CN111186581A - Airborne food heating assembly - Google Patents
Airborne food heating assembly Download PDFInfo
- Publication number
- CN111186581A CN111186581A CN201911270968.5A CN201911270968A CN111186581A CN 111186581 A CN111186581 A CN 111186581A CN 201911270968 A CN201911270968 A CN 201911270968A CN 111186581 A CN111186581 A CN 111186581A
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- CN
- China
- Prior art keywords
- heating
- compartment
- airborne
- water tank
- frame
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
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- 238000010438 heat treatment Methods 0.000 title claims abstract description 99
- 235000013305 food Nutrition 0.000 title abstract description 16
- 239000008236 heating water Substances 0.000 claims abstract description 37
- 230000037213 diet Effects 0.000 claims abstract description 12
- 235000005911 diet Nutrition 0.000 claims abstract description 12
- 239000002699 waste material Substances 0.000 claims description 7
- 230000035943 smell Effects 0.000 claims 1
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 abstract description 25
- 239000010813 municipal solid waste Substances 0.000 abstract description 11
- 239000003651 drinking water Substances 0.000 abstract description 4
- 235000020188 drinking water Nutrition 0.000 abstract description 4
- 238000004026 adhesive bonding Methods 0.000 abstract description 3
- 230000035622 drinking Effects 0.000 abstract description 3
- 230000003647 oxidation Effects 0.000 abstract description 3
- 238000007254 oxidation reaction Methods 0.000 abstract description 3
- 210000001503 joint Anatomy 0.000 abstract 2
- 230000005670 electromagnetic radiation Effects 0.000 description 3
- 238000009825 accumulation Methods 0.000 description 2
- 230000006978 adaptation Effects 0.000 description 2
- 230000017525 heat dissipation Effects 0.000 description 2
- 238000012986 modification Methods 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- 238000013021 overheating Methods 0.000 description 2
- 125000004122 cyclic group Chemical group 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 238000009792 diffusion process Methods 0.000 description 1
- 230000002349 favourable effect Effects 0.000 description 1
- 235000021268 hot food Nutrition 0.000 description 1
- 239000012774 insulation material Substances 0.000 description 1
- 230000002452 interceptive effect Effects 0.000 description 1
- 239000007788 liquid Substances 0.000 description 1
- 238000012544 monitoring process Methods 0.000 description 1
- 235000019659 mouth feeling Nutrition 0.000 description 1
- 238000004321 preservation Methods 0.000 description 1
- 230000002265 prevention Effects 0.000 description 1
- 230000005855 radiation Effects 0.000 description 1
- 238000004064 recycling Methods 0.000 description 1
- 230000007306 turnover Effects 0.000 description 1
Images
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D11/00—Passenger or crew accommodation; Flight-deck installations not otherwise provided for
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Devices For Warming Or Keeping Food Or Tableware Hot (AREA)
Abstract
The invention provides an airplane onboard diet heating assembly. The assembly consists of a frame, a control panel, a heating box, a heating water tank, a water accumulating box, a storage compartment, a spare water tank compartment, a garbage can compartment and a garbage can. Wherein: the frame is fixed by adopting a honeycomb plate and profile parts through a screw connection and gluing mode; the heating box and the frame are electrically connected through an electric connector in a butt joint mode, and are fixed in a bolt and nut connection mode; the heating water tank is in butt joint with the frame through an electric connector and is fixed in a limiting mode; the storage compartment, the spare water tank compartment and the garbage can compartment are provided with door components which can be opened or closed, and each door component is provided with two door locks to realize double locking; the heating of food and drinking water is realized through the electric control system in the heating box and the heating water tank, and the whole device adopts a shielding cable and solves the electromagnetic shielding problem of airborne equipment through conductive oxidation treatment. The invention greatly improves the food and water drinking guarantee level in the air and ensures the flight safety.
Description
Technical Field
The invention relates to a diet heating assembly, in particular to an onboard diet heating assembly used on a special airplane.
Background
The special airplane has narrow structural space, low air pressure and temperature during high-altitude flight, large vibration bump and difficult food and water drinking guarantee for crew. At the present stage, the main means of the food and water drinking guarantee of the aircrew is to carry a vacuum cup, a vacuum bottle and uncooked and cold convenient food, so that the mouth feeling is not added, the air dining difficulty is high, modern medical science proves that the hot food guarantee is more favorable for people to quickly recover physical strength, and the battle capacity of troops is improved, so that the flight efficiency in long voyage is improved.
Under the prior art condition, various sensors, heating pipes, fans, heat insulation materials, chips for circuit design and other electronic components are mature products, and mature food heating and drinking water heating equipment is also arranged in actual life, but is influenced by the working environment and the space environment of the airplane, and the equipment can not be simply transplanted to a special airplane. Therefore, an onboard diet heating component which can be applied to a special airplane needs to be researched and developed.
Disclosure of Invention
In view of the above problems, an object of the present invention is to provide an onboard food heating assembly for aircraft, which is mainly used to provide heating and hot water guarantee for the crew, can reliably store random articles and data, and has the functions of food storage and waste recycling.
In order to achieve the aim, the technical scheme provided by the invention is to provide an onboard food heating assembly which comprises a frame 4, a control panel 1, an onboard heating box 2, an onboard heating water tank 3, storage compartments 5 and 6, a spare water tank compartment 7, a garbage bin compartment 8 and a garbage bin 9,
the heating component frame 4 is a cuboid with an open front face formed by honeycomb plates, and the internal space of the heating component frame is divided into an upper part, a middle part and a lower part;
the upper part is provided with a control panel 1 which comprises a control component of an onboard heating box 2 and a control component of the onboard heating water tank 3;
an airborne heating box 2 and an airborne heating water tank 3 are arranged in the middle, wherein the airborne heating box 2 is electrically connected with the airborne heating box control assembly and is positioned below the airborne heating control assembly, and the airborne heating water tank 3 is electrically connected with the airborne heating water tank control assembly and is positioned below the airborne heating water tank control assembly;
the lower part sets up storing compartment 5, 6 reserve tank compartment 7 dustbin compartment 8, storing compartment 5, 6 are including big storing compartment 5 and little storing compartment 6, wherein, big storing compartment 5 sets up machine-mounted heating box 2 below, little storing compartment 6 sets up machine-mounted heating box 3 below, reserve tank compartment 7 with dustbin compartment 8 sets up side by side little storing compartment 6 below, dustbin 9 place in dustbin compartment 8.
Further, the frame 4 is fixed by a honeycomb plate and profile parts in a screw joint and gluing mode.
Further, an electrical socket 11 and a heat dissipation hole 10 for supplying power to the onboard heating box 2 and the onboard heating water box 3 are arranged on the back of the heating assembly.
Further, the length of the onboard heating water tank 3 is smaller than that of the frame, so that the difference between the water outlet of the onboard heating water tank 3 and the front surface of the frame is provided with the water accumulating box 12.
Further, be provided with stopper right angle knob 14 on the frame 4, it is right control panel 1, machine carries heating tank 2, machine carries heating tank 3, ponding box 12, storing compartment 5, 6, reserve tank compartment 7, dustbin compartment 8, dustbin 9 fix a position and are fixed.
Further, the storage compartments 5 and 6, the reserve tank compartment 7 and the garbage bin compartment 8 are all provided with double right-angle knobs 14 for double locking.
Furthermore, a turnable opening cover 13 is arranged on the dustbin 8 door box to prevent peculiar smell from diffusing, and handles 15 are designed on the upper surface and the front surface of the dustbin 9.
Furthermore, the honeycomb plates of the frame 4 except the storage spaces 5 and 6 are all tied with interfaces.
Due to the adoption of the technical scheme, the invention has the following advantages:
1. the invention solves the problem that the airplane has no diet and drinking water heating device in long voyage.
2. The invention is effectively suitable for the working environment of special airplanes with low temperature, low air pressure and bumping vibration.
3. The invention has good heating and heat preservation performance for food and drinking water and high heat efficiency.
4. The invention has the protection functions of overheating, overcurrent and dry burning of the circuit.
5. The invention adopts the shielding cable and the conductive oxidation treatment, thereby effectively shielding the electromagnetic radiation generated by equipment and interfering the airborne equipment.
6. The invention has the function of garbage storage.
7. The invention has the function of storing the standby water.
8. The invention has the function of storing articles.
Drawings
FIG. 1 is a schematic diagram of the overall structure of an on-board diet heating assembly;
FIG. 2 is a typical cross-section of a heating assembly frame;
FIG. 3 is a schematic view of a right angle knob of a stopper of an on-board diet heating assembly;
FIG. 4 is a schematic view of the socket and louvers of the on-board diet heating assembly;
FIG. 5 is a schematic view of a heated water tank front sump box of an on-board food heating assembly;
FIG. 6 is a schematic view of the trash bin spacing of the on-board diet heating assembly;
figure 7 is a schematic view of a waste bin of an on-board diet heating assembly.
In the drawings are labeled:
1. a control panel; 2. an airborne heating cabinet; 3. an onboard heating water tank; 4. a frame; 5. a large storage compartment; 6. a small storage compartment; 7. a spare water tank compartment; 8. a dustbin compartment; 9. a dustbin; 10. heat dissipation holes; 11. an electrical outlet; 12. a water accumulation box; 13. a flap can be turned over; 14. a right-angle knob; 15. the dustbin handle.
Detailed Description
The following description is made with reference to the drawings and examples.
Referring to fig. 1, the onboard diet heating assembly of the present embodiment is composed of a frame 4, a control panel 1, an onboard heating tank 2, an onboard heating water tank 3, a large storage compartment 5, a small storage compartment 6, a spare water tank compartment 7, a garbage bin compartment 8, and a garbage bin 9.
The heating component frame 4 is a cuboid with an open front face formed by honeycomb plates, and the internal space of the heating component frame is divided into an upper part, a middle part and a lower part;
the upper part is provided with a control panel 1 which comprises a control component of an onboard heating box 2 and a control component of an onboard heating water tank 3;
the middle part of the heating box is provided with an airborne heating box 2 and an airborne heating water tank 3, wherein the airborne heating box 2 is electrically connected with an airborne heating box control assembly and is positioned below the airborne heating control assembly, and the airborne heating water tank 3 is electrically connected with an airborne heating water tank control assembly and is positioned below the airborne heating water tank control assembly;
the lower part sets up big storing compartment 5, little storing compartment 6, reserve tank compartment 7, dustbin compartment 8, and wherein, big storing compartment 5 sets up 2 below on-board heating box, and little storing compartment 6 sets up in on-board heating water tank 3 below, and reserve tank compartment 7 and dustbin compartment 8 set up in little storing compartment below side by side, and dustbin 9 places in dustbin compartment 8.
As shown in fig. 2, the frame 4 of the heating assembly is fixed by the honeycomb plate and the section parts through screwing and gluing.
As shown in fig. 4, an electrical socket 11 for supplying power to the onboard heating tank 2 and the onboard heating tank and a heat radiation hole 10 for radiating heat are provided on the back surface of the heating unit.
As shown in fig. 5, the length of the onboard heating water tank 3 is smaller than that of the frame, so that the water collecting box 12 is arranged at the position of a difference space between the water outlet of the onboard heating water tank 3 and the front surface of the frame.
As shown in fig. 3, the frame 4 is provided with a plurality of stopper right-angle knobs 14 for positioning and fixing the control panel 1, the onboard heating box 2, the onboard heating water box 3, the water accumulation box 12, the storage compartment 5, the storage compartment 6, the reserve tank compartment 7, the dustbin compartment 8 and the dustbin 9. Wherein, the storage compartment 5, the storage compartment 6, the spare water tank compartment 7 and the garbage bin compartment 8 are all provided with double right-angle knobs 14 for double locking.
As shown in figures 6 and 7, the dustbin compartment 8 is provided with a turnover cover 13 on the dustbin to prevent odor from diffusing, and the dustbin 9 is provided with a handle 15 on the upper surface and the front surface.
In addition, the honeycomb plates of the frame 4 except the storage compartment 5 and the storage compartment 6 are provided with mooring interfaces.
When the component is used, the main power button of the device is pressed on the control panel to switch on the power supply, and the heating box and the heating water tank power button are pressed in sequence to switch on the heating box and the heating water tank power supply.
The food is put into the onboard heating box, the cabinet door is closed, and heating is started. When the preset heating time and temperature are reached, the heating box keeps cyclic heating, and the heat is prevented from flowing outwards through the heat-insulating layer, so that the temperature of the food is kept within a specified range. When the food is eaten, the stop button is pressed to stop heating, then the power button of the heating box is turned off, and the heating box is powered off.
The power supply of the heating water tank is connected, the electric control system works, the water temperature in the inner container is continuously increased, when the water temperature reaches the set temperature of the control system, the electric control system cuts off the current to stop heating, and when the water temperature is lower than the set temperature, the electric control system is connected with the current to start heating; keeping the water temperature within a certain range.
The heating cabinet has the overheat prevention function, a temperature controller and a temperature relay are designed in the heating cabinet, the temperature inside the heating cabinet is monitored simultaneously, the temperature inside the heating cabinet is controlled by the temperature controller when the equipment works normally, and when the temperature controller fails, the direct current power supply of a system is directly cut off by the temperature relay within a certain temperature range.
The heating water tank has the function of preventing overheating, and the design of its inner bag bottom has the temperature relay of two different temperature points, and equipment normal during operation relies on the temperature relay control heating state that the temperature point is low, when this temperature relay accident goes wrong, if the temperature reachs another temperature relay's accuse temperature point, this temperature relay opens work, can effectual control heating temperature.
The electric control system in the heating water tank is also provided with an anti-dry heating protection circuit, and when the water level in the heating water tank is continuously lower than the set water level of the liquid level monitoring system, the anti-dry heating module can automatically cut off the power supply, so that the equipment dry heating is prevented from influencing the system safety.
The circuit breakers are arranged in the direct current circuit and the alternating current circuit in the electric control system, strong current is controlled according to weak current, and a three-phase alternating current power supply is switched on and off by power devices such as a direct current control relay when the current is overloaded, so that equipment fault diffusion caused by the current overload is prevented.
The electric control system adopts the shielding cable and adopts the conductive oxidation treatment, so that the electromagnetic radiation generated during the electric work can be shielded, the electromagnetic radiation is prevented from leaking to influence and interfere the normal function of the electric instrument of the special airplane, and the flight safety of the airplane is ensured.
The above is only a preferred embodiment of the present invention, and it should be noted that the above preferred embodiment should not be considered as limiting the present invention, and the protection scope of the present invention should be subject to the scope defined by the claims. It will be apparent to those skilled in the art that various modifications and adaptations can be made without departing from the spirit and scope of the invention, and these modifications and adaptations should be considered within the scope of the invention.
Claims (8)
1. The utility model provides an airborne diet heating element comprises frame (4), control panel (1), airborne heating tank (2), airborne heating tank (3), storing compartment (5, 6), reserve tank compartment (7), dustbin compartment (8), dustbin (9), its characterized in that:
the heating component frame (4) is a cuboid with an open front face formed by honeycomb plates, and the internal space of the heating component frame is divided into an upper part, a middle part and a lower part;
the upper part is provided with a control panel (1) which comprises a control component of an onboard heating box (2) and a control component of the onboard heating water tank (3);
an airborne heating box (2) and an airborne heating water tank (3) are arranged in the middle, wherein the airborne heating box (2) is electrically connected with the airborne heating box control component and is positioned below the airborne heating control component, and the airborne heating water tank (3) is electrically connected with the airborne heating water tank control component and is positioned below the airborne heating water tank control component;
the lower part sets up storing compartment (5, 6), reserve tank compartment (7), dustbin compartment (8), storing compartment (5, 6) are including big storing compartment (5) and little storing compartment (6), wherein, big storing compartment (5) set up airborne heating box (2) below, little storing compartment (6) set up airborne heating water tank (3) below, reserve tank compartment (7) with dustbin compartment (8) set up side by side little storing compartment (6) below, dustbin (9) place in dustbin compartment (8).
2. An on-board assembly as claimed in claim 1, characterised in that the frame (4) is fixed to the profiled element by means of a honeycomb plate screwed and glued.
3. An on-board heating assembly according to claim 2, characterized in that it is provided with electrical sockets (11) and heat-dissipating vents (10) on the back for powering the on-board heating tank (2) and the on-board heating water tank (3).
4. An on-board heating assembly according to claim 2, characterized in that the length of the on-board heating reservoir (3) is smaller than the length of the frame, so that the outlet of the on-board heating reservoir (3) is spaced from the front of the frame by the drip box (12).
5. An on-board heating assembly according to any of claims 1-4, characterized in that the frame (4) is provided with a stopper right-angle knob (14) for positioning and fixing the control panel (1), the on-board heating tank (2), the on-board heating tank (3), the water-collecting box (12), the storage compartments (5, 6), the reserve tank compartment (7), the waste bin compartment (8), and the waste bin (9).
6. An on-board heating assembly according to claim 5, characterized in that the stowage compartment (5, 6), the reserve tank compartment (7) and the waste bin compartment (8) are provided with double right-angle knobs (14) for double locking.
7. An on-board heating assembly according to claim 6, characterized in that the door of the waste bin compartment (8) is provided with a flap (13) which can be turned to prevent the spread of bad smells, and that the upper and front sides of the waste bin (9) are provided with a handle (15).
8. An on-board heating assembly according to claim 7, characterized in that the frame (4) is provided with a captive interface on the honeycomb panel except for the storage compartment (5, 6) portion.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201911270968.5A CN111186581A (en) | 2019-12-11 | 2019-12-11 | Airborne food heating assembly |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201911270968.5A CN111186581A (en) | 2019-12-11 | 2019-12-11 | Airborne food heating assembly |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN111186581A true CN111186581A (en) | 2020-05-22 |
Family
ID=70703299
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201911270968.5A Withdrawn CN111186581A (en) | 2019-12-11 | 2019-12-11 | Airborne food heating assembly |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN111186581A (en) |
Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20030042361A1 (en) * | 2001-09-05 | 2003-03-06 | George Simadiris | Liquid galley refrigeration system for aircraft |
| CN103842250A (en) * | 2011-08-30 | 2014-06-04 | B/E航空公司 | Reconfigurable chilled air outlet for an aircraft galley chiller |
| WO2018077466A1 (en) * | 2016-10-25 | 2018-05-03 | Uwe Dieter Weigele | Temperature-control system and oven for controlling the temperature of meals in a vehicle, frame for receiving meal containers and method for controlling the temperature of meals in a vehicle |
| CN109334993A (en) * | 2018-11-22 | 2019-02-15 | 西安飞豹科技有限公司 | A kind of integrated airplane cabinet equipment |
| CN110015429A (en) * | 2018-01-08 | 2019-07-16 | 空中客车运营有限公司 | The kitchen warehouse structure with electrical lock mode for aircraft or spacecraft |
-
2019
- 2019-12-11 CN CN201911270968.5A patent/CN111186581A/en not_active Withdrawn
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20030042361A1 (en) * | 2001-09-05 | 2003-03-06 | George Simadiris | Liquid galley refrigeration system for aircraft |
| CN103842250A (en) * | 2011-08-30 | 2014-06-04 | B/E航空公司 | Reconfigurable chilled air outlet for an aircraft galley chiller |
| WO2018077466A1 (en) * | 2016-10-25 | 2018-05-03 | Uwe Dieter Weigele | Temperature-control system and oven for controlling the temperature of meals in a vehicle, frame for receiving meal containers and method for controlling the temperature of meals in a vehicle |
| CN110015429A (en) * | 2018-01-08 | 2019-07-16 | 空中客车运营有限公司 | The kitchen warehouse structure with electrical lock mode for aircraft or spacecraft |
| CN109334993A (en) * | 2018-11-22 | 2019-02-15 | 西安飞豹科技有限公司 | A kind of integrated airplane cabinet equipment |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| WW01 | Invention patent application withdrawn after publication | ||
| WW01 | Invention patent application withdrawn after publication |
Application publication date: 20200522 |