KR20130034083A

KR20130034083A - Helideck having solar cell

Info

Publication number: KR20130034083A
Application number: KR1020110097911A
Authority: KR
Inventors: 서형석; 박주신; 김태우; 전상배
Original assignee: 삼성중공업 주식회사
Priority date: 2011-09-28
Filing date: 2011-09-28
Publication date: 2013-04-05

Abstract

PURPOSE: A helideck with a solar cell is provided to increase the utilization of a helideck by converting sunlight into electric energy. CONSTITUTION: A helideck(100) with a solar cell(130) comprises a body(110) and a transparent plate(120). The transparent plate is installed in the upper part of the body. Aircrafts take off and land on the transparent plate. Sunlight incoming to the transparent plate is converted into electric energy. The transparent plate comprises a tempered glass. A buffer member(140) is arranged on one or more of the top and the bottom of the solar cell.

Description

HELIDECK HAVING SOLAR CELL}

The present invention relates to a heli-deck with a solar cell.

Various ships or offshore structures are provided with a landing pad (hereinafter referred to as a "heli deck") where aircraft such as a helicopter can take off and land as needed. The heli-deck is designed to withstand the weight of the aircraft during takeoff and landing. For example, the heli-deck can be made of an aluminum alloy with excellent marine corrosion resistance and strength.

In the past, the use of the heli-deck was limited to the take-off and landing of the aircraft, so the utilization of the heli-deck was low. That is, the heli-deck was left for a long time as it is exposed to the external environment in the absence of the aircraft.

Thus, there is a need to increase the utilization of the HeliDeck exposed to the external environment in the absence of a vehicle.

An embodiment of the present invention is to provide a heli-deck with a solar cell that converts the light energy of the sun incident on the heli-deck into electrical energy in order to increase the utilization of the heli-deck exposed to the external environment in the absence of the vehicle.

According to an aspect of the invention, the body of the heli-deck; A transparent plate installed at an upper portion of the body and for taking off and landing of a vehicle; And a solar cell installed below the transparent plate and converting light energy of the sun incident on the transparent plate into electrical energy.

The transparent plate may include tempered glass.

A buffer member may be provided at one or more of the top and bottom of the solar cell.

The solar cell may have a structure in which modules consisting of two or more cells are arranged in a predetermined shape, and the buffer member may be provided on an outer circumferential surface of the cell.

It may further include a piezoelectric element installed in the shock absorbing member, and converts the pressure caused by the weight of the air vehicle landing on the transparent plate into electrical energy.

The piezoelectric element may be installed in a form in which two or more are stacked inside the buffer member.

The display device may further include a storage battery electrically connected to at least one of the piezoelectric element and the solar cell, and configured to charge electrical energy converted by at least one of the piezoelectric element and the solar cell.

The heli-deck having a solar cell according to an embodiment of the present invention converts the light energy of the sun incident on the heli-deck into electrical energy, thereby increasing the utilization of the heli-deck exposed to the external environment in the absence of a vehicle.

In addition, it is possible to further expand the utilization of the heli-deck by converting the pressure caused by the weight of the aircraft landing on the heli-deck into electrical energy.

1 illustrates a heli-deck with a solar cell according to an embodiment of the present invention.
2 is a cross-sectional view of the heli-deck of FIG.
3 and 4 illustrate an installation form of a solar cell installed in the heli-deck of FIG. 2.
Figure 5 shows a form in which a piezoelectric element is installed on the heli-deck equipped with a solar cell according to another embodiment of the present invention.
FIG. 6 illustrates an installation form of a piezoelectric element provided in the heli deck of FIG. 5.

Hereinafter, embodiments of the present invention will be described in detail with reference to the accompanying drawings.

1 illustrates a heli-deck with a solar cell according to an embodiment of the present invention. 2 is a cross-sectional view of the heli-deck of FIG. 3 and 4 illustrate an installation form of a solar cell installed in the heli-deck of FIG. 2.

Referring to FIG. 1, the helicopter deck 100 according to an embodiment of the present invention may be installed on the deck of the ship 10 so that a vehicle such as a helicopter can land or take off. In addition, the heli-deck 100 is utilized as a means for converting the sun's light energy into electrical energy in the absence of a vehicle. Hereinafter, a case where the heli-deck 100 is installed in the vessel 10, but the heli-deck 100 is to be installed in offshore structures such as floating production, storage, and offloading facility (FPSO) or land buildings such as high-rise building Can be.

2, the heli-deck 100 according to the embodiment of the present invention includes a body 110, a transparent plate 120, a solar cell 130, and a buffer member 140.

The transparent plate 120 installed above the body 110 and taking off and landing of the aircraft is manufactured to withstand the weight of the vehicle during takeoff and landing of the vehicle. The transparent plate 120 may include, for example, tempered glass. Here, the tempered glass may include a low iron tempered glass. The transparent plate 120 may be manufactured in the form of one glass plate, or may be manufactured in the form of a combination of several glass plates.

The solar cell 130 is installed below the transparent plate 120 and converts the light energy of the sun incident on the transparent plate 120 into electrical energy. The solar cell 130 may include, for example, a silicon solar cell, a compound semiconductor solar cell, or the like. Here, the buffer member 140 may be provided at one or more of the top and bottom of the solar cell 130.

The buffer member 140 may include a rubber pad, and the transparent plate 120 and the solar cell 130 may be protected by the buffering action of the buffer member 140 to improve durability. In addition, the piezoelectric effect of the piezoelectric element 150 to be described later may be increased.

3 and 4, the solar cell 130 described above may be provided in a structure in which a module 131 including two or more cells 132 is arranged in a predetermined form. At this time, the buffer member 140 is provided on the outer circumferential surface of each cell 132, the light energy of the sun incident on the transparent plate 120 is transmitted to the solar cell 130 more effectively without being disturbed by the buffer member 140. Be sure to

Figure 5 shows a form in which a piezoelectric element is installed on the heli-deck equipped with a solar cell according to another embodiment of the present invention. And Figure 6 shows the installation form of the piezoelectric element provided in the heli deck of FIG.

Referring to FIG. 5, the piezoelectric element 150 may be installed in the heli-deck 100 having the solar cell 130 described above.

The piezoelectric element 150 is installed in the shock absorbing member 140, and converts the pressure due to the weight of the aircraft landing on the transparent plate 120 into electrical energy.

In this case, referring to FIG. 6, the piezoelectric element 150 may be installed in a form in which two or more are stacked inside the buffer member 140.

As described above, the piezoelectric effect of the piezoelectric element 150 may be enhanced by stacking two or more piezoelectric elements 150 inside the buffer member 140.

Meanwhile, a storage battery electrically connected to at least one of the piezoelectric element 150 and the solar cell 130 and charging the electrical energy converted by at least one of the piezoelectric element 150 and the solar cell 130 (not shown). May be provided.

The storage battery (not shown) may include a nickel cadmium battery, a lead storage battery, a nickel-hydrogen battery and the like. As such, the electrical energy charged in the storage battery (not shown) may be utilized as an energy source of various equipment of ships or offshore structures.

The foregoing has shown and described specific embodiments. However, the present invention is not limited to the above embodiments, and those skilled in the art may make various changes without departing from the spirit of the technical idea of the invention as set forth in the claims below. .

100: heli-deck 110: body
120: transparent plate 130: solar cell
132: cell 140: rubber sheet
150: piezoelectric element

Claims

The body of the heli-deck;
A transparent plate installed at an upper portion of the body and for taking off and landing of a vehicle; And
A solar cell installed under the transparent plate and converting light energy of the sun incident on the transparent plate into electrical energy;
Heli deck with a solar cell comprising a.

The method of claim 1,
The transparent plate is a heli-deck with a solar cell comprising a tempered glass.

The method of claim 1,
Heli deck with a solar cell, characterized in that the buffer member is provided on at least one of the top and bottom of the solar cell.

The method of claim 3,
The solar cell is a heli-deck having a solar cell, characterized in that the module consisting of two or more cells (cell) is arranged in a predetermined form, the buffer member is provided on the outer peripheral surface of the cell.

The method of claim 3,
And a piezoelectric element installed on the shock absorbing member, the piezoelectric element converting the pressure caused by the weight of the flying vehicle to the transparent plate into electrical energy.

The method of claim 5,
The piezoelectric element is a heli-deck having a solar cell, characterized in that installed in the form of two or more stacked inside the buffer member.

The method of claim 5,
And a storage battery electrically connected to at least one of the piezoelectric element and the solar cell, the storage cell charging electrical energy converted by at least one of the piezoelectric element and the solar cell.