• 专利附录
  • 专利说明
  • 权利要求
  • 类似技术
  • 同族专利
  • 引用文献
  • 法律状态
  • 优先权
    • 专利摘要:
    System for measuring concentrated solar radiation and unmanned aerial vehicle that includes it. The system for measuring concentrated solar radiation comprising a reflective tubular structure comprising first coupling means for a drone, a first segment (14), a second segment (20) and a second coupling means between both segments (14, 20); a plurality of radiometers (12) installed longitudinally in the first segment; a data acquisition unit (18) for recording the measurements taken by the plurality of radiometers (12). The unmanned aerial vehicle (10) incorporates the system and allows measuring solar radiation at the center of the solar receiver (2). (Machine-translation by Google Translate, not legally binding)
    公开号:ES2726474A1
    申请号:ES201930606
    申请日:2019-07-01
    公开日:2019-10-04
    发明作者:Espinosa Rafael Monterreal
    申请人:Centro de Investigaciones Energeticas Medioambientales y Tecnologicas CIEMAT；
    IPC主号:
    专利说明:

    [0001]
    [0002] Technical Field of the Invention
    [0003] The invention belongs to the systems associated with the concentrating solar thermal power plants. In particular, it relates to techniques for measuring radiation in tower-type solar power plants.
    [0004]
    [0005] Background of the invention or State of the Art
    [0006] A tower-type solar power plant uses a collector tower to receive concentrated sunlight that is usually used to heat a working fluid with which to move turbines with which to generate electricity. Use a set of generally curved, focal length and mobile mirrors (called heliostats) to focus the sun's rays on a tower (the white one). Concentrated thermal solar energy is seen as a viable solution to generate renewable and pollution-free energy from a source.
    [0007] In experimental tower or central receiver solar plants (small power), there is evidence of concentrated solar radiation flow measurement systems through the use of electro-mechanical devices installed in the immediate vicinity of the solar receiver, and which involve the intervention of mobile mechanisms with radiometers and / or lambertian targets supported by video systems. These systems are complex with respect to their assembly, installation, control, protection, operation and maintenance. They are also quite expensive. In no case has it been possible to use them in large commercial tower production plants. Some of these devices are described in articles and publications:
    [0008] [1] Neumann A. and Monterreal, R. Advanced Flux Measurement System for Solar Tower Plants. 7th International Symposium on Solar Thermal Concentrating Technologies. Moscow, Russia September 26-30, 1994.
    [0009] [2] ES2249957B1 Patent: Radiant power measuring device for large surfaces.
    [0010] [3] Shiel, W. Hermes Measurements. SSPS Technical Report 4 (1983)
    [0011] [4] Durish, W. and Shelders, Ch. Radiation Input Measurements with the Flux Analyzing System FAS. IAE-SSPS Central Receiver System Midterm Workshop, April 1983. Tabernas, Spain.
    [0012] [5] Thalhammer, E.E. and Phipps, G.H. Scatterplate Flux Mapping for Solar Concentrators. Solar Energy Research Institute (SERI) TR-255-1432 (1982).
    [0013] [6] Becker, M; Bate, J. and Diessner, F. Device for the Measurements of Heat Flux Distribution (HFD) near the receiver aperture plane of the Almeria CRS Solar Power Station. DFVLR Interner Bericht (1981).
    [0014] [7] Brinner, A. and Shiel, W. Advanced Sodium Receiver (ASR) Performance with the HERMES Measuring System at the IEA SSPS Central Receiver System. Proc. Of 1986 Int. Congress on Renewable Energy Sources. Madrid.
    [0015] In solar plants of the tower type or central commercial receiver (high power), there is no record of the implementation of a high-flow measurement system of solar radiation to date. No patent document is known, nor is there any scientific publication referring to unmanned aerial vehicles used to measure the concentration of concentrated solar radiation in central solar receiver plants. The known background is restricted to the use of drones in solar installations for other uses, such as the detection of failures in the operation of photovoltaic solar panels or the repositioning of heliostats in central receiver plants.
    [0016] - GB2546564 discloses techniques to detect defects in solar panel assemblies. - CN106644399 discloses heliostatic correction techniques using a drone.
    [0017] - ES2604554 discloses a procedure for the measurement of heliostats.
    [0018] Other related documents are:
    [0019] - Lock, JC et al. “An Investigation Into Multi-Dimensional Prediction Models to Estimate the Pose Error of a Quadcopter in a CSP Plant Setting”. Solarpaces 2015: International Conference on Concentrating Solar Power and Chemical Energy Systems; Collection: AIP Conference Proceedings; Vol: 173, N °: 130012, 2016.
    [0020] - Prahl, C et al. "Airborne shape measurement of parabolic trough collector fields". Solar Energy, Vol .: 91, Page: 68-78, May 2013.
    [0021] - Matsuoka, R et al. “Measurement of large-scale solar power plant by using images acquired by non-metric digital camera on board UAV”. Magazine: XXII ISPRS Congress, Technical Commission I; Collection: International Archives of the Photogrammetry Remote Sensing and Spatial Information Sciences; Vol .: 39-B1, Page: 435-440, 2012.
    [0022] Brief Description of the Invention
    [0023] The measurement of concentrated solar radiation in tower solar plants (or solar receiver) presents great difficulties.
    [0024] This measure is of capital importance in the knowledge of the energy performance of the plant, since it quantifies the amount of solar fuel provided by the heliostats field to be finally transformed into electrical energy by the plant.
    [0025] The difficulties for the measurement are essentially three:
    [0026] a) the high concentration factor of solar energy that is contributed to the solar receiver by the heliostat field (of the order of megawatts / m2);
    [0027] b) the location of the receiver (in a tower between 100m-150m high); Y
    [0028] c) the large dimensions of the solar receiver itself (of the order of tens of m2). All this entails the difficulty, if not the impossibility, of the installation, passive protection due to collateral damage of the concentrated radiation (insulation, cooling, etc.), maintenance of measuring equipment, such as radiometers or moving targets, as well as mechanisms of drag and positioning, active refrigeration equipment, data acquisition, etc.
    [0029] The invention proposes a solution for these problems according to the system of claim 1. Specifically, a system for measuring concentrated solar radiation is incorporated which incorporates:
    [0030] - a longitudinal, generally tubular, reflective structure that includes first coupling means for coupling to an unmanned aerial vehicle, a first segment, a second segment and a second coupling means between said segments;
    [0031] - several radiometers installed longitudinally in the first segment that is furthest from the unmanned aerial vehicle;
    [0032] - The system includes a unit for collecting information produced by radiometers.
    [0033] This information collection unit can be implemented in one embodiment as a data acquisition unit to record the measurements taken by the radiometers. The electrical signals coming from the radiometers can be stored in the unmanned vehicle itself to be overturned later and to carry out the adequate data processing for the solar plant under study. Preferably, this temporary storage is performed in said data acquisition unit on board the unmanned aerial vehicle.
    [0034] Alternatively, there is another option. In a different embodiment, a signal repeater can be included, so that the electrical signals from the radiometers are not stored on board the unmanned vehicle, but are replicated and transmitted via wireless (eg Wi-Fi or similar) to a General data processing system of the solar plant.
    [0035] Optionally, a counterweight attached to the end of the second segment closest to the unmanned aerial vehicle in order to balance the center of gravity of the previous elements in the position where the first coupling means are located.
    [0036] Alternatively to the use of a counterweight in the longitudinal support structure, it is possible to use support structures light enough to reduce the moment of its own weight on the drone. Metal structures type lattice or other materials that provide lightness and rigidity, such as carbon fiber or similar, provided they have a suitable thermal coating that protects them from high concentrated solar radiation, are suitable for the purpose of the invention. Optionally, the data acquisition unit can implement wireless communication.
    [0037] Optionally, radiometers are distributed equidistant.
    [0038] The invention also proposes an unmanned aerial vehicle (commonly called a drone) that has a system installed as indicated in the previous lines to measure concentrated solar radiation.
    [0039]
    [0040] Brief description of the figures
    [0041] FIG. 1A is an overview of a central tower and a solar receiver in operation. FIG. 1B illustrates in greater detail the solar receiver.
    [0042] FIGs. 2A-2C shows several components for coupling in an embodiment of the invention. FIG. 2A shows the cross section of a first tubular segment. FIG. 2B illustrates disassembled two segments and the acquisition and storage unit. FIG. 2C is an example of the system with its components assembled.
    [0043] FIG. 3 illustrates a schematic mode of operation of the proposed invention.
    [0044] FIG. 4A is a scheme of taking measurements at the receiver to build a matrix whose elements are experimental data. FIG. 4B shows an example of 2D flow distribution. FIG. 4C shows an example of 3D flow distribution.
    [0045] 2 solar receiver.
    [0046] 4 Tower of a heliostat field.
    [0047] 10 Drone (unmanned aerial vehicle).
    [0048] 12 Radiometer.
    [0049] 14 First segment.
    [0050] 16 Vision camera.
    [0051] 18 Acquisition and storage unit.
    [0052] 20 Second segment.
    [0053] 22 Counterweight.
    [0054] 24 signal cable.
    [0055]
    [0056] Detailed description of the invention
    [0057] Various aspects of the invention are described with reference to the preceding figures according to an embodiment without limitation.
    [0058] FIG. 1A illustrates an example a tower 4 with a solar receiver 2 for a heliostat field. FIG. 1B illustrates in greater detail the upper part where it is installed in solar receiver 2 . Advantageously, the measuring instrument is not in the immediate vicinity of the solar receiver 2 , not even in tower 4 , which avoids the inconvenience of installation, passive protection of the equipment or interference with other genuine plant elements.
    [0059] FIGs. 2A-2C illustrate the assembly of the measuring instruments. The non-refrigerated rapid response radiation sensors (eg, radiometers 12 ) are installed in a longitudinal structure, preferably tubular, formed by a first segment 14 attached to a second segment 20 . Preferably, this tubular structure is made of polished stainless steel (with high reflectance) or any other coating that provides it with thermal resistance to radiation, so that it provides rigidity to the assembly and arranges it in an arrangement of specific dimensions, adapted to each type of solar receiver 2 . The number of radiometers 12 will be proportional to the extent of the surface to be measured, as well as the resolution required for it. This geometric arrangement of radiometers 12 is then coupled by means of signal cables 24 to an acquisition and storage unit 18 of the data generated by the radiometers 12 . The acquisition and storage unit 18 is transported by an unmanned aerial vehicle or drone 10 , which has a vision camera 16 , GPS navigator, as well as programmable positioning coordinates and closed loop position control system. The mode of operation comprises three phases:
    [0060] a) Drone 10 takes off from its base and will raise the concentrated solar radiation measurement system to the altitude level of the center of the receiver 2 , although still outside the area of influence of the radiation provided by tower 4 of the heliostat field (cold zone), where the measurement order from the central control of the plant is waiting;
    [0061] b) Once the measurement order is activated, the drone 10 - which will not enter the irradiated zone at any time - will introduce the measurement system in the irradiated zone, by means of a programmed, sequential or unique movement, depending on the strategy chosen for each case. The irradiated zone includes, not only where the solar receiver itself is, but also its near periphery (variable, but typically between 2-5 meters). Specifically, it encompasses passive elements of the tower or surrounding atmosphere) that are affected by spillage energy generally due to optical errors and / or inaccuracy at the heliostat field point.
    [0062] In any case, the irradiated area could be bounded - due to the overflow of the incident radiation - in a circle centered on the receiver and radius «2R, where R is the radius of the solar receiver. In rectangular receivers of dimensions ab, the equivalent radius that limits the irradiated area would be worth: R « 2 ^ ( ab / 2n)
    [0063] The response of the radiometers 12 is so rapid, that it allows a time of exposure of the measuring system to concentrated solar radiation short enough to avoid damage and not need a coupled cooling system; Y
    [0064] c) once the measurement is completed, the data is transmitted wirelessly ( eg WiFi) to the central control of the plant, and the drone 10 will return to its base, cooling the set of instruments naturally as it passes through the cold atmosphere.
    [0065] There is thus a system of measurement of solar radiation concentrated in completely autonomous tower solar plants, detached from the solar plant infrastructure to perform the measurement, without the need for installation of passive protection elements and without cooling. Its autonomy implies that, since it is not linked to the infrastructure of a certain plant, it can in fact measure in any solar tower plant, by simply adapting the arrangement of its radiometers 12 and the sequence of movement to the requirements of the new requirements. In addition, its price is estimated to be lower than that of conventional systems.
    [0066] For a better understanding, the applicability of the invention to the measurement of concentrated solar radiation in the TSA solar receiver is complemented with an example. This receiver is currently located at level 86m of the CESA-1 tower, in the Solar Platform of Almeria, Spain according to FIG. 1. It is a circular volumetric solar receiver 2 , 3.4m in diameter, and supports an incident power of 3000 kW and a maximum flow density of 800 kW / m2. Solar fuel comes from the CESA-1 heliostat field. The concentrated solar radiation measurement system includes the following elements:
    [0067] I) A set of radiometers 12 as fast response sensors, non-refrigerated and small in size, provided with signal cable (FIG. 2A).
    [0068] II) A first segment 14 or tube preferably made of stainless steel or any other material resistant to solar irradiance, which: a) serves as a fastener to the radiometers and b) protects and conducts the signal cables to a data acquisition unit 18 or data logger (FIG. 2B).
    [0069] III) A second segment 20 or stainless steel pole (FIG. 2B) that can be coupled (for example by threading) to the first segment 14 of section ii) and that is calibrated in length and weighted by a counterweight 22 if necessary at its end contrary.
    [0070]
    [0071] Iv) An unmanned aerial vehicle or drone 10 coupled to the second segment 20 described in section iii), equipped with the power and control capable of elevating - once coupled the elements described in the previous sections - to the height of the tower where find the receiver (FIG. 2C) and descend to its base following a programmed sequence of positions.
    [0072] The proposed concentrated solar radiation measurement system, which is the subject of the invention, follows the following operating procedure:
    [0073]
    [0074] v) The assembled assembly (shown in FIG. 2C) takes off from its base and approaches the level of the solar receiver 2 always confined in the so-called “cold zone” of the plant, that is, in no case area irradiated by radiation concentrated solar from the solar field (see FIGs. 3 and 4A).
    [0075]
    [0076] v I) Once the height of the receiver base is reached, the drone executes a lateral movement and introduces, using the second segment 20 , the arrangement of radiometers 12 in the predicted irradiated area, without exposing it to concentrated radiation. Then, it performs an ascension movement to sweep the entire area of the solar receiver 2 , all in the shortest possible time. All signals from radiometers 12 are stored in the acquisition and storage unit 18 . Once the upper level of the solar receiver 2 is reached, the drone 10 returns to the base, always within the cold zone.
    [0077] The data recorded in the acquisition and storage unit unit 18 is sent via WiFi (or any other wireless procedure) to the central control, where the data corresponding to the generated nxm point map (see FIG. 4A), is they can represent as elements I¡j, [kW / m2] of a flow matrix I are processed to provide characteristics such as the amount of incident power, its shape, distribution, singular points, etc., both in 2D, as seen in FIG. 4B, as in 3D, as illustrated in FIG. 4C.
    权利要求:
    Claims (8)
    [1]
    1. System for measuring concentrated solar radiation characterized in that it comprises: - a longitudinal reflective structure comprising
    a first segment (14),
    a second segment (20),
    first coupling means of the second segment (20) with an unmanned aerial vehicle (10), and
    second coupling means between both segments (14,20);
    - a plurality of radiometers (12) installed longitudinally in the first segment (14);
    - a unit for collecting information produced by the plurality of radiometers (12).
    [2]
    2. System according to claim 1, further comprising a counterweight (22) attached to the free end of the second segment (20) to balance the center of gravity of the previous elements in the position where the first coupling means are located.
    [3]
    3. System according to claim 1 or 2, wherein the information collection unit produced by the plurality of radiometers (12) is a data acquisition unit (18) for recording the measurements taken by the plurality of radiometers (12) .
    [4]
    4. System according to any one of the preceding claims, wherein the data acquisition unit (18) implements wireless communication.
    [5]
    5. System according to claim 1 or 2, wherein the information collection unit is a repeater configured to wirelessly replicate and transmit electrical signals from radiometers (12).
    [6]
    6. System according to any one of the preceding claims, wherein the radiometers (12) are distributed equidistant.
    [7]
    7. Unmanned aerial vehicle (10) comprising the system for measuring concentrated solar radiation according to any one of claims 1 to 6.
    [8]
    8. Unmanned aerial vehicle (10) according to claim 7 which is programmed to:
    - raise and position the system for measuring concentrated solar radiation to the altitude level of the center of the solar receiver (2), keeping said system separate at least a predetermined distance from the solar receiver (2);
    - introducing the first segment (14) of the tubular structure in a region irradiated by the heliostat field (4) and measuring with the plurality of radiometers (12);
    - wirelessly transmit the measurement data performed by the plurality of radiometers (12).
    类似技术:
    公开号 | 公开日 | 专利标题
    CN103229000B|2016-07-06|The concentration solar generating in greenhouse
    US20140366929A1|2014-12-18|System and method for solar energy utilization
    CN101462599B|2011-04-27|Novel terrestrial globe simulator for static state infrared horizon ground detection
    CN103959035A|2014-07-30|Method and system for positioning apparatus for monitoring parabolic reflector aerially
    ES2878098T3|2021-11-18|System and method for thermomechanical monitoring of a solar receiver
    CN102588892A|2012-07-18|Optical system of solar simulator
    US20140174503A1|2014-06-26|Energy convertor/concentrator system
    ES2726474B2|2020-02-10|SYSTEM FOR MEASURING CONCENTRATED SOLAR RADIATION AND UNTRIPULATED AIR VEHICLE UNDERSTANDING
    ES2715612T3|2019-06-05|Element of capture and concentration of direct solar radiation
    ES2579208B1|2017-05-22|INCIDENT RADIATION DETECTION SYSTEM AND METHOD ON A SOLAR RECEIVER
    CN106291513A|2017-01-04|Laser satellite reflector array thermal vacuum test system and method
    ES2472449T3|2014-07-01|Support device for a solar generator unit
    Zech et al.2013|SST-GATE: A dual mirror telescope for the Cherenkov Telescope Array
    Röger et al.2017|New methods and instruments for performance and durability assessment
    CN106872030B|2018-07-06|Visible-short-wave infrared ultraphotic spectrum irradiance instrument available for long-term automatic Observation
    CN202975364U|2013-06-05|Atmospheric optical parameter measuring instrument for Antarctic plateau astronomical site selection
    Faiman et al.2002|PETAL: a research pathway to fossil-competitive solar electricity
    ES2422806B1|2014-09-17|SYSTEM, PROCEDURE AND COMPUTER PROGRAM OF CALIBRATION OF THE POSITIONING OF MIRRORS IN HELIOSTATS
    Jägers et al.2008|Fast foldable tent domes
    CN108153336A|2018-06-12|The device and method for tracking sun altitude
    Burton et al.2015|Astronomy from the high Antarctic plateau
    Shortis et al.2008|Photogrammetric analysis of solar collectors
    ES1074545U|2011-05-11|Armor for multiple heliostatos or photovoltaic panels with independent adjustment and automatic arrastre |
    Khosroshahi2011|Site characterization studies for the Iranian National Observatory
    Zhang et al.2015|China radiometric calibration sites ground-based automatic observing systems for CAL/VAL
    同族专利:
    公开号 | 公开日
    ES2726474B2|2020-02-10|
    引用文献:
    公开号 | 申请日 | 公开日 | 申请人 | 专利标题
    US5861947A|1997-02-25|1999-01-19|Deutshes Zentrum fur Luft-und Raumfahrt e.V.|Measuring device for measuring concentrated radiation of light|
    WO2015117192A1|2014-02-06|2015-08-13|Commonwealth Scientific And Industrial Research Organisation|Monitoring and measuring of multiple light sources especially heliostats|
    US20180003656A1|2016-06-30|2018-01-04|Unmanned Innovation Inc.|Solar panel inspection using unmanned aerial vehicles|
    CN208079019U|2018-04-16|2018-11-09|哈尔滨哈程电气科技发展有限公司|A kind of photovoltaic plant inspection device based on unmanned plane remote control and regulation|
    KR101977304B1|2018-07-17|2019-05-10|주식회사 다인에스엔티|Solar Panel Maintenance Drone and Maintenance Method Using the Same|
    法律状态:
    2019-10-04| BA2A| Patent application published|Ref document number: 2726474 Country of ref document: ES Kind code of ref document: A1 Effective date: 20191004 |
    2020-02-10| FG2A| Definitive protection|Ref document number: 2726474 Country of ref document: ES Kind code of ref document: B2 Effective date: 20200210 |
    优先权:
    申请号 | 申请日 | 专利标题
    ES201930606A|ES2726474B2|2019-07-01|2019-07-01|SYSTEM FOR MEASURING CONCENTRATED SOLAR RADIATION AND UNTRIPULATED AIR VEHICLE UNDERSTANDING|ES201930606A| ES2726474B2|2019-07-01|2019-07-01|SYSTEM FOR MEASURING CONCENTRATED SOLAR RADIATION AND UNTRIPULATED AIR VEHICLE UNDERSTANDING|
    [返回顶部]