CN209870712U - Aircraft passenger plane - Google Patents
Aircraft passenger plane Download PDFInfo
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- CN209870712U CN209870712U CN201821964226.3U CN201821964226U CN209870712U CN 209870712 U CN209870712 U CN 209870712U CN 201821964226 U CN201821964226 U CN 201821964226U CN 209870712 U CN209870712 U CN 209870712U
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Abstract
The utility model discloses an airliner, including flexible thin-film solar energy component, organism and battery, flexible thin-film solar energy component fixes the surface of organism is the electric energy with light energy conversion, and stores in the battery, with right consumer in the organism supplies power. The embodiment of the utility model provides an aviation passenger plane is through fixing flexible thin-film solar energy component at the surface of organism, on the one hand make full use of the idle region of organism, converts light energy into electric energy to improve the duration of a journey of passenger plane, and energy-concerving and environment-protective; on the other hand, when the passenger plane flies at high altitude, the solar radiation effect is better, the power generation efficiency of the flexible thin-film solar module can be further improved, and the electric power support is provided for the passenger plane.
Description
Technical Field
The utility model relates to a flight equipment technical field especially indicates an aviation passenger plane.
Background
At present, solar energy is already applied to the field of aerospace, such as unmanned planes, solar satellites and the like, but the solar energy is not applied to common passenger planes which are occupied by the people.
On 23.7.7.1983, canadian aviation # 143 airliner (boeing 767 aircraft) turned off the engine at high altitudes due to insufficient fuel, and the aircraft ram air turbine was automatically started to provide power to the aircraft systems. The airplane can be controlled only by the electric power, namely the airplane successfully lands after gliding for 17 minutes. Therefore, the electric power plays a great role in ensuring the safety of the airplane.
SUMMERY OF THE UTILITY MODEL
In view of this, the present invention provides an aircraft to improve the endurance of the aircraft.
The embodiment of the utility model provides an aviation passenger plane, including flexible thin-film solar energy component, organism and battery, flexible thin-film solar energy component fixes the surface of organism is the electric energy with light energy conversion, and stores in the battery, with right consumer in the organism supplies power.
In some embodiments of the present invention, the body includes a body, the body includes an upper body and a lower body, and the flexible thin film solar module is fixed on the surface of the upper body.
In some embodiments of the present invention, the body further includes a left wing and a right wing respectively connected to two sides of the body, and the flexible thin film solar module is fixed to the upper surface of the left wing and the upper surface of the right wing.
In some embodiments of the present invention, the body further includes an empennage respectively connected to the tail of the body, and the flexible thin film solar module is fixed to the light receiving surface of the empennage.
In some embodiments of the present invention, the flexible thin film solar module is fixed on the surface of the body by means of adhesion.
In some embodiments of the present invention, the flexible thin film solar module is a copper indium gallium selenide thin film solar module.
The embodiment of the utility model provides an aviation passenger plane is through fixing flexible thin-film solar energy component at the surface of organism, on the one hand make full use of the idle region of organism, converts light energy into electric energy to improve the duration of a journey of passenger plane, and energy-concerving and environment-protective; on the other hand, when the passenger plane flies at high altitude, the solar radiation effect is better, the power generation efficiency of the flexible thin-film solar module can be further improved, and the electric power support is provided for the passenger plane. The utility model discloses fix flexible thin-film solar energy component on the surface of aviation passenger plane, rather than traditional crystal silicon battery for still can normally generate electricity under low temperature environment and low light environment, even the passenger plane sails at night, also can provide electric power and support.
Drawings
In order to more clearly illustrate the embodiments of the present invention or the technical solutions in the prior art, the drawings used in the description of the embodiments or the prior art will be briefly described below, it is obvious that the drawings in the following description are only some embodiments of the present invention, and for those skilled in the art, other drawings can be obtained according to these drawings without creative efforts.
Fig. 1 is a front view of an aircraft according to an embodiment of the invention;
fig. 2 is a side view of an aircraft according to an embodiment of the invention.
Detailed Description
In order to make the technical solution of the present invention better understood, the technical solution of the embodiments of the present invention will be clearly and completely described below with reference to the accompanying drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only some embodiments of the present invention, not all embodiments. Based on the embodiments in the present invention, all other embodiments obtained by a person skilled in the art without creative efforts shall belong to the protection scope of the present invention.
It should be noted that the terms "first," "second," and the like in the description and claims of the present invention and in the drawings described above are used for distinguishing between similar elements and not necessarily for describing a particular sequential or chronological order. It is to be understood that the data so used is interchangeable under appropriate circumstances such that the embodiments of the invention described herein are capable of operation in sequences other than those illustrated or otherwise described herein. Furthermore, the terms "comprises," "comprising," and "having," and any variations thereof, are intended to cover a non-exclusive inclusion, such that a process, method, system, article, or apparatus that comprises a list of steps or elements is not necessarily limited to those steps or elements expressly listed, but may include other steps or elements not expressly listed or inherent to such process, method, article, or apparatus.
An embodiment of the utility model provides an airliner, airliner includes flexible thin-film solar module, organism and battery, flexible thin-film solar module fixes the surface of organism converts light energy into the electric energy, and stores in the battery, with right consumer in the organism supplies power. The aircraft is generally bigger in size, and the surface body has large tracts of land idle area, and when the aircraft was flying in addition, the weakening of atmosphere to solar radiation and scattering all are less than ground, so install flexible thin-film solar energy component and can obtain better power generation effect on the aircraft, supply continuation of journey for the inside electricity consumption of aircraft, electric power storage. Therefore, the utility model discloses be applied to large-scale aviation passenger plane organism surface with flexible thin-film solar energy component, provide electric power support for the passenger plane to energy-concerving and environment-protective.
It should be noted that the fixed position of the flexible thin film solar module can select the regions of the wings, the upper part of the airframe and the like without mechanical change, so that the free region of the passenger plane can be fully utilized, and the normal operation of the passenger plane can not be influenced.
The schematic structural diagram of the aircraft is shown in fig. 1-2, the airframe comprises an airframe, the airframe comprises an upper half airframe 200 and a lower half airframe 100, and the flexible thin film solar module is fixed on the surface of the upper half airframe 200. Therefore, the flexible thin film solar module is fixed on the largest part of the machine body, namely the surface of the machine body, so that the free area on the surface of the machine body can be utilized as much as possible, and more light energy can be converted into electric energy.
Optionally, as shown in fig. 1-2, the airframe further includes a left wing 500 and a right wing 600 respectively connected to two sides of the airframe, and the flexible thin-film solar module is fixed on the upper surface of the left wing 500 and the upper surface of the right wing 600. In addition to the fuselage, the left wing 500 and the right wing 600 connected to the fuselage are also free areas that can be fully utilized, so that flexible thin-film solar modules are continuously fixed on the upper surfaces of the left wing 500 and the right wing 600 to convert more light energy into electric energy.
Optionally, as shown in fig. 1-2, the main body further includes tail fins 300 respectively connected to the tail portions of the main body, and the flexible thin film solar modules are fixed on the light receiving surfaces of the tail fins 300. In addition to the fuselage, the left wing 500 and the right wing 600, the tail wing 300 connected to the tail of the fuselage is a free area that can be fully utilized, so that a flexible thin film solar module can be fixed on the light receiving surface of the tail wing 300 to convert more light energy into electric energy.
As shown in fig. 1-2, the fuselage is further provided with a door 800, a power device 400, a landing gear 700, etc., which are not described in detail. If necessary, the flexible thin film solar module may be fixed at these positions, which is not limited by the present invention.
Optionally, the flexible thin-film solar module is fixed on the surface of the machine body in a sticking mode, and the installation mode is very simple. The flexible thin-film solar module can be customized according to different sizes so as to meet the requirements of different models. The flexible thin-film solar modules have different lengths, such as 2 meters, 4 meters, 6 meters and the like, and can be pasted with modules of different sizes according to different sizes and positions of the machine body, so that the effective area is fully utilized for power generation. Because the flexible thin-film solar module is flexible, the flexible thin-film solar module can be fixed on the surface of the aircraft body in a direct pasting mode and then is connected into a storage battery through a circuit, and power generation is accumulated during flight, especially the demand on power is higher like transnational long-distance flight and night flight, so that an additional convenient and environment-friendly power generation mode is arranged, and the cruising ability of the aircraft is favorably improved. In addition, the storage battery can provide electric power support for the infrastructure in the airframe, and can be connected to a backup generator or a turbine to provide backup electric power support for the passenger plane, thereby providing safety guarantee. The flexible thin-film solar module has the characteristic of being bendable, gets rid of the constraint of the traditional crystalline silicon solar cell, can adapt to the surface of an airplane shell with radian or a narrow space, and has strong adaptability.
In another embodiment of the present invention, the flexible thin film solar module is a copper indium gallium selenide thin film solar module. The CIGS thin-film solar module has the advantage of weak light power generation which is different from other solar modules. At clear nights, electricity can also be generated through moonlight, in other words, during the night flight of the passenger plane, additional power support can still be obtained, which is an effect that other products cannot achieve. Therefore, the plane can still obtain electric power support when flying at night due to weak light power generation of the CIGS thin-film solar module, so that the CIGS thin-film solar module is fixed on the surface of the plane body, and the endurance of an aviation passenger plane is improved.
In the flying process of the passenger plane, the stable flying height reaches 8000-10000 m, the air temperature can be reduced by 0.6 ℃ according to the physical law that the air temperature is reduced by 100 m per rise of altitude, on the basis of the normal ground surface temperature, the air temperature of the passenger plane in the flying process can reach below-30 ℃, the traditional crystalline silicon solar cell cannot work normally and stably, and the copper indium gallium selenide thin-film solar module can work normally in the temperature range of-45-80 ℃, so that the problem of temperature reduction in the air can be solved. And the service life of the CIGS thin-film solar module is as long as 25 years, and the CIGS thin-film solar module is durable. In addition, the outer surface of the CIGS thin-film solar module is provided with a 3M water-blocking film to resist cloud layers and water vapor in the air.
The CIGS thin-film solar module has the advantages of light weight and small thickness, the weight of a crystalline silicon solar panel in each square meter is more than 12kg, and the weight of the flexible thin-film solar module is only one fourth of that of a crystalline silicon cell, which is incomparable with the traditional crystalline silicon solar panel. Therefore, the CIGS thin-film solar module is fixed on the surface of the airframe, which does not cause excessive burden on the airframe of the passenger plane.
Therefore, the embodiment of the utility model provides an aviation passenger plane is through fixing flexible thin-film solar energy component at the surface of organism, on the one hand make full use of the idle region of organism, converts light energy into electric energy to improve the duration of the passenger plane, and energy-concerving and environment-protective; on the other hand, when the passenger plane flies at high altitude, the solar radiation effect is better, the power generation efficiency of the flexible thin-film solar module can be further improved, and the electric power support is provided for the passenger plane. The utility model discloses fix flexible thin-film solar energy component on the surface of aviation passenger plane, rather than traditional crystal silicon battery for still can normally generate electricity under low temperature environment and low light environment, even the passenger plane sails at night, also can provide electric power and support.
Those of ordinary skill in the art will understand that: the discussion of any embodiment above is meant to be exemplary only, and is not intended to intimate that the scope of the disclosure, including the claims, is limited to these examples; within the idea of the invention, also combinations between technical features in the above embodiments or in different embodiments are possible, and there are many other variations of the different aspects of the invention as described above, which are not provided in detail for the sake of brevity. Therefore, any omission, modification, equivalent replacement, or improvement made within the spirit and principle of the present invention should be included within the protection scope of the present invention.
Claims (6)
1. An airliner is characterized by comprising a flexible thin film solar module, a machine body and a storage battery, wherein the flexible thin film solar module is fixed on the surface of the machine body, converts light energy into electric energy and stores the electric energy in the storage battery so as to supply power to electric equipment in the machine body.
2. An aircraft according to claim 1, characterized in that the fuselage comprises a fuselage comprising an upper half-fuselage (200) and a lower half-fuselage (100), the flexible thin-film solar module being fixed to the surface of the upper half-fuselage (200).
3. An airliner as in claim 2, wherein said body further comprises a left wing (500) and a right wing (600) respectively associated with each side of said fuselage, said flexible thin-film solar modules being fixed to the upper surface of said left wing (500) and to the upper surface of said right wing (600).
4. An aircraft according to claim 2, wherein the body further comprises empennages (300) respectively associated with the tail portions of the fuselage, the flexible thin-film solar module being secured to a light-receiving surface of the empennages (300).
5. The aircraft of claim 1, wherein the flexible thin film solar module is adhesively secured to the surface of the airframe.
6. An airliner as defined in claim 1 wherein said flexible thin film solar module is a copper indium gallium selenide thin film solar module.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201821964226.3U CN209870712U (en) | 2018-11-27 | 2018-11-27 | Aircraft passenger plane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201821964226.3U CN209870712U (en) | 2018-11-27 | 2018-11-27 | Aircraft passenger plane |
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| Publication Number | Publication Date |
|---|---|
| CN209870712U true CN209870712U (en) | 2019-12-31 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201821964226.3U Active CN209870712U (en) | 2018-11-27 | 2018-11-27 | Aircraft passenger plane |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112793795A (en) * | 2021-03-19 | 2021-05-14 | 靳晨昊 | Carry on new forms of energy system's unmanned aerial vehicle |
-
2018
- 2018-11-27 CN CN201821964226.3U patent/CN209870712U/en active Active
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112793795A (en) * | 2021-03-19 | 2021-05-14 | 靳晨昊 | Carry on new forms of energy system's unmanned aerial vehicle |
| CN112793795B (en) * | 2021-03-19 | 2022-03-29 | 靳晨昊 | Carry on new forms of energy system's unmanned aerial vehicle |
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Address after: 3001, room 6, building No. 7, Rongchang East Street, Beijing economic and Technological Development Zone, Beijing, Daxing District 100176, China Patentee after: Beijing Dingrong Photovoltaic Technology Co.,Ltd. Address before: 3001, room 6, building No. 7, Rongchang East Street, Beijing economic and Technological Development Zone, Beijing, Daxing District 100176, China Patentee before: BEIJING APOLLO DING RONG SOLAR TECHNOLOGY Co.,Ltd. |
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Effective date of registration: 20210427 Address after: 201, room 518057, building A, No. 1, front Bay Road, Qianhai, Shenzhen Guangdong cooperation zone (Shenzhen Qianhai business secretary Co., Ltd.) Patentee after: Hongyi Technology Co.,Ltd. Address before: 3001, room 6, building No. 7, Rongchang East Street, Beijing economic and Technological Development Zone, Beijing, Daxing District 100176, China Patentee before: Beijing Dingrong Photovoltaic Technology Co.,Ltd. |