17 |
Family
ID=57540451
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
KR1020150063268A KR101727800B1 (en) | 2015-05-06 | 2015-05-06 | Device for heating hellideck |
Country Status (1)
Country | Link |
---|---|
KR (1) | KR101727800B1 (en) |
Families Citing this family (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
KR101877956B1 (en) * | 2017-11-06 | 2018-07-12 | 주식회사 송산특수엘리베이터 | Heliport Elevator Capable of Improving Balance Safety and Wind Pressure Resistance and Preventing Infiltration of Rainwater and Icing |
KR101981735B1 (en) * | 2018-07-20 | 2019-05-23 | 세보테크 주식회사 | Anti-freezing Helideck Plank Using Heating Medium |
KR101997542B1 (en) * | 2018-07-20 | 2019-07-08 | 세보테크 주식회사 | A Guide Pipe of Heating Medium for Helideck Plank |
KR102304872B1 (en) * | 2020-10-30 | 2021-09-27 | 주식회사 월드디엔씨 | Aluminum deck system |
Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP2004360221A (en) * | 2003-06-02 | 2004-12-24 | Aero Facility Kk | Heliport and deck material thereof |
JP2010156155A (en) * | 2008-12-27 | 2010-07-15 | Aero Facility Kk | Heliport and deck material for the same |
KR101205225B1 (en) | 2012-09-20 | 2012-11-27 | 경도에어로 주식회사 | Self-assembly heliport |
KR101451087B1 (en) | 2013-06-07 | 2014-10-15 | 세보테크 주식회사 | Helicopter deck plank for offshore structure to install heat tracing cable |
-
2015
- 2015-05-06 KR KR1020150063268A patent/KR101727800B1/en active IP Right Grant
Patent Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP2004360221A (en) * | 2003-06-02 | 2004-12-24 | Aero Facility Kk | Heliport and deck material thereof |
JP2010156155A (en) * | 2008-12-27 | 2010-07-15 | Aero Facility Kk | Heliport and deck material for the same |
KR101205225B1 (en) | 2012-09-20 | 2012-11-27 | 경도에어로 주식회사 | Self-assembly heliport |
KR101451087B1 (en) | 2013-06-07 | 2014-10-15 | 세보테크 주식회사 | Helicopter deck plank for offshore structure to install heat tracing cable |
Also Published As
Publication number | Publication date |
---|---|
KR20160131279A (en) | 2016-11-16 |
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A201 | Request for examination | ||
E902 | Notification of reason for refusal | ||
E601 | Decision to refuse application | ||
AMND | Amendment | ||
X701 | Decision to grant (after re-examination) | ||
GRNT | Written decision to grant |