Patent Application
20220405910
This application claims priority to European patent application No. EP 21400014.3 filed on Jun. 22, 2021, the disclosure of which is incorporated in its entirety by reference herein.
The disclosure is related to a method of quantifying a loss of visibility through a transparent object caused by icing on a surface of the transparent object. The disclosure is further related to a measurement arrangement that is configured to perform a method of quantifying a loss of visibility through a transparent object caused by icing on a surface of the transparent object.
Icing is a well-known phenomenon on vehicles, such as e.g., rotary wing aircrafts and, more particularly, helicopters. More specifically, icing and a resulting ice accretion e.g., on a windshield of a helicopter may lead to a loss of transparency of the windshield and, thus, a loss of visibility leading to a reduced visibility through the windshield for the helicopter's flight crew. Therefore, in order to enable flights of a helicopter under full- or even light-icing conditions, the helicopter's windshield must mandatorily be equipped with an ice protection system with suitable anti- or de-icing capabilities. Such an ice protection system is usually provided by the manufacturer of the helicopter and defined on the basis of predetermined anti- or de-icing performance objectives, as well as corresponding test protocols.
Currently, various different predetermined anti- or de-icing performance objectives are used as a basis to define an ice protection system for a windshield of a helicopter. For instance, a heating power that is required for reaching a specific temperature threshold on the windshield's outer surface under certification-based icing conditions may be used as predetermined anti- or de-icing performance objective. Accordingly, the ice protection system for the windshield may be implemented using a windshield heating device. Other ice protection systems may e.g., be implemented using active vibrating devices or passive, hydrophobic and/or ice-repellent surface treatments, and so on.
By way of example, the document WO 2018/050786 A1 describes an ice protection system with an active vibrating device. The document WO 2018/209098 A1 describes an ice protection system with a passive, hydrophobic surface treatment.
However, the predetermined anti- or de-icing performance objectives underlying a windshield heating device are not suitable for implementation of active vibrating devices or passive, hydrophobic and/or ice-repellent surface treatments. Similarly, the predetermined anti- or de-icing performance objectives underlying active or passive devices, such as active vibrating devices or passive, hydrophobic and/or ice-repellent surface treatments, are not suitable for implementation of windshield heating devices. Similarly, the predetermined anti- or de-icing performance objectives underlying active vibrating devices or passive, hydrophobic and/or ice-repellent surface treatments associated with non-transparent objects, such as e.g., rotor blades, air intakes and so on for helicopter applications, may not merely be transposed to ice protection systems for helicopter windshields.
More specifically, for active vibrating devices or passive, hydrophobic and/or ice-repellent surface treatments used in non-transparent objects the predetermined anti- or de-icing performance objectives may be based on parameters such as a maximum allowed ice adhesion strength and/or a maximum allowed ice accretion specific weight. However, these parameters are not suitable as a basis for the predetermined anti- or de-icing performance objectives in the context of helicopter windshields, where a transparent ice type, such as e.g., glaze ice, may be tolerable even if adhesion is strong and accretion specific weight is significant, while a translucent ice type, such as e.g., rime ice, may result in immediate loss of visibility independently from its adhesion strength or accretion specific weight and should, therefore, not accrete whatsoever.
An alternative parameter that may be used as a basis for the predetermined anti- or de-icing performance objectives of a transparent object such as a helicopter windshield is light transmittance which permits detection of ice accretion on the transparent object by measuring light transmission therethrough.
By way of example, the documents KR 10-1405120 B1 and EP 1 102 962 B1 describe detection of ice accretion by means of measuring light transmission.
However, light transmittance alone does not directly correlate with transparency and cannot characterize an empiric loss of visibility experienced by helicopter pilots. For instance, a translucent ice deposit may only generate a minor light transmittance decrease, but a significant loss of visibility. Conversely, tinted materials typically used for sunshade applications significantly reduce light transmittance while still being translucent.
At this point, it should be noted that also currently existing transparency measurement protocols, such as e.g., ASTM D1003, ISO 13468 haze measurement, and so on, are generally established for intrinsic material transparency measurement, i.e., static and homogeneous, and may, thus, not be used directly to measure dynamic and heterogeneous transparency change over time. Furthermore, they do not reflect heterogeneous loss of visibility generated by ice, as e.g., high-granularity ice deposits generally allow for higher “empirical visibility” than haze values reflect.
As a result, there is currently no measurement protocol that enables characterization of a loss of transparency of a transparent object, i.e., quantification of a loss of visibility through the transparent object, under icing conditions. Thus, it is a complex, laborious and time-consuming task, if possible at all, to compare e.g., existing heating anti- or de-icing technologies in anti- or de-icing systems with upcoming alternative anti- or de-icing technologies, such as the above-described active or passive device technologies.
It is, therefore, an object of the present disclosure to provide a method of quantifying a loss of visibility through a transparent object caused by icing on a surface of the transparent object, the method being suitable to enable comparison of different anti- or de-icing systems that use differing anti- or de-icing technologies. It is a further object of the present disclosure to provide a measurement arrangement that is configured to perform such a method of quantifying a loss of visibility through a transparent object caused by icing on a surface of the transparent object.
One object of the present disclosure is solved by a method of quantifying a loss of visibility through a transparent object caused by icing on a surface of the transparent object, said method comprising the features of claim 1.
More specifically, according to the present disclosure a method of quantifying a loss of visibility through a transparent object caused by icing on a surface of the transparent object is provided. The method comprises: providing a light source, a high contrast providing object, and an image acquisition device; emitting a light beam from the light source through the high contrast providing object toward the transparent object, the light beam being directed through the transparent object and the surface of the transparent object toward the image acquisition device; exposing the surface of the transparent object to icing conditions such that a layer of ice is formed by ice accretion on the surface, wherein the light beam traverses the layer of ice after having traversed the transparent object; acquiring a series of images over time of the high contrast providing object using the image acquisition device, wherein acquisition of at least two immediately successive images of the series of images is temporally spaced by a predetermined time interval; determining blur occurring in the series of images over the time; and quantifying the loss of visibility over the time through the transparent object on the basis of the determined blur.
Advantageously, this method of quantifying a loss of visibility through a transparent object caused by icing on a surface of the transparent object defines a new test protocol that is usable to characterize a visual impairment generated by ice accretion on a transparent object, such as e.g., a helicopter windshield. This new test protocol may be used for research or serial purposes in the context of new anti- or de-icing performance specifications. In particular, the method according to the present disclosure enables besides others the possibility to open/extend future windshield tenders to innovative anti- or de-icing systems, the performance of which can currently not be assessed.
More particularly, the method of quantifying a loss of visibility through a transparent object caused by icing on a surface of the transparent object advantageously combines a suitable transparent object icing protocol and a picture analysis method. The transparent object icing protocol may be performed in an icing wind tunnel.
Advantageously, the method is adaptable to transparent objects in multiple applications, e.g., in any kind of vehicle, and may be applied to a multitude of different transparent objects, such as e.g., windshields, camera covers, sensor covers, and so on, via a simple parameter adaptation. As a result, determination of a transparency index for a given transparent object type that comprises a predetermined material and that is exposed to a given ice type is enabled as a function over time, i.e., transparencymaterial_xicetype_y=f(time).
The transparent object icing protocol preferably consists in emitting a light beam from a light source through a high contrast providing object through a transparent object and a surface of the transparent object, on which a layer of ice is formed by ice accretion, toward an image acquisition device, and acquiring a series of images over time of the high contrast providing object using an image acquisition device. A suitable high contrast providing object is e.g., a diaphragm, such that respectively acquired images are pictures taken of the diaphragm. In other words, pictures of the diaphragm are taken at a set time interval, which may be constant or not.
The transparent object may be a sample that is subjected to the icing conditions in the icing wind tunnel, or e.g., a windshield installed on a vehicle, such as a rotary wing aircraft, in particular a helicopter, or a car, etc.
The image acquisition device may be a camera and must be isolated from a respectively created or existing icing atmosphere in order to prevent parasitic ice and/or condensation deposits on its lens, which would affect an achievable quality of the pictures taken and, thus, a respective quality of an overall achievable result. This may be ensured by means of a cover or transparent wind tunnel wall.
An occurring loss of visibility may be quantified by analysing how blur a reference is seen through the transparent object. This reference is preferably the high contrast providing object that may be a backlit diaphragm, or any other object that provides a high contrast in the absence of ice. The reference must also be isolated from the respectively created or existing icing atmosphere in order to avoid parasitic ice accretion, water condensation, etc. which affect the achievable quality of the pictures taken and, thus, the respective quality of the overall achievable result. If a dedicated icing wind tunnel is used, dry bleed air may for instance be blown onto the reference and/or the transparent wind tunnel walls to this end.
Furthermore, ice shall not accrete on a back side of the transparent object which should, in addition, be protected from dust and/or water condensation. Therefore, and in order to avoid wake, recirculation, turbulence, etc., various contraptions may be used, such as e.g., spoilers or flaps, both up- and downstream of the transparent object.
The picture analysis method preferably consists in combining the pictures taken at the set time interval into respective picture batches, and analyzing the respective picture batches to determine an evolution over time of a respective transparency loss, i.e., loss of visibility, in order to derive an associated transparency index. Analyzing the respective picture batches may e.g., be based on a gray level analysis of each picture by means of a function that maps a number of pixels to gray levels in each picture, the function being defined as Gray_level=f(number of pixels), and subsequently analyzing evolution of the respectively determined gray levels. In other words, a haze level for each picture may for instance be correlated with a minimum value of a second derivative of a determined Gray_level=f(number of pixel) curve. Thus, a respective end result that may be obtained could describe a Haze=f(transparent material, icing conditions, time) curve, which can be linked to a pass/fail criterion and, thus, define an anti-icing performance objective for research or specification purposes, and/or a live Haze measurement that could be associated with a close-loop “automatic anti-icing” mode on an anti-iced transparency.
Advantageously, the picture analysis method may be extended to heterogeneous optical effects that cannot be quantified by currently existing transparency measurement protocols, e.g., the so-called “orange-peel” effect, the unidirectional polishing-induced halo effect, and so on. Furthermore, instead of using the picture analysis method only with a transparent object icing protocol that is performed in a dedicated icing wind tunnel, the picture analysis method may likewise be used as base principle for a vehicle onboard ice detection and/or protection system, for windshields or other subsystems exposed to icing.
According to some aspects, determining the blur comprises determining an individual haze level for each acquired image of the series of images, wherein quantifying the loss of visibility over the time through the transparent object on the basis of the determined blur comprises quantifying the loss of visibility over the time through the transparent object on the basis of the determined individual haze levels.
According to some aspects, determining an individual haze level for each acquired image of the series of images comprises correlating each determined individual haze level with a minimum value of a second derivative of a function that maps a number of pixels to gray levels in an associated acquired image, the function being defined as Gray_level=f(number of pixels).
According to some aspects, quantifying the loss of visibility over the time through the transparent object on the basis of the determined individual haze levels comprises plotting the determined individual haze levels into a diagram using a function that associates each determined individual haze level at least with a time stamp, icing conditions at a point of time indicated by the time stamp, and an associated material of the transparent object, wherein each time stamp represents an acquisition time of an associated acquired image, and wherein the function is defined as Haze_level=f(transparent object material, icing conditions, time stamp).
According to some aspects, plotting the determined individual haze levels into a diagram comprises deriving an overall transparency index for the transparent object from the diagram.
According to some aspects, the method further comprises associating a suitable de-icing procedure for the surface of the transparent object with the quantified loss of visibility.
According to some aspects, the transparent object is arranged inside an icing wind tunnel, wherein exposing the surface of the transparent object to icing conditions comprises isolating the high contrast providing object and the image acquisition device from the icing conditions to avoid at least parasitic ice accretion, water condensation and/or dust deposition on the high contrast providing object and the image acquisition device.
According to some aspects, isolating the high contrast providing object and the image acquisition device from the icing conditions comprises covering the high contrast providing object and the image acquisition device by means of associated covers at least between acquisition of immediately successive images of the series of images.
According to some aspects, isolating the high contrast providing object and the image acquisition device from the icing conditions comprises blowing dry bleed air onto the high contrast providing object and/or the image acquisition device.
According to some aspects, blowing dry bleed air onto the high contrast providing object and/or the image acquisition device comprises at least blowing the dry bleed air along associated tunnel walls of the icing wind tunnel in the region of the high contrast providing object and/or the image acquisition device.
According to some aspects, exposing the surface of the transparent object to icing conditions comprises isolating an opposed surface of the transparent object from the icing conditions to avoid at least parasitic ice accretion, water condensation and/or dust deposition on the opposed surface.
According to some aspects, the image acquisition device comprises a camera.
According to some aspects, the high contrast providing object comprises a backlit diaphragm.
According to some aspects, the transparent object is a vehicle windshield or a sample of a vehicle windshield, in particular an aircraft windshield or a sample of an aircraft windshield.
Advantageously, the vehicle windshield may be the windshield of a wide range of vehicles including, but not being limited to, helicopters, aircrafts, cars, and vessels. Preferably, the vehicle is a rotary wing aircraft and, more particularly, a helicopter.
The other object of the present disclosure is solved by a measurement arrangement that is configured to perform a method of quantifying a loss of visibility through a transparent object caused by icing on a surface of the transparent object as described above.
Preferred embodiments of the disclosure are outlined by way of example in the following description with reference to the attached drawings. In these attached drawings, identical or identically functioning components and elements are labeled with identical reference numbers and characters and are, consequently, only described once in the following description.
According to one aspect of the present disclosure, the measurement arrangement 100 is configured to perform a method of quantifying a loss of visibility through the transparent object 110 caused by icing on the surface 115 of the transparent object 110. Preferably, the surface 115 of the transparent object 110 is subjected to icing conditions such that a layer of ice 150 is formed by ice accretion on the surface 115.
By way of example, the measurement arrangement 100 is mounted to an icing wind tunnel 120 which enables creation of suitable icing conditions. Illustratively, the icing wind tunnel 120 is formed with opposed, preferably diametrically opposed, wind tunnel walls 122, 124, wherein the high contrast providing object 180 and the light source 160 are arranged behind the wind tunnel wall 124, and wherein the image acquisition device 190 is arranged behind the wind tunnel wall 122.
In other words, the light source 160, the high contrast providing object 180 and the image acquisition device 190 are preferably arranged outside of the icing wind tunnel 120. However, in order to enable traversal of the light beam 170 emitted from the light source 160 through the high contrast providing object 180 toward the image acquisition device 190, the wind tunnel walls 124, 122 may be transparent in the region of the light source 160, the high contrast providing object 180 and the image acquisition device 190. Alternatively, or in addition, suitable covers 123, 125 may be provided at the wind tunnel walls 122, 124, which may either be transparent or movable so as to be opened as required to enable traversal of the light beam 170 emitted from the light source 160 through the high contrast providing object 180 toward the image acquisition device 190.
In contrast to the light source 160, the high contrast providing object 180 and the image acquisition device 190, the transparent object 110 is illustratively arranged inside of the icing wind tunnel 120. By way of example, any suitable mounting element may be used to mount the transparent object 110 in the icing wind tunnel 120 between the wind tunnel walls 122, 124 such that the light beam 170 emitted from the light source 160 through the high contrast providing object 180 is directed through the transparent object 110 and the surface 115 of the transparent object 110 toward the image acquisition device 190.
For instance, the transparent object 110 is a vehicle windshield or a sample of a vehicle windshield, in particular an aircraft windshield or a sample of an aircraft windshield. The high contrast providing object 180 may e.g., comprise a backlit diaphragm or any other object that provides a high contrast in the absence of ice. The image acquisition device 190 may e.g., comprise a camera.
In an illustrative operation of the measurement arrangement 100 for quantifying a loss of visibility through the transparent object 110 caused by icing on the surface 115 of the transparent object 110, the transparent object 110 is subjected to icing conditions such that the layer of ice 150 is formed by ice accretion on the surface 115. The icing conditions are preferably obtained by means of an icing wind flow 130 that is directed in the icing wind tunnel 120 toward the surface 115 of the transparent object 110 and that creates an icing atmosphere 140 on the surface 115 of the transparent object 110 to cause a desired ice accretion on the surface 115 such that the layer of ice 150 is formed. Accordingly, the light beam 170 emitted from the light source 160 through the high contrast providing object 180 and the transparent object 110 as well as the surface 115 of the transparent object 110 toward the image acquisition device 190 traverses the layer of ice 150 after having traversed the transparent object 110 and prior to reaching the image acquisition device 190. Thus, the image acquisition device 190 may acquire a series of images over time of the high contrast providing object 180, as described below at
However, in order to guarantee obtention of accurate results in operation of the measurement arrangement 100, the high contrast providing object 180, as well as the light source 160 and the image acquisition device 190 are preferably isolated from the icing conditions to avoid at least parasitic ice accretion, water condensation and/or dust deposition on the high contrast providing object 180 and/or the image acquisition device 190. This may be achieved by means of the covers 123, 125 on the wind tunnel walls 122, 124, which may e.g., cover the image acquisition device 190 and the high contrast providing object 180 at least between acquisition of immediately successive images taken by the image acquisition device 190, or by embodying at least partly transparent wind tunnel walls 122, 124, as described above. Furthermore, dry bleed air may be blown onto the high contrast providing object 180 and/or the image acquisition device 190, and/or along the wind tunnel walls 124, 122 in the region of the high contrast providing object 180 and/or the image acquisition device 190.
Moreover, still in order to guarantee obtention of accurate results in operation of the measurement arrangement 100, a surface 117 of the transparent object 110 that is opposed to the surface 115 is preferably isolated from the icing conditions to avoid at least parasitic ice accretion, water condensation and/or dust deposition on the opposed surface 117. This may e.g., be achieved by means of various contraptions, such as e.g., spoilers or flaps, both up- and downstream of the transparent object 110, which may be used to avoid wake, recirculation, turbulence, etc. on the transparent object. However, suitable contraptions are well-known to the person skilled in the art and, therefore, not illustrated in detail in
According to one aspect of the present disclosure, the six separate images 210, 220, 230, 240, 250, 260 are taken over time at a set time interval, which may be constant or not. In other words, acquisition of at least two immediately successive images of the series of images 200, e.g., the images 210, 220, is temporally spaced by a predetermined time interval.
Illustratively, blur occurring in the series of images 200 increases. More specifically, the blur increases with a respectively increasing ice accretion level on the surface 115 of the transparent object 110 of
More specifically, the gray level function diagram 300 illustrates a measured gray level function 310 and a theoretical gray level function 320. The theoretical gray level function 320 illustrates a comparative gray level function associated with the transition zone 340 in non-icing conditions, i.e., without blur and, consequently, with optimal contrast and without haze. Accordingly, the left-hand portion of the illustrated transition zone 340, i.e., illustratively the inner portion of the high contrast providing object 180, has a desired white part of gray value 255, while the right-hand portion of the illustrated transition zone 340, i.e., illustratively the portion outside of the high contrast providing object 180, has a black part of gray value 0. Thus, the theoretical gray level function 320 has a rectangular form with a sharp edge.
In contrast thereto, the measured gray level function 310 illustrates actually present gray levels associated with the transition zone 340 in icing conditions, i.e., with blur due to haze and, consequently, reduced contrast. Accordingly, the gray level of the left-hand portion of the illustrated transition zone 340, i.e., illustratively the inner portion of the high contrast providing object 180, is reduced compared to the theoretical gray level function 320, and transition to the gray level of the right-hand portion of the illustrated transition zone 340, i.e., illustratively the portion outside of the high contrast providing object 180, is stretched. Thus, instead of having a rectangular form with a sharp edge, the measured gray level function 310 has the form of a rounded rectangle with a ramp-shaped transition.
As a result, a comparison of the measured gray level function 310 with the theoretical gray level function 320 enables determination of an actual transparency reduction and, thus, an actual transparency loss of the transparent object 110 of
Preferably, a gray level analysis of each one of the images 210, 220, 230, 240, 250, 260 of
In an optional step S470, a suitable de-icing procedure for the surface of the transparent object is associated with the quantified loss of visibility. Thus, if a quantified loss of visibility exceeds e.g., a predetermined threshold, de-icing of the transparent object may be initiated, as described in more detail below at
According to one aspect, determining the blur at step S450 comprises determining an individual haze level for each acquired image (e.g., each one of the images 210, 220, 230, 240, 250, 260 of
Thus, quantifying the loss of visibility over the time through the transparent object on the basis of the determined blur at step S460 may comprise quantifying the loss of visibility over the time through the transparent object on the basis of the determined individual haze levels. More specifically, quantifying the loss of visibility over the time through the transparent object on the basis of the determined individual haze levels may comprise plotting the determined individual haze levels into a diagram using a function that associates each determined individual haze level at least with a time stamp, icing conditions at a point of time indicated by the time stamp, and an associated material of the transparent object. Each time stamp preferably represents an acquisition time of an associated acquired image. The function is preferably defined as Haze_level=f(transparent object material, icing conditions, time stamp). Plotting the determined individual haze levels into a diagram may comprise deriving an overall transparency index for the transparent object from the diagram.
According to one aspect, exposing the surface of the transparent object at step S430 to icing conditions comprises isolating the high contrast providing object and the image acquisition device from the icing conditions. Thus, at least parasitic ice accretion, water condensation and/or dust deposition on the high contrast providing object and the image acquisition device may be avoided.
Isolating the high contrast providing object and the image acquisition device from the icing conditions may comprise covering the high contrast providing object and the image acquisition device by means of associated covers (e.g., covers 123, 125 of
In addition, or alternatively, exposing the surface of the transparent object at step S430 to icing conditions may comprise isolating an opposed surface (e.g., opposed surface 117 in
The vehicle 500 may be any vehicle that may be equipped with the windshield 515, such as a spacecraft or an aircraft, e.g., a spaceship, an airplane, a rotary wing aircraft, in particular a helicopter, etc., a land-operated vehicle, e.g., a car, a bus, a truck, a train, etc., or even a watercraft, e.g., a ship, a boat, or a hovercraft, etc. The windshield 515 illustratively represents the transparent object 100 of
According to one aspect of the present disclosure, the vehicle frame 510 is provided with a measurement device 520. Preferably, the measurement device 520 is of the Pitot-type, i.e., it is formed similar to a Pitot tube or probe with an air flow channel 525 having associated air flow channel walls 527, 529 and an inlet opening 530 that points directly into the icing wind flow 130. Illustratively, the measurement device 520 is provided with the measurement arrangement 100 of
More specifically, the magnified detail view 560 shows a kinked section 570 of the air flow channel 525, to which the measurement arrangement 100 of
In an illustrative operation of the vehicle 500 and, thus, the measurement device 520, the icing wind flow 130 enters the air flow channel 525 via the inlet opening 530 and creates an icing atmosphere 140 that is blown in a flow direction 540 toward the surface 115 of the sample 550, where it causes ice accretion on the surface 115 of the sample 550 such that the layer of ice 150 is formed on the surface 115. Accordingly, the light beam 170 emitted from the light source 160 through the high contrast providing object 180 and the sample 550 as well as the surface 115 of the sample 550 toward the image acquisition device 190 traverses the layer of ice 150 after having traversed the sample 550 and prior to reaching the image acquisition device 190. Thus, the image acquisition device 190 may acquire a series of images over time of the high contrast providing object 180 (e.g., the series of images 200 of
According to one aspect of the present disclosure, the quantified loss of visibility over the time through the sample 550 is representative for a respective loss of visibility over the time through the windshield 515. Thus, in the vehicle 500 a suitable de-icing procedure for de-icing the windshield 515 may be activated e.g., if the respective loss of visibility exceeds a predetermined threshold.
For instance, if the vehicle 500 is an aircraft, such as e.g., a rotary wing aircraft and, more particularly, a helicopter, an associated flight control system of the aircraft may implement together with the measurement device 520 an ice protection system of the helicopter. The ice protection system may be adapted to control acquisition of the series of images over time of the high contrast providing object 180, and to determine blur occurring in the series of images over the time as well as to quantify the loss of visibility over the time through the sample 550 on the basis of the determined blur, preferably in accordance with the method steps S440, S450, and S460 as described above at
| Number | Date | Country | Kind |
|---|---|---|---|
| 21400014.3 | Jun 2021 | EP | regional |
