TWI682743B - Computer cockpit with food thermal insulation rack - Google Patents

Abstract

A computer cockpit includes a cockpit body, a computer host, a heat pipe and a thermal insulation rack. The computer host is disposed to the cockpit body, and the computer host includes a heat source. The heat pipe is connected to the heat source. The thermal insulation rack is disposed to the cockpit body and is connected to the heat pipe. The heat from the heat source is adapted to be conducted to the thermal insulation rack by the heat pipe to maintain the thermal insulation rack at a particular temperature.

Description

Computer cockpit with food insulation rack

The invention relates to a computer cockpit, and in particular to a computer cockpit with a food insulation rack.

With the rise of the e-sports industry, more and more products have emerged. In order to provide users with a more comfortable environment, vendors have developed products such as computer cockpits. The computer cockpit provides users with a higher degree of comfort, which can meet the needs of users sitting on the computer cockpit for a long time, and the computer cockpit is equipped with a computer host of higher specifications, thereby providing users with higher enjoyment. However, in the existing computer cockpit, the heat generated by the computer host is meaninglessly dissipated to the outside world. In other words, the heat generated by the computer host lacks good applications.

The invention provides a computer cockpit, which can use the heat generated by the computer host as the heat source of the food heat preservation rack, and help to efficiently use the heat generated by the computer host.

The computer cockpit of the present invention includes a cabin body, a computer host, a heat pipe, and an insulation rack. The computer host is arranged in the cabin body, and the computer host includes a heat source. The heat pipe is connected to the heat source. The heat preservation frame is arranged in the cabin body and connected to the heat pipe. The heat emitted by the heat source is suitable to be conducted to the heat preservation frame through the heat pipe, so that the heat preservation frame is maintained at a temperature.

In an embodiment of the invention, the above-mentioned heat preservation rack includes a box body and a heating module. The box body is fixed to the cabin body. The heating module is arranged under the box body and located on the heat conduction path of the heat pipe.

In an embodiment of the invention, the aforementioned heat pipe includes a heating section. The heating section is disposed in the heating module, and the heat conducted by the heating section is suitable to be conducted into the box body through the heating module to maintain the box body at this temperature.

In an embodiment of the present invention, the above heating module includes a heating element and a heat insulating element. The heating element is arranged below the box body. The heat insulation element is arranged below the heating element, and the heating section is located between the heating element and the heat insulation element.

In an embodiment of the present invention, the above-mentioned heating element is suitable for conducting the heat of the heating section into the box body, and the heat insulation element is suitable for isolating the heat of the heating section and the heating element in the box body.

In an embodiment of the invention, the above box has at least one opening, and at least one object to be heated is adapted to pass through the at least one opening and be placed in the box.

In an embodiment of the present invention, the above-mentioned heat preservation frame includes a fixing member connected to the box body, and the heat preservation frame is fixed to the cabin body through the fixing member.

In an embodiment of the invention, the aforementioned computer cockpit further includes a cooling The system is connected to the host computer, and the heat preservation rack is located on the heat conduction path of the cooling system.

In an embodiment of the invention, the above-mentioned cooling system includes a heat dissipating element, the heat pipe and a return pipe. The heat dissipation element is arranged in the cabin body. The heat pipe is connected between the computer host and the heat dissipation element. The return pipe is connected between the heat dissipation element and the computer host. The heat emitted by the heat source is suitable to be conducted to the heat dissipation element through the heat pipe, and the heat dissipation element is suitable to reduce the heat conducted by the heat pipe to the heat source and then conduct it back to the heat source through the return pipe.

In an embodiment of the present invention, the aforementioned heat pipe includes a water-cooled heat pipe, and the return pipe includes a water-cooled return pipe.

Based on the above, in the computer cockpit of the present invention, the heat emitted by the heat source is suitable to be conducted to the thermal insulation frame through the heat pipe to maintain the thermal insulation frame at a temperature. Accordingly, the computer cockpit of the present invention can use the heat generated by the computer host as the heat source of the food insulation rack, which helps to efficiently use the heat generated by the computer host.

In order to make the above-mentioned features and advantages of the present invention more obvious and understandable, the embodiments are specifically described below in conjunction with the accompanying drawings for detailed description as follows.

100‧‧‧ Computer cockpit

110‧‧‧ Cockpit body

120‧‧‧computer host

122‧‧‧heat source

130‧‧‧cooling system

132‧‧‧Cooling element

132a‧‧‧cold row

132b‧‧‧fan

134‧‧‧Heat pipe

134a‧‧‧Heating section

136‧‧‧Return tube

140‧‧‧Insulation rack

142‧‧‧Box

142a, 142b ‧‧‧ opening

144‧‧‧ heating module

144a‧‧‧Heating element

144b‧‧‧Insulation element

146‧‧‧Fittings

A‧‧‧Air

B1, B2‧‧‧ objects to be heated

FIG. 1 is a schematic diagram of a computer cockpit according to an embodiment of the invention.

FIG. 2 is a perspective schematic view of the heat preservation frame of FIG. 1.

FIG. 3 is an exploded schematic view of the heat preservation frame of FIG. 2.

FIG. 4 is a schematic view of the heat preservation frame of FIG. 2 provided with fixing members.

5 is a schematic diagram of the cooling system of FIG.

FIG. 1 is a schematic diagram of a computer cockpit according to an embodiment of the invention. FIG. 1 schematically shows the host computer 120, the heat source 122, the cooling system 130, the heat dissipation element 132, the heat pipe 134, the return pipe 136, and the heat preservation frame 140 in broken lines. Please refer to FIG. 1. The computer cabin 100 of this embodiment includes a cabin body 110, a computer main body 120, a heat pipe 134 and an insulation rack 140. The computer host 120 is disposed in the cabin body 110, and the computer host 120 includes a heat source 122. The heat pipe 134 is connected to the heat source 122. The heat preservation frame 140 is disposed in the cabin body 110 and connected to the heat pipe 134. Accordingly, the heat generated by the heat source 122 is conducted to the heat preservation frame 140 through the heat pipe 134, so that the heat preservation frame 140 is maintained at a temperature. Therefore, the computer cockpit 100 of this embodiment can use the heat generated by the computer host 120 as the heat source of the heat preservation rack 140, which helps to efficiently use the heat generated by the computer host 120.

FIG. 2 is a perspective schematic view of the heat preservation frame of FIG. 1. FIG. 3 is an exploded schematic view of the heat preservation frame of FIG. 2. FIG. 4 is a schematic view of the heat preservation frame of FIG. 2 provided with fixing members. Please refer to FIGS. 1, 3 and 4, the heat preservation frame 140 includes a box 142, a heating module 144 and a fixing member 146. The fixing member 146 is connected to the box body 142, and the heat preservation frame 140 is further fixed to the cabin body 110 through the fixing member 146. The heating module 144 is disposed below the box 142, and the heating module 144 is located on the heat conduction path of the heat pipe 134.

Please refer to FIG. 1, FIG. 2 and FIG. 3, the heating module 144 of this embodiment includes a heating element 144 a and a heat insulating element 144 b. The heating element 144a is provided in the box Below 142. The heat insulating element 144b is disposed below the heating element 144a. A heating section 134a of the heat pipe 134 is disposed between the heating element 144a and the heat insulating element 144b of the heating module 144. Accordingly, the heat conducted by the heat pipe 134 can be conducted to the heating element 144a of the heating module 144, and the heat of the heating element 144a can be conducted into the box 142, so that the box 142 can be maintained at this temperature. In addition, the heat insulation element 144b can isolate the heat of the heating element 144a and the heat of the heating section 134a of the heat pipe 134 within the box 142, so that the heat preservation rack 140 of the present invention can have a better heat preservation effect.

In this embodiment, the box 142 of the heat preservation rack 140 has at least one opening (such as opening 142a and opening 142b), and at least one object to be heated (such as object B1 and object B2 to be heated) can pass through the opening 142a, 142b is further placed in the box 142. The object to be heated B1 is, for example, food, and the object to be heated B2 is, for example, a drink. Preferably, after the object B1 and the object B2 to be heated pass through the openings 142a and 142b, they can be directly carried and contacted with the heating element 144a of the heating module 144 to obtain a better heating and heat preservation effect.

5 is a schematic diagram of the cooling system of FIG. Please refer to FIGS. 1, 2 and 5. The computer cabin 100 of this embodiment further includes a cooling system 130. The cooling system 130 includes a heat dissipating element 132, the aforementioned heat pipe 134 and a return pipe 136. The heat pipe 134 includes a water-cooled heat pipe, and the return pipe 136 includes a water-cooled return pipe. The heat preservation rack 140 is located on the heat conduction path of the heat pipe 134 of the cooling system 130. The heat dissipation element 132 includes a cold exhaust 132a (or condenser) and a fan 132b. The heat dissipation element 132 is disposed in the cabin body 110. The heat pipe 134 is connected between the computer host 120 and the heat dissipation element 132. The return pipe 136 is connected to the heat dissipation element 132 and the host computer 120 between. The heat emitted by the heat source 122 can be conducted to the cold row 132a of the heat dissipating element 132 through the heat pipe 134. The fan 132b can draw the outside air A to the cold row 132a, thereby cooling the liquid in the cold row 132a. Then, the cooled liquid can be transported back to the heat source 122 through the return pipe 136, so as to lower the temperature of the heat source 122.

In summary, in the computer cockpit of the present invention, the heat emitted by the heat source is conducted to the heat preservation frame through the heat pipe to maintain the temperature of the heat preservation frame. Therefore, the computer cockpit of the present invention can use the heat generated by the computer host as the heat source of the heat preservation rack, which helps to efficiently use the heat generated by the computer host.

Although the present invention has been disclosed as above with examples, it is not intended to limit the present invention. Any person with ordinary knowledge in the technical field can make some changes and modifications without departing from the spirit and scope of the present invention. The scope of protection of the present invention shall be subject to the scope defined in the appended patent application.

100‧‧‧ Computer cockpit

110‧‧‧ Cockpit body

120‧‧‧computer host

122‧‧‧heat source

130‧‧‧cooling system

132‧‧‧Cooling element

134‧‧‧Heat pipe

136‧‧‧Return tube

140‧‧‧Insulation rack

Claims (9)

A computer cabin includes: a cabin cabin; a computer host, which is installed in the cabin cabin, and the computer host includes a heat source; a heat pipe, connected to the heat source; and an insulation rack, which is installed in the cabin cabin And connected to the heat pipe, wherein the heat emitted by the heat source is suitable to be conducted to the heat preservation frame through the heat pipe to maintain the temperature of the heat preservation frame, wherein the heat preservation frame includes: a box body, fixed to The cockpit body; and a heating module, which is arranged below the box body and located on the heat conduction path of the heat pipe. The computer cockpit described in item 1 of the patent application scope, wherein the heat pipe includes a heating section disposed in the heating module, and the heat conducted by the heating section is suitable to be conducted into the box body through the heating module To maintain the box at this temperature. The computer cockpit described in item 2 of the patent application scope, wherein the heating module includes: a heating element disposed below the box; and a heat insulating element disposed below the heating element, and the heating section Located between the heating element and the heat insulating element. The computer cockpit of claim 3, wherein the heating element is adapted to conduct the heat of the heating section into the box body, and the heat insulating element is adapted to isolate the heat of the heating section and the heating element from the Inside the box. The computer cockpit of claim 1, wherein the box has at least one opening, and at least one object to be heated is adapted to pass through the at least one opening and be placed in the box. The computer cockpit described in item 1 of the patent application scope, wherein the heat preservation rack includes: a fixing member connected to the box body, and the heat preservation rack is fixed to the cabin cabin body through the fixing member. The computer cockpit described in item 1 of the scope of the patent application further includes: a cooling system connected to the computer host, and the heat preservation rack is located on the heat conduction path of the cooling system. The computer cockpit described in item 7 of the patent application scope, wherein the cooling system includes: a heat dissipating element disposed in the cockpit body; the heat pipe connected between the computer main body and the heat dissipating element; and a return pipe , Connected between the heat dissipation element and the computer host, wherein the heat emitted by the heat source is suitable for conduction to the heat dissipation element through the heat pipe, and the heat dissipation element is suitable for further cooling the heat conducted by the heat pipe Conducted back to the heat source through the return pipe. The computer cockpit described in item 8 of the patent application scope, wherein the heat pipe includes a water-cooled heat pipe, and the return pipe includes a water-cooled return pipe.

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