WO2006080873A1 - Improvement of the aerodynamic properties of ground vehicles - Google Patents

Improvement of the aerodynamic properties of ground vehicles Download PDF

Info

Publication number
WO2006080873A1
WO2006080873A1 PCT/SE2006/000031 SE2006000031W WO2006080873A1 WO 2006080873 A1 WO2006080873 A1 WO 2006080873A1 SE 2006000031 W SE2006000031 W SE 2006000031W WO 2006080873 A1 WO2006080873 A1 WO 2006080873A1
Authority
WO
WIPO (PCT)
Prior art keywords
air
vehicle
openings
modulator
approximately
Prior art date
Application number
PCT/SE2006/000031
Other languages
French (fr)
Inventor
Sam Fredriksson
Per Kjellgren
Original Assignee
Wm-Data Caran Ab
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Wm-Data Caran Ab filed Critical Wm-Data Caran Ab
Priority to EP06700063A priority Critical patent/EP1841639B1/en
Priority to AT06700063T priority patent/ATE485994T1/en
Priority to US11/813,188 priority patent/US7794011B2/en
Priority to DE602006017799T priority patent/DE602006017799D1/en
Publication of WO2006080873A1 publication Critical patent/WO2006080873A1/en
Priority to US12/853,975 priority patent/US20110031777A1/en

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B62LAND VEHICLES FOR TRAVELLING OTHERWISE THAN ON RAILS
    • B62DMOTOR VEHICLES; TRAILERS
    • B62D37/00Stabilising vehicle bodies without controlling suspension arrangements
    • B62D37/02Stabilising vehicle bodies without controlling suspension arrangements by aerodynamic means
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B62LAND VEHICLES FOR TRAVELLING OTHERWISE THAN ON RAILS
    • B62DMOTOR VEHICLES; TRAILERS
    • B62D35/00Vehicle bodies characterised by streamlining
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B62LAND VEHICLES FOR TRAVELLING OTHERWISE THAN ON RAILS
    • B62DMOTOR VEHICLES; TRAILERS
    • B62D35/00Vehicle bodies characterised by streamlining
    • B62D35/001For commercial vehicles or tractor-trailer combinations, e.g. caravans

Definitions

  • the present invention relates generally to the improvement of the aerodynamic properties of vehicles, such as trucks, busses, trains, trailers, passenger cars, hovercrafts and motorcycles. More particularly the invention relates to an airflow control system according to the preamble of claim 1 and a ground vehicle according to the preamble of claim 10.
  • bluff body i.e. a non-streamlined shape that produces considerable resistance when moving through the air, or a similar medium.
  • a region of separated airflow occurs over a large portion of the surface of a bluff body. This results in a high drag force and a large wake region.
  • the airflow often exhibits unsteadiness in the form of periodic vortex formation and shedding. Naturally, these effects are undesired. Therefore, to obtain low fuel consumption, bluff-body vehicle shapes should generally be avoided.
  • ground vehicles trucks, busses and trailers in particular
  • various regulations place restrictions on the vehicles' maximum outer dimensions.
  • blowers emit air through openings in the rear wall of the vehicle to increase the Bernoulli's total pressure behind the vehicle, and thus reduce the air resistance.
  • the blowers are also arranged to suck in air through openings in walls of the vehicle that are located in a so-called eddying zone.
  • the document US, 5,374,013 discloses a method for reducing the drag on a moving body, such as a truck.
  • the vehicle's rear air pressure is increased by forming a pressure shell having a large vortex behind the vehicle.
  • a plurality of dynamic flow controllers emit air via a respective high pressure nozzle, which may be rotatable to produce a vortex having a rotation axis parallel to the vehicle's driving direction.
  • the air from the individual flow controllers is then combined into the large vortex.
  • One object of the present invention is therefore to provide a solution, which alleviates the above-mentioned problems, and thus enables an uncomplicated, cost-efficient and reliable drag re- duction for ground vehicles.
  • Another object of the present invention is to improve the stability of a ground vehicle.
  • Yet another object of the present invention is to lessen any undesired lift forces exerted on a ground vehicle as a result of a high air resistance experienced by the vehicle.
  • the system includes an air modulator and a control unit.
  • the air modulator has an array of openings including a number of openings, which are arranged next to one another along an essentially straight line.
  • the control unit is adapted to control the air modulator to output oscillating air from each opening, such that air vortices are created outside the opening. These air vortices have spin axes that in proximity to the opening are essentially parallel to the essentially straight line.
  • the array of openings includes a number of slots, which each has a width and a length dimension where the length dimension is several factors larger than the width dimension.
  • the slot width dimension may lie in an interval from approximately 0,1 mm to approximately 10 mm
  • the slot length dimension may lie in an interval from approximately 30 mm to approximately 300 mm. More preferably, the width dimension lies in the 0,3 mm - 2,0 mm.
  • the slots are arranged next to one another along an essentially straight line parallel to each slot's length dimension. This opening configuration accomplishes a very cost- efficient implementation of the air modulator.
  • the array of openings instead includes a number of holes, which each has an opening dimension in an interval from approximately 0, 1 mm to approximately 10 mm, and more preferably, within 0,3 mm - 2,0 mm.
  • Such an opening configuration is highly flexible in terms of accomplishing an unobtrusive integration of the air modulator into a vehicle.
  • the air modulator includes a tubular element on which the array of openings is arranged.
  • the tubular element also includes a modulating member that extends along a substantial portion of an interior of the tubular element.
  • the modulating member has a polygon shaped cross section, and is rotatable around its symmetry axis in response to a control signal from the control unit, so as to produce the oscillating output of air. (I.e. the air oscillations are created as an amount of air located in an interspace between the modulating member and the tubular element is pushed out through the slot each time an edge of this element passes the slot).
  • This design is desirable because it provides an efficient and reliable means for generating a synchronized oscillating airflow through a large total opening area.
  • the air modulator includes at least one diaphragm, which is arranged in a cavity adjoining at least one of the openings in the array of openings.
  • the diaphragm is adapted to vibrate in response to a control signal from the control unit, so as to produce the oscillating output of air.
  • the air modulator includes at least one valve, which is arranged to emit an active airflow from a compressed air system in response to a control signal from the control unit.
  • the oscillating output of air is produced as the valves are repeatedly opened and closed.
  • control unit is adapted to control an air oscillating frequency of the air exiting from the array of openings in a range from approximately 5 Hz to approximately 500 Hz, or more preferably within 10 - 60 Hz. Namely, this renders it possible to adapt the air oscillating frequency to a most relevant range of vehicle speeds.
  • the initially described ground vehicle which includes least one of the proposed airflow control systems.
  • the air modulator of each of the at least one system is here arranged on the vehicle with the array of openings having such an orientation relative to the outer surface that when the vehicle travels at a particular speed, an amount of vortex shedding behind the rear surface is lower than if the vehicle had traveled at this speed without the at least one airflow control system.
  • one of the at least one airflow control system has its air modulator arranged essentially along an intersection line between the main upper surface and the rear surface. Namely, this positio- ning of the air modulator causes the oscillating air vortices to interact very efficiently with the lateral shear layers behind the vehicle.
  • one of the at least one airflow control system has its air modulator arranged essentially along an intersection line between the general front surface and the main upper surface. This positioning is also advantageous with respect to air resistance, how- ever, perhaps more as a complement rather than an alternative to the above-mentioned rear positioning.
  • a first airflow control system has its air modulator arranged essentially along a first intersection line between a first side surface and the rear surface.
  • a second airflow control system has its air modulator arranged essentially along a second intersection line between a second side surface and the rear surface.
  • each of the at least one airflow control system has its air modulator arranged on the vehicle with the essentially straight line of the respective array of openings oriented essentially perpendicular to a forward driving direction of the vehicle. This orientation is efficient because thereby a longest array is exposed to the airflow around the vehicle.
  • each of the at least one airflow control system has its air modulator arranged on the vehicle with the array of openings oriented, such that each opening emits air in a main direction having an angle of 90 to 175 degrees to the forward driving direction. Namely, angles in this range have been found to give rise to especially well-behaved airflow behind the vehicle.
  • the control unit is adapted to receive a velocity signal that represents a speed of the vehicle.
  • the control unit is then adapted control the air modulator in response to the velocity signal, such that a relatively high vehicle speed results in a com- paratively high output air oscillation frequency, and vice versa, a relatively low vehicle speed results in a comparatively low output air oscillation frequency.
  • the airflow control system may even be shut off. Namely, for optimal results, a velocity dependant oscillation frequency is desirable. However, at very low velocities, the air resistance becomes insignificant.
  • the control unit is also adapted to receive a velocity signal that represents a speed of the vehicle.
  • the control unit controls the air modulator in response to the velocity signal, such that a peak-to-peak amplitude of a speed of the air exiting from each opening is equivalent to approximately 0,5 time to approximately 10 times the speed (or the so-called freestream velocity).
  • the control unit may regulate both the output air oscillation frequency and the peak-to-peak amplitude of the air speed in response to the measured speed of the vehicle.
  • the vehicle includes a compressed air system, which is connected to the air modulator of at least one of the at least one air flow control system.
  • a compressed air system which is connected to the air modulator of at least one of the at least one air flow control system.
  • the vehicle includes at least one flow amplification surface, which is arranged on the vehicle downstream relative to the air flow of at least one of the at least one air modulator.
  • the at least one flow amplification surface is adapted to augment the air vortices.
  • the invention is beneficial in that it reduces the amount of soiling of the vehicle's exterior surfaces that results from the global vortices behind the vehicle.
  • the average wind noise level can be reduced.
  • Figure 1 illustrates how vortex shedding arises behind a ground vehicle without any airflow control mecha- nisms
  • FIGS. 2a-b show different views of a first type of ground vehicle, through which the operation principles of the invention are schematically illustrated,
  • Figure 3 shows an amplification surface in the form of a protruding plate according to one embodiment of the invention
  • Figure 4 illustrates how the invention may be applied to a second type of ground vehicle
  • Figures 5a-b show variations of a proposed air modulator ac- cording to a first embodiment of the invention
  • Figures 6a-b show variations of proposed air modulator according to a second embodiment of the invention
  • Figures 7a-b show variations of proposed air modulator according to a third embodiment of the invention
  • Figures 8a-c exemplify different configurations of the arrays of openings according to embodiments of the inven- tion.
  • FIG. 1 shows a ground vehicle 10 that travels in a forward direction D F .
  • the vehicle 10 is not equipped with any airflow con- trol mechanisms. Therefore, due to the vehicle's 10 pronounced bluff-body shape, a relatively large amount of vortex shedding 16 arises behind the vehicle 10.
  • Figure 2a shows a side-view of a first type of ground vehicle 100 in the form of a truck.
  • the vehicle 100 has a body with an outer surface including a general front surface 1 10, a bottom surface 115, a main upper surface 120, two side surfaces 130b (of which one appears in this view), and a rear surface 140.
  • the general front surface 1 10 extends also over an almost horizontal surface of the vehicle's cabin.
  • a transition from the general front surface 110 to the main upper surface 120 is defined to be at the front- most part of a horizontal vehicle top surface of substantial length.
  • the main upper surface 120 is normally delimited by the front and back edges of the vehicle's cargo space.
  • other delimitations may be applicable.
  • the vehicle 100 is equipped with at least one airflow control system to modify an air flow F around the vehicle 100, such that when the vehicle 100 travels at a particular speed (and wind conditions) the drag on the vehicle 100 is lower than if the vehicle 100 had traveled at this speed (and wind conditions) without the system.
  • the proposed system creates small-scale air vortices 150 adjacent to shear layers of the airflow F around the vehicle 100. This, in turn, weakens the strength of any of global vortex shedding behind the vehicle 100.
  • the airflow control system includes an air modulator and a control unit.
  • the airflow control sys- tern includes a plurality of air modulators 210a, 210b1 , 210b2, 210c, 210d1 , 210d2 (see figure 2b) and 21 Oe respectively and a common control unit 230.
  • a separate control unit for each air modulator is also conceivable.
  • Each air modulator 210a, 210b1 , 210b2, 210c, 210d1 , 210d2 and 21 Oe has an array of openings 215 that includes a number of slots or holes, i.e. one or more slots/holes.
  • the dimensions and aspect ratios of these openings will be discussed in detail below with reference to figures 5a to 8c. Nevertheless, the openings are arranged next to one another along an essentially straight line.
  • the control unit 230 is adapted to control each air modulator 210a, 210b1 , 210,b2, 210c, 210d1 , 210d2 and 21 Oe to output os- dilating air from each opening in such a manner that air vortices 150 are created outside the openings.
  • the air vortices 150 which have spin axes that in proximity to the openings are essentially parallel to the essentially straight line, are accomplished by repeatedly (either periodically or irregularly) pushing amounts of air from inside the air modulator out through the openings.
  • Different embodiments of air modulators according to the invention will be described below with reference to figures 5a, 5b, 6a, 6b, 7a and 7b.
  • each air modulator 210a, 210b1 , 210b2, 210c, 210d1 , 210d2 and 21 Oe is further arranged on the vehicle 100 with the essentially straight line of the respective array of openings 215 oriented essentially perpendicular to a forward driving direction D F of the vehicle 100. It is further preferable if the air modulators 210a, 21 ObI 1 210b2, 210c, 210d1 , 210d2 and 21 Oe are arranged on the vehicle 100, such that the openings of the respective air modulator are located downstream of a flow separation line FSL at which flow separation would occur if no synthetic air vortices 150 had been generated.
  • the air modulator openings are preferably positioned at the far back of the vehicle 100.
  • essentially perpendicular to the direction D F is meant a maximum deviation of 10 degrees from 90 degrees (i.e. from 80 degrees to 100 degrees). Consequently, the spin axes of the air vortices 150 are also (at least in proximity to the openings) essentially perpendicular to the direction D F . This is a key factor in the above-mentioned perturbation of the shear layers around the vehicle 100, which reduces the global vortices behind the vehicle 100.
  • one or more flow amplification surfaces 120, 160b, 160c, 16Od and 16Oe are provided further downstream of the each air modulator 210a, 210b1 , 210b2, 210c, 210d1 , 210d2 and 21 Oe respectively relative to the air flow F, which are adapted to augment the air vortices 150.
  • protruding plates 160b, 160c, 16Od and 16Oe may constitute the amplification surfaces.
  • Such protruding plates preferable have a profile that is slightly curved towards the rear surface 140. It is further advantageous if the plates are foldable, so that they do not protrude from the vehicle 100 when the airflow control system is inactive. Specific aspects of the protruding plates 160b, 160c, 16Od and 16Oe according to preferred embodiments of the invention will be discussed below with reference to figure 3.
  • a first air modulator 210a is arranged essentially along an intersection line between the general front surface 1 10 and the main upper surface 140 (i.e. here at the front edge of the vehicle's 100 cargo space).
  • the top surface 120 may serve as a flow amplification surface in respect of this air modulator 210a.
  • the side surface 130b may serve as a flow amplification surface in respect of an air modulator 210b2 arranged vertically at the front edge of the vehicle's 100 cargo space.
  • the control unit 230 controls the operation of the modulator 210a by means of a first control signal CMa. Moreover, a second air modulator 210c is arranged essentially along an intersection line between the main upper surface 120 and the rear surface 140 (i.e. here at the back edge of the vehicle's 100 cargo space). The control unit'230 controls the operation of this modulator 210c by means of a second control signal CMc.
  • control unit 230 controls the operation of a third and a fourth air modulator 210b and 21 Od (see figure 2b), which are arranged essentially along a first intersection line between a first side surface 130b and the rear surface 140, respective essentially along a second intersection line between a second side surface 13Od (see figure 2b) and the rear surface 140.
  • each air modulator 210a, 210b1 , 210b2, 210c, 210d1 , 210d2 and 21 Oe is arranged on the vehicle 100 with the array of openings 215 oriented, such that the openings thereof emit air in a main direc- tion A at an angle ⁇ j to the forward driving direction D F .
  • ⁇ j « 155 degrees.
  • a complementary angle ⁇ j c between a main direction A of for example the first air modulator 210a and the (essentially horizontal) main upper surface 120 is most preferably around 25 degrees.
  • the angle ⁇ j may lie anywhere in an interval from 90 degrees to 175 degrees (i.e. with a complementary angle ⁇ j c ranging from 5 degrees to 90 degrees).
  • Such a main direction A results in that the oscillating air vortices 150 interact very efficiently with the lateral shear layers of the air flow F behind the vehicle 100.
  • this is here illustrated in a highly simplified manner by .
  • air modulators 21 Oa 1 210b1 , 210b2, 210c, 2i ⁇ d1 , 210d2 and 21 Oe air modulators may be positioned for example at the rear surfaces of the vehicle's 100 fender wings.
  • an air modulator can be arranged along each bodyline of the vehicle 100 where flow separation occurs. Hence, if the vehicle 100 has a protruding engine hood, air modulators may also be positioned proximate to any edges of this hood.
  • FIG 2b which shows a top-view of the vehicle 100 in the figure 2a
  • the air modulators 210b1 , 210b2, 210d1 and 210d2 are oriented with their arrays of openings 215, such that the openings thereof emit air in a main direction A at the angle ⁇ j to the forward driving direction D F .
  • this main direction A results in that the oscillating air vortices 150 from the air modulators 210b1 , 210b2, 210d1 and 210d2 interact very efficiently with the vertical shear layers of the air flow F behind the vehicle 100.
  • control unit 230 receives a velocity signal V, which represents a speed of the vehicle 100.
  • V a velocity signal
  • 210b1 , 210b2, 210c, 210d1 , 210d2, 21 Oe and 210 in response to the velocity signal V, such that a relatively high vehicle speed results in a comparatively high output air oscillation frequency, and vice versa, a relatively low vehicle speed results in a comparatively low output air oscillation frequency.
  • control unit 230 may control at least one air modulator 210a, 210b1 , 210b2, 210c, 210d1 , 210d2, 21 Oe and/ or 210 in response to the velocity signal V, such that a peak-to- peak amplitude of an air speed exiting from each opening depends on the vehicle speed.
  • the peak-to-peak amplitude is equivalent to approximately 0,5 time to approximately 10 times the vehicle speed, and more preferably, the peak-to-peak amplitude is equivalent to approximately 1 time to approximately 3 times the vehicle speed.
  • the vehicle speed here represents the so-called freestream velocity, i.e. the speed at which the airflow F passes the vehicle 100.
  • a compressed air system 250 (which is normally included in the vehicle 100 for other purposes) is connected to at least one of the air modulators.
  • the compressed air system 250 is connected to the first air modulator 210a and the second air modulator 210c.
  • an active airflow P is supplied to the arrays of openings 215 of these modulators 210a and 210c respectively.
  • the amount of energy added to the airflow F via these modulators can be increased to improve their influence on the reduction of the vortex shedding.
  • FIG 3 shows an amplification surface in the form of a protruding plate 160 according to one embodiment of the invention.
  • the plate 160 is mounted at a rear surface 140 of a vehicle 100, such as the truck in the figures 2a and 2b.
  • the plate 160 protrudes from the rear surface 140 a dis- tance represented by an overall length ⁇ .
  • an air modulator 210 is arranged relative to the plate 160, such that an array of openings 215 of the modulator 210 is positioned a distance ⁇ c from a flow separation line FSL adjacent to the surface 140.
  • ⁇ G lies in an interval from 0 to 0,6OA, however, more preferably 0,05 ⁇ ⁇ ⁇ c ⁇ 0,30 ⁇ .
  • a non-dimensional normalized frequency F + is defined as:
  • f represents the frequency at which the air modulator 210 produces oscillating air vortices. It is desirable that the non- dimensional normalized frequency F + is larger than 0,05 and less than 30. More preferably 0, 1 ⁇ F + ⁇ 1 ,0, and optimally F + lies in an interval from 0,1 to 0,6.
  • Figure 4 shows a second type of ground vehicle 100 in the form of a bus. Also this vehicle 100 has a body with an outer surface that includes a general front surface 1 10, a main upper surface 120, two side surfaces 130b (of which one appears in this view), and a rear surface 140.
  • the general front surface 110 transitions into the main upper surface 120 relatively sharply, since in this case the horizontal vehicle top surface of substantial length begins almost immediately at front of the vehicle 100.
  • the vehicle 100 in the figure 4 is equipped with at least one airflow control system to modify an air flow F around the vehicle 100, such that when the vehicle 100 travels at a particular speed (and wind conditions) the drag on the vehicle 100 is lower than if the vehicle 100 had traveled at this speed (and wind conditions) without the system.
  • each air modulator has an array of openings 215 that includes a number of openings, which are arranged next to one another along an essentially straight line.
  • a control unit (not shown) controls each air modulator 210a1 , 210a2, 210b1 , 210b2, 210c and 21 Oe to output oscillating air from each opening in such a manner that air vortices are created outside the openings.
  • the air vortices which have spin axes that in proximity to the openings are essentially parallel to the essentially straight line, are accomplished by repeatedly (either periodically or irregularly, continuously varying or burst wise) pushing amounts of air from inside the air modulator out through the openings.
  • the air modulators 210a1 , 210a2, 210b1 , 210b2, 210c and 21 Oe are arranged on the vehicle 100 with the essentially straight line of the respective array of openings 215 oriented essentially perpendicular to a forward driving direction of the vehicle 100, so that the spin axes of the air vortices 150 are also (at least in proximity to the openings) essentially perpendicular to this direction.
  • each air modulator 210a1 , 210a2, 21 ObI 1 210b2, 210c and 21 Oe is arranged on the vehicle 100 with the array of openings 215 oriented, such that the openings thereof emit air in a main direction A at an angle ⁇ j to the forward driving direction D F , where ⁇ j preferably is around 155 degrees and a complementary angle ⁇ j c between a main direction A of for example the first air modulator 210a and the main upper surface 120 is preferably around 25 degrees.
  • the angle ⁇ j may lie anywhere in an interval from 90 degrees to 175 degrees (i.e. with a complementary angle ⁇ j c ranging from 5 degrees to 90 degrees).
  • the air modulators 210a1 , 210a2, 210b1 , 210b2, 210c and 21 Oe are arranged on the vehicle 100, such that the openings of the respective air modulator are located downstream of a flow separation line FSL at which flow separation would occur if no synthetic air vortices 150 had been generated.
  • the vehicle 100 has relatively rounded edges between the rear surface 140 and the side surfaces 1.30b, between the rear surface 140 and the bottom surface 115 and between the rear surface 140 and the top surface 120. Therefore, adequate flow amplification surfaces 120, 130b, 160b, 160c and 16Oe can be provided by portions of the vehicle's 100 body, namely said rounded edges.
  • an existing body shape may have to be modified to some extent in order to represent an optimal flow amplification surface. Nevertheless, these surfaces may be designed very discretely. Furthermore, the design may be complemented by one or more protruding plates, which can foldable, so that they do not protrude from the vehicle 100 when the airflow control system is inactive.
  • Figure 5a shows section of a proposed air modulator 210 accor- ding to a first embodiment of the invention.
  • the air modulator
  • This slot 515 has a width dimension W and a length L dimension, where the length dimension L is several factors larger than the width dimension W.
  • the width dimension W lies in a range from approximately 0, 1 mm to approximately 10 mm (more preferably, 0,3 mm ⁇ W ⁇ 2,0 mm), and the length dimension L lies in a range from approximately 30 mm to approximately 300 mm.
  • the tubular element includes a modulating member 520 that extends along a substantial portion of an interior of the tubular element.
  • the modulating member 520 has a polygon shaped cross section, such a hexagon or a pentagon.
  • any other re- gular or irregular cross section shape is conceivable according to the invention.
  • the modulating member 520 is rotatable around its symmetry axis 525 (or, if the cross section shape is irregular, center-of-gravity axis). Therefore, the cross section shape must allow the modulating member 520 to rotate freely within the tubular element of the air modulator 210.
  • a transmission line connects the modulating member 520 to a control unit 230 (see also figure 2a), such that this unit, by means of a control signal CM, may control the member 520 to produce a desired oscillating output of air.
  • this unit by means of a control signal CM, may control the member 520 to produce a desired oscillating output of air.
  • these air oscillations are created when an amount of air located in a interspace between the modulating member 520 and the tubular element is pushed out through the slot 515 ' each time an edge of the element 520 passes the slot 515.
  • a constant rotation speed and a regular cross section shape of the modulating member 520 causes equally large amounts of air to be emitted each time.
  • the openings in the air modulator's 210 array of openings may also have non- slot shaped profiles, such as circular, oval, polygon etc.
  • the control unit 230 is adapted to control the air oscillating frequency of the air exiting from each slot 515 in a range from approximately 5 Hz to approximately 500 Hz. The most desirable range is 10 - 60 Hz. It is further preferable if the oscillating frequency depends on a current vehicle speed. Therefore, as mentioned above, the control unit 230 may receive a velocity signal V representing a speed of the vehicle, in response thereto, control the modulating member 520, such that a relatively high vehicle speed results in a comparatively high output air oscillation frequency, and vice versa, a relatively low vehicle speed results in a comparatively low output air oscillation frequency.
  • Figure 6a shows a section of a proposed air modulator 210 according to a second embodiment of the invention.
  • the air modulator 210 includes at least one diaphragm 620, which is arranged in a cavity 625 adjoining at least one opening in the above-mentioned array of openings.
  • corresponding cavities and diaphragms are arranged behind each opening (here in the form of slots 615) in the air modulator's 210 array of openings.
  • each slot 615 has a width dimension W and a length L dimension, where the length dimension L is several factors larger than the width dimension W.
  • the width dimension W lies in a range from approximately 0, 1 mm to approximately 10 mm (more preferably 0,3-2,0 mm), and the length dimension L lies in a range from approximately 30 mm to approximately 300 mm.
  • all the slots 615 in the array of openings are positioned next to one another along an essentially straight line 630, which is parallel to each slot's 615 length dimension L.
  • the air modulator 210 is connected to a control unit 230, and the diaphragm 620 is adapted to vibrate in response to a control signal CM from the control unit 230, so as to produce the os- cillating output of air.
  • the control signal CM may in turn be correlated with a velocity signal V representing a speed of the vehicle onto which the air modulator 210 is mounted.
  • Figure 5b shows a section of the air modulator 210 according to the above-described first embodiment of the invention, however where the tubular element is connected to a compressed air system 250 via an air conduit.
  • an active airflow P is supplied to the tubular element.
  • Such an active air- flow P enables a net amount of air to added the airflow that surrounds a vehicle, and thus accomplished an enhancement of the performance of the proposed airflow control system.
  • the control unit 230 receives a velocity signal V, which represents a speed of the vehicle onto which the air modulator 210 is mounted.
  • the control unit 230 then controls the air modulator 210 in response to the velocity signal V, such that a peak-to-peak amplitude of a speed of the air exiting from each opening 515 is equivalent to approximately 0,5 time to approximately 10 times the speed.
  • Figure 6b shows the air modulator 210 according to the above- described second embodiment of the invention, however where the openings 715 in the array of openings are holes, i.e. apertures with an approximately equal opening dimension D in all directions.
  • the openings 715 may have a circular, oval or polygon shape.
  • the opening dimension D lies in a range from approximately 0,1 mm to approximately 10 mm, or more preferably 0,3 mm - 2,0 mm.
  • an air conduit connects the cavity 625 to a compressed air system 250.
  • FIG. 7a shows a section of the air modulator 210 according to a third embodiment of the invention, wherein an array of openings 215 contains a number of openings 715 arranged next to one another along an essentially straight line 530.
  • the air modulator 210 is represented by a set of valves 710, 720, 730 and 740 respectively. Namely, each opening 715 is connected to an air conduit, which is further connected to one of the valves 710, 720, 730 and 740. Each of these valves, in turn, 710, 720, 730 and 740 is connected to a compressed air system 250 via one or more further air conduits, so that an active airflow P can be received.
  • Each valve 710, 720, 730 and 740 is controllable by a control unit 230 in response to a control signal CM. Thereby, the openings 715 may be controlled to emit synthetic air vortices according to what has been described above.
  • Figure 7b shows a section of the air modulator 210 according to the third embodiment of the invention, however, where a sub-set of openings 615 are connected to a common air chamber 71 1 , 721 , 731 and 741 respectively.
  • a respective valve 710, 720, 730 and 740 controls an active airflow P to each air chamber 71 1 , 721 , 731 and 741 .
  • the valves 710, 720, 730 and 740 are, in turn, are controlled in response to a control signal CM from a control unit 230.
  • the active airflow P is fed to the valves 710, 720, 730 and 740 from a compressed air system 250 via one or more air conduits.
  • the control unit 230 may control the openings 615 to emit synthetic air vortices according to what has been described above.
  • valves that are common for more than one opening as shown in the figures 7a and 7b, a separate valve may equally well be employed to control the airflow from each opening.
  • an active air flow P may be supplied to the openings of the air modulator 210 alternately either from a first air system providing air at a pressure such that air flows out of the air modulator openings, or from a second air system providing air at a pressure such that air is sucked in through the air modulator openings.
  • the active air flow P may be controlled so that its average pressure level attains a desired value.
  • Figure 8a illustrates an array of openings 215 where a number of slot shaped openings 615, e.g. six, are arranged next to one another along an at least essentially straight line 630, which is parallel to each slot's 615 length dimension L.
  • the length sides of the slots 615 form the essentially straight line 630.
  • Figure 8b illustrates another array of openings 215 where a number of openings in the form of holes 715 are arranged next to one another along an at least essentially straight line 630. In this case, however, only few of the holes 715 actually lie on this line 630. The remaining holes 715 are slightly displaced with respect to the essentially straight line 630.
  • Figure 8c illustrates yet another slot array 215 where a number of openings in the form of slots 615 are arranged next to one another along an at least essentially straight line 630, which is parallel to each slot's 615 length dimension L.
  • some of the slots 615 are slightly displaced with respect to the essentially straight line 630, whereas the length sides of other slots 615 are aligned with this line 630.
  • protective shields may be provided, which are controllable in response to a velocity signal that represents the speed of the vehicle, so that the shields either cover or expose the openings to the exterior depending on a current vehicle speed.

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Transportation (AREA)
  • Mechanical Engineering (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Body Structure For Vehicles (AREA)
  • Vehicle Body Suspensions (AREA)
  • Air-Conditioning For Vehicles (AREA)

Abstract

The present invention relates to the improvement of the aerody namic properties of bluff-body shaped ground vehicles (100). A least one air modulator (210, 21 Oa1 210b1 , 210b2, 210c, 21 Oe is assembled on the vehicle (100) to modify an air flow (F around the vehicle (100), such that the drag on the vehicle (100 is decreased. Each air modulator (210, 210a, 210b1 , 210b2 210c, 21 Oe) has an array of openings (215) including a numbe of openings, which are arranged next to one another along a essentially straight line. A control unit (230) controls the at leas one air modulator (210, 210a, 210b1 , 210b2, 210c, 21 Oe) t output oscillating air from each opening such that air vortice (150) are formed outside the opening. The at least one ai modulator (210, 210a, 210b1 , 210b2, 210c, 21 Oe) is arranged o the vehicle (100), such that these air vortices (150) have spi axes that in proximity to the opening are essentially perpen dicular to a forward driving direction (DF) of the vehicle (100).

Description

Applicant: WM-data Caran AB
Improvement of the Aerodynamic Properties of Ground Vehicles
THE BACKGROUND OF THE INVENTION AND PRIOR ART The present invention relates generally to the improvement of the aerodynamic properties of vehicles, such as trucks, busses, trains, trailers, passenger cars, hovercrafts and motorcycles. More particularly the invention relates to an airflow control system according to the preamble of claim 1 and a ground vehicle according to the preamble of claim 10.
Various solutions are known for improving the aerodynamic properties of a so-called bluff body, i.e. a non-streamlined shape that produces considerable resistance when moving through the air, or a similar medium. Typically, a region of separated airflow occurs over a large portion of the surface of a bluff body. This results in a high drag force and a large wake region. The airflow often exhibits unsteadiness in the form of periodic vortex formation and shedding. Naturally, these effects are undesired. Therefore, to obtain low fuel consumption, bluff-body vehicle shapes should generally be avoided. However, for ground vehicles (trucks, busses and trailers in particular) various regulations place restrictions on the vehicles' maximum outer dimensions. Thus, in order to economize the available vehicle volume, heavy vehicles are normally designed with a shape which to a large extent is a bluff body, i.e. where the front and back surfaces are essentially flat, vertical walls. Instead, to reduce the known drawbacks of such a vehicle shape, airflow control systems may be used to improve the aerodynamics. The document US, 5,908,217 describes a pneumatic aerodynamic control and drag-reduction system for ground vehicles. The system reduces flow separation at the rear portion of a moving vehicle by discharging air at this portion of the vehicle. Blowing outlets are arranged to discharge the air through one or more tangential slots which extend transversely of the upper and/or lower rear portion of the vehicle. Moreover, differential right/left blowing systems may be used to counteract lateral and directional instabilities, for instance when the vehicle is exposed to side winds.
The document US, 5,407,245 shows another solution for reducing the drag in the rear region of a vehicle. Blowers emit air through openings in the rear wall of the vehicle to increase the Bernoulli's total pressure behind the vehicle, and thus reduce the air resistance. Here, the blowers are also arranged to suck in air through openings in walls of the vehicle that are located in a so-called eddying zone.
The document US, 5,374,013 discloses a method for reducing the drag on a moving body, such as a truck. Here, the vehicle's rear air pressure is increased by forming a pressure shell having a large vortex behind the vehicle. Specifically, a plurality of dynamic flow controllers emit air via a respective high pressure nozzle, which may be rotatable to produce a vortex having a rotation axis parallel to the vehicle's driving direction. The air from the individual flow controllers is then combined into the large vortex.
Thus, various solutions are known for improving the aerodynamic properties of bluff-body shaped vehicles. However, the known strategies either fail to reduce the air drag behind large vehicles sufficiently, and/or these strategies imply an apparatus that is complex, expensive and/or unreliable. SUMMARY OF THE INVENTION
One object of the present invention is therefore to provide a solution, which alleviates the above-mentioned problems, and thus enables an uncomplicated, cost-efficient and reliable drag re- duction for ground vehicles.
Another object of the present invention is to improve the stability of a ground vehicle.
Yet another object of the present invention is to lessen any undesired lift forces exerted on a ground vehicle as a result of a high air resistance experienced by the vehicle.
According to one aspect of the invention, these objects are achieved by the initially described airflow control system, wherein the system includes an air modulator and a control unit. The air modulator has an array of openings including a number of openings, which are arranged next to one another along an essentially straight line. The control unit is adapted to control the air modulator to output oscillating air from each opening, such that air vortices are created outside the opening. These air vortices have spin axes that in proximity to the opening are essentially parallel to the essentially straight line.
An important advantage attained by this system is that the oscillating (or non-steady-state) airflow generated thereby pertur- bates the shear layers around the vehicle. This in turn, reduces the global vortices (or eddies) that arise behind the vehicle. Moreover, these vortices arise more remote from the vehicle. As a result, the vehicle's air resistance decreases and the fuel consumption can be lowered. Furthermore, any tailing passenger cars or motorcycles experience less stability problems when approaching from behind the vehicle.
According to one embodiment of this aspect of the invention, the array of openings includes a number of slots, which each has a width and a length dimension where the length dimension is several factors larger than the width dimension. For instance, the slot width dimension may lie in an interval from approximately 0,1 mm to approximately 10 mm, and the slot length dimension may lie in an interval from approximately 30 mm to approximately 300 mm. More preferably, the width dimension lies in the 0,3 mm - 2,0 mm. The slots are arranged next to one another along an essentially straight line parallel to each slot's length dimension. This opening configuration accomplishes a very cost- efficient implementation of the air modulator.
According to another embodiment of this aspect of the invention, the array of openings instead includes a number of holes, which each has an opening dimension in an interval from approximately 0, 1 mm to approximately 10 mm, and more preferably, within 0,3 mm - 2,0 mm. Such an opening configuration is highly flexible in terms of accomplishing an unobtrusive integration of the air modulator into a vehicle.
According to a further embodiment of this aspect of the invention, the air modulator includes a tubular element on which the array of openings is arranged. The tubular element also includes a modulating member that extends along a substantial portion of an interior of the tubular element. The modulating member has a polygon shaped cross section, and is rotatable around its symmetry axis in response to a control signal from the control unit, so as to produce the oscillating output of air. (I.e. the air oscillations are created as an amount of air located in an interspace between the modulating member and the tubular element is pushed out through the slot each time an edge of this element passes the slot). This design is desirable because it provides an efficient and reliable means for generating a synchronized oscillating airflow through a large total opening area.
According to another embodiment of this aspect of the invention, the air modulator includes at least one diaphragm, which is arranged in a cavity adjoining at least one of the openings in the array of openings. The diaphragm is adapted to vibrate in response to a control signal from the control unit, so as to produce the oscillating output of air. This design is desirable because it enables a slim air modulator profile, i.e. it is comparatively straightforward to integrate this unit in an existing vehicle body.
According to a further embodiment of this aspect of the inven- tion, the air modulator includes at least one valve, which is arranged to emit an active airflow from a compressed air system in response to a control signal from the control unit. Thereby, the oscillating output of air is produced as the valves are repeatedly opened and closed.
According to yet another embodiment of this aspect of the invention, the control unit is adapted to control an air oscillating frequency of the air exiting from the array of openings in a range from approximately 5 Hz to approximately 500 Hz, or more preferably within 10 - 60 Hz. Namely, this renders it possible to adapt the air oscillating frequency to a most relevant range of vehicle speeds.
According to another aspect of the invention, these objects are achieved by the initially described ground vehicle, which includes least one of the proposed airflow control systems. The air modulator of each of the at least one system is here arranged on the vehicle with the array of openings having such an orientation relative to the outer surface that when the vehicle travels at a particular speed, an amount of vortex shedding behind the rear surface is lower than if the vehicle had traveled at this speed without the at least one airflow control system.
According to one embodiment of this aspect of the invention, one of the at least one airflow control system has its air modulator arranged essentially along an intersection line between the main upper surface and the rear surface. Namely, this positio- ning of the air modulator causes the oscillating air vortices to interact very efficiently with the lateral shear layers behind the vehicle.
According to another embodiment of this aspect of the invention, one of the at least one airflow control system has its air modulator arranged essentially along an intersection line between the general front surface and the main upper surface. This positioning is also advantageous with respect to air resistance, how- ever, perhaps more as a complement rather than an alternative to the above-mentioned rear positioning.
According to still another embodiment of this aspect of the invention, a first airflow control system has its air modulator arranged essentially along a first intersection line between a first side surface and the rear surface. Correspondingly, a second airflow control system has its air modulator arranged essentially along a second intersection line between a second side surface and the rear surface. Such a positioning of the air modulators causes the oscillating air vortices to interact very efficiently with the vertical shear layers behind the vehicle, and thus reduce the drag.
According to yet another embodiment of this aspect of the invention, each of the at least one airflow control system has its air modulator arranged on the vehicle with the essentially straight line of the respective array of openings oriented essentially perpendicular to a forward driving direction of the vehicle. This orientation is efficient because thereby a longest array is exposed to the airflow around the vehicle.
According to another embodiment of this aspect of the invention, each of the at least one airflow control system has its air modulator arranged on the vehicle with the array of openings oriented, such that each opening emits air in a main direction having an angle of 90 to 175 degrees to the forward driving direction. Namely, angles in this range have been found to give rise to especially well-behaved airflow behind the vehicle.
According to still another embodiment of this aspect of the invention, the control unit is adapted to receive a velocity signal that represents a speed of the vehicle. The control unit is then adapted control the air modulator in response to the velocity signal, such that a relatively high vehicle speed results in a com- paratively high output air oscillation frequency, and vice versa, a relatively low vehicle speed results in a comparatively low output air oscillation frequency. For very low velocities, the airflow control system may even be shut off. Namely, for optimal results, a velocity dependant oscillation frequency is desirable. However, at very low velocities, the air resistance becomes insignificant.
According to yet another embodiment of this aspect of the in- vention, the control unit is also adapted to receive a velocity signal that represents a speed of the vehicle. Here, however, the control unit controls the air modulator in response to the velocity signal, such that a peak-to-peak amplitude of a speed of the air exiting from each opening is equivalent to approximately 0,5 time to approximately 10 times the speed (or the so-called freestream velocity). Namely, also the amount of airflow energy to add for optimal results depends the vehicle's speed. Naturally, the control unit may regulate both the output air oscillation frequency and the peak-to-peak amplitude of the air speed in response to the measured speed of the vehicle.
According to another embodiment of this aspect of the invention, the vehicle includes a compressed air system, which is connected to the air modulator of at least one of the at least one air flow control system. Thereby, an active airflow can be supplied to the array of openings, such that the energy added to the airflow around the vehicle is increased. Hence, the advantageous effects of the proposed air vortices are improved.
According to a further embodiment of this aspect of the invention, the vehicle includes at least one flow amplification surface, which is arranged on the vehicle downstream relative to the air flow of at least one of the at least one air modulator. The at least one flow amplification surface is adapted to augment the air vortices. Thereby, the efficiency of the airflow control system is improved. In addition to the above-mentioned advantages, the invention is beneficial in that it reduces the amount of soiling of the vehicle's exterior surfaces that results from the global vortices behind the vehicle. Moreover, by applying the invention, the average wind noise level can be reduced.
Further advantages, advantageous features and applications of the present invention will be apparent from the following description and the dependent claims.
BRIEF DESCRIPTION OF THE DRAWINGS The present invention is . now to be explained more closely by means of embodiments, which are disclosed as examples, and with reference to the attached drawings.
Figure 1 illustrates how vortex shedding arises behind a ground vehicle without any airflow control mecha- nisms,
Figures 2a-b show different views of a first type of ground vehicle, through which the operation principles of the invention are schematically illustrated,
Figure 3 shows an amplification surface in the form of a protruding plate according to one embodiment of the invention,
Figure 4 illustrates how the invention may be applied to a second type of ground vehicle,
Figures 5a-b show variations of a proposed air modulator ac- cording to a first embodiment of the invention,
Figures 6a-b show variations of proposed air modulator according to a second embodiment of the invention,
Figures 7a-b show variations of proposed air modulator according to a third embodiment of the invention, and Figures 8a-c exemplify different configurations of the arrays of openings according to embodiments of the inven- tion.
DESCRIPTION OF EMBODIMENTS OF THE INVENTION Figure 1 shows a ground vehicle 10 that travels in a forward direction DF. The vehicle 10 is not equipped with any airflow con- trol mechanisms. Therefore, due to the vehicle's 10 pronounced bluff-body shape, a relatively large amount of vortex shedding 16 arises behind the vehicle 10.
Figure 2a shows a side-view of a first type of ground vehicle 100 in the form of a truck. The vehicle 100 has a body with an outer surface including a general front surface 1 10, a bottom surface 115, a main upper surface 120, two side surfaces 130b (of which one appears in this view), and a rear surface 140. As can be seen in the figure 2a, the general front surface 1 10 extends also over an almost horizontal surface of the vehicle's cabin. Namely, in this specification, a transition from the general front surface 110 to the main upper surface 120 is defined to be at the front- most part of a horizontal vehicle top surface of substantial length. Thus, for trucks, the main upper surface 120 is normally delimited by the front and back edges of the vehicle's cargo space. However, as will be seen in figure 4, for other types of vehicles, other delimitations may be applicable.
The vehicle 100 is equipped with at least one airflow control system to modify an air flow F around the vehicle 100, such that when the vehicle 100 travels at a particular speed (and wind conditions) the drag on the vehicle 100 is lower than if the vehicle 100 had traveled at this speed (and wind conditions) without the system. The proposed system creates small-scale air vortices 150 adjacent to shear layers of the airflow F around the vehicle 100. This, in turn, weakens the strength of any of global vortex shedding behind the vehicle 100.
According to the invention, the airflow control system includes an air modulator and a control unit. Here, the airflow control sys- tern includes a plurality of air modulators 210a, 210b1 , 210b2, 210c, 210d1 , 210d2 (see figure 2b) and 21 Oe respectively and a common control unit 230. Of course, instead of the illustrated common control unit 230, a separate control unit for each air modulator is also conceivable.
Each air modulator 210a, 210b1 , 210b2, 210c, 210d1 , 210d2 and 21 Oe has an array of openings 215 that includes a number of slots or holes, i.e. one or more slots/holes. The dimensions and aspect ratios of these openings will be discussed in detail below with reference to figures 5a to 8c. Nevertheless, the openings are arranged next to one another along an essentially straight line.
The control unit 230 is adapted to control each air modulator 210a, 210b1 , 210,b2, 210c, 210d1 , 210d2 and 21 Oe to output os- dilating air from each opening in such a manner that air vortices 150 are created outside the openings. The air vortices 150, which have spin axes that in proximity to the openings are essentially parallel to the essentially straight line, are accomplished by repeatedly (either periodically or irregularly) pushing amounts of air from inside the air modulator out through the openings. Different embodiments of air modulators according to the invention will be described below with reference to figures 5a, 5b, 6a, 6b, 7a and 7b.
Preferably, each air modulator 210a, 210b1 , 210b2, 210c, 210d1 , 210d2 and 21 Oe is further arranged on the vehicle 100 with the essentially straight line of the respective array of openings 215 oriented essentially perpendicular to a forward driving direction DF of the vehicle 100. It is further preferable if the air modulators 210a, 21 ObI 1 210b2, 210c, 210d1 , 210d2 and 21 Oe are arranged on the vehicle 100, such that the openings of the respective air modulator are located downstream of a flow separation line FSL at which flow separation would occur if no synthetic air vortices 150 had been generated. Thus, in case of a vehicle 100 with sharp edges between the rear surface 140 and the side surfaces 130b, 13Od and/or between the rear surface 140 and the bottom surface 115 and/or between the rear surface 140 and the top surface 120; the air modulator openings are preferably positioned at the far back of the vehicle 100.
According to the. invention, by essentially perpendicular to the direction DF is meant a maximum deviation of 10 degrees from 90 degrees (i.e. from 80 degrees to 100 degrees). Consequently, the spin axes of the air vortices 150 are also (at least in proximity to the openings) essentially perpendicular to the direction DF. This is a key factor in the above-mentioned perturbation of the shear layers around the vehicle 100, which reduces the global vortices behind the vehicle 100.
Moreover, it is advantageous if one or more flow amplification surfaces 120, 160b, 160c, 16Od and 16Oe are provided further downstream of the each air modulator 210a, 210b1 , 210b2, 210c, 210d1 , 210d2 and 21 Oe respectively relative to the air flow F, which are adapted to augment the air vortices 150. For example, at the rear surface 140, protruding plates 160b, 160c, 16Od and 16Oe may constitute the amplification surfaces. Such protruding plates preferable have a profile that is slightly curved towards the rear surface 140. It is further advantageous if the plates are foldable, so that they do not protrude from the vehicle 100 when the airflow control system is inactive. Specific aspects of the protruding plates 160b, 160c, 16Od and 16Oe according to preferred embodiments of the invention will be discussed below with reference to figure 3.
In the example shown in the figure 2a, a first air modulator 210a is arranged essentially along an intersection line between the general front surface 1 10 and the main upper surface 140 (i.e. here at the front edge of the vehicle's 100 cargo space). Of course, the top surface 120 may serve as a flow amplification surface in respect of this air modulator 210a. Correspondingly the side surface 130b may serve as a flow amplification surface in respect of an air modulator 210b2 arranged vertically at the front edge of the vehicle's 100 cargo space.
The control unit 230 controls the operation of the modulator 210a by means of a first control signal CMa. Moreover, a second air modulator 210c is arranged essentially along an intersection line between the main upper surface 120 and the rear surface 140 (i.e. here at the back edge of the vehicle's 100 cargo space). The control unit'230 controls the operation of this modulator 210c by means of a second control signal CMc. Additionally, by means of a third control signal CMb, the control unit 230 controls the operation of a third and a fourth air modulator 210b and 21 Od (see figure 2b), which are arranged essentially along a first intersection line between a first side surface 130b and the rear surface 140, respective essentially along a second intersection line between a second side surface 13Od (see figure 2b) and the rear surface 140.
According to one embodiment of the invention, each air modulator 210a, 210b1 , 210b2, 210c, 210d1 , 210d2 and 21 Oe is arranged on the vehicle 100 with the array of openings 215 oriented, such that the openings thereof emit air in a main direc- tion A at an angle αj to the forward driving direction DF. Most preferably αj « 155 degrees. In other words, a complementary angle αjc between a main direction A of for example the first air modulator 210a and the (essentially horizontal) main upper surface 120 is most preferably around 25 degrees. However, according to the invention, the angle αj may lie anywhere in an interval from 90 degrees to 175 degrees (i.e. with a complementary angle αjc ranging from 5 degrees to 90 degrees).
Such a main direction A results in that the oscillating air vortices 150 interact very efficiently with the lateral shear layers of the air flow F behind the vehicle 100. For reasons of a clear presentation, this is here illustrated in a highly simplified manner by . means arrows 150 that represent the air vortices generated by the air modulators 210a and 210c adjoining the dashed arrow symbolizing the air flow F. In addition, or as alternatives, to the above-mentioned air modulators 21 Oa1 210b1 , 210b2, 210c, 2iθd1 , 210d2 and 21 Oe, air modulators may be positioned for example at the rear surfaces of the vehicle's 100 fender wings. These locations are sche- matically shown in the figure 2a by means of dashed circles 210. In fact, an air modulator can be arranged along each bodyline of the vehicle 100 where flow separation occurs. Hence, if the vehicle 100 has a protruding engine hood, air modulators may also be positioned proximate to any edges of this hood.
Turning now to figure 2b, which shows a top-view of the vehicle 100 in the figure 2a, we see that also the air modulators 210b1 , 210b2, 210d1 and 210d2 are oriented with their arrays of openings 215, such that the openings thereof emit air in a main direction A at the angle αj to the forward driving direction DF. Correspondingly, this main direction A results in that the oscillating air vortices 150 from the air modulators 210b1 , 210b2, 210d1 and 210d2 interact very efficiently with the vertical shear layers of the air flow F behind the vehicle 100.
Returning to the figure 2a, according to one embodiment of the invention, the control unit 230 receives a velocity signal V, which represents a speed of the vehicle 100. The control unit
230, in turn, controls one or more of the air modulators 210a,
210b1 , 210b2, 210c, 210d1 , 210d2, 21 Oe and 210 in response to the velocity signal V, such that a relatively high vehicle speed results in a comparatively high output air oscillation frequency, and vice versa, a relatively low vehicle speed results in a comparatively low output air oscillation frequency.
Moreover, the control unit 230 may control at least one air modulator 210a, 210b1 , 210b2, 210c, 210d1 , 210d2, 21 Oe and/ or 210 in response to the velocity signal V, such that a peak-to- peak amplitude of an air speed exiting from each opening depends on the vehicle speed. Preferably, the peak-to-peak amplitude is equivalent to approximately 0,5 time to approximately 10 times the vehicle speed, and more preferably, the peak-to-peak amplitude is equivalent to approximately 1 time to approximately 3 times the vehicle speed. The vehicle speed here represents the so-called freestream velocity, i.e. the speed at which the airflow F passes the vehicle 100.
According to one embodiment of the invention, a compressed air system 250 (which is normally included in the vehicle 100 for other purposes) is connected to at least one of the air modulators. In the example illustrated in the figure 2a, the compressed air system 250 is connected to the first air modulator 210a and the second air modulator 210c. Thus, an active airflow P is supplied to the arrays of openings 215 of these modulators 210a and 210c respectively. Thereby, the amount of energy added to the airflow F via these modulators can be increased to improve their influence on the reduction of the vortex shedding.
Figure 3 shows an amplification surface in the form of a protruding plate 160 according to one embodiment of the invention. We here presume that the plate 160 is mounted at a rear surface 140 of a vehicle 100, such as the truck in the figures 2a and 2b. The plate 160 protrudes from the rear surface 140 a dis- tance represented by an overall length Λ. Moreover, an air modulator 210 is arranged relative to the plate 160, such that an array of openings 215 of the modulator 210 is positioned a distance Λc from a flow separation line FSL adjacent to the surface 140. Thus, a remaining surface over which oscillating air vor- tices from the air modulator 210 may be amplified extends a distance XTE = Λ - ΛC from the array of openings 215. Preferably ΛG lies in an interval from 0 to 0,6OA, however, more preferably 0,05Λ < Λc < 0,30Λ.
In the figure 3, an arrow indicates a freestream velocity U rep- resenting the speed at which the vehicle 100 travels. According to this embodiment of the invention, a non-dimensional normalized frequency F+ is defined as:
Figure imgf000016_0001
where f represents the frequency at which the air modulator 210 produces oscillating air vortices. It is desirable that the non- dimensional normalized frequency F+ is larger than 0,05 and less than 30. More preferably 0, 1 < F+ < 1 ,0, and optimally F+ lies in an interval from 0,1 to 0,6.
Figure 4 shows a second type of ground vehicle 100 in the form of a bus. Also this vehicle 100 has a body with an outer surface that includes a general front surface 1 10, a main upper surface 120, two side surfaces 130b (of which one appears in this view), and a rear surface 140. Here, however, the general front surface 110 transitions into the main upper surface 120 relatively sharply, since in this case the horizontal vehicle top surface of substantial length begins almost immediately at front of the vehicle 100.
In similarity with the vehicle shown in the figures 2a and 2b, the vehicle 100 in the figure 4 is equipped with at least one airflow control system to modify an air flow F around the vehicle 100, such that when the vehicle 100 travels at a particular speed (and wind conditions) the drag on the vehicle 100 is lower than if the vehicle 100 had traveled at this speed (and wind conditions) without the system.
In this example, eight air modulators 210a1 , 210a2, 210b1 , 210b2, 210c and 21 Oe (plus two vertical modulators at the front and the rear on the vehicle's right-hand side, which are not visible in this view) are included in the airflow control system. Each air modulator has an array of openings 215 that includes a number of openings, which are arranged next to one another along an essentially straight line. A control unit (not shown) controls each air modulator 210a1 , 210a2, 210b1 , 210b2, 210c and 21 Oe to output oscillating air from each opening in such a manner that air vortices are created outside the openings. The air vortices, which have spin axes that in proximity to the openings are essentially parallel to the essentially straight line, are accomplished by repeatedly (either periodically or irregularly, continuously varying or burst wise) pushing amounts of air from inside the air modulator out through the openings. Preferably, the air modulators 210a1 , 210a2, 210b1 , 210b2, 210c and 21 Oe are arranged on the vehicle 100 with the essentially straight line of the respective array of openings 215 oriented essentially perpendicular to a forward driving direction of the vehicle 100, so that the spin axes of the air vortices 150 are also (at least in proximity to the openings) essentially perpendicular to this direction.
According to one embodiment of the invention, each air modulator 210a1 , 210a2, 21 ObI 1 210b2, 210c and 21 Oe is arranged on the vehicle 100 with the array of openings 215 oriented, such that the openings thereof emit air in a main direction A at an angle αj to the forward driving direction DF, where αj preferably is around 155 degrees and a complementary angle αjc between a main direction A of for example the first air modulator 210a and the main upper surface 120 is preferably around 25 degrees. However, as mentioned above, the angle αj may lie anywhere in an interval from 90 degrees to 175 degrees (i.e. with a complementary angle αjc ranging from 5 degrees to 90 degrees).
In similarity with the vehicle shown in the figures 2a and 2b, it is advantageous if the air modulators 210a1 , 210a2, 210b1 , 210b2, 210c and 21 Oe are arranged on the vehicle 100, such that the openings of the respective air modulator are located downstream of a flow separation line FSL at which flow separation would occur if no synthetic air vortices 150 had been generated. Here, the vehicle 100 has relatively rounded edges between the rear surface 140 and the side surfaces 1.30b, between the rear surface 140 and the bottom surface 115 and between the rear surface 140 and the top surface 120. Therefore, adequate flow amplification surfaces 120, 130b, 160b, 160c and 16Oe can be provided by portions of the vehicle's 100 body, namely said rounded edges. Naturally, an existing body shape may have to be modified to some extent in order to represent an optimal flow amplification surface. Nevertheless, these surfaces may be designed very discretely. Furthermore, the design may be complemented by one or more protruding plates, which can foldable, so that they do not protrude from the vehicle 100 when the airflow control system is inactive.
Figure 5a shows section of a proposed air modulator 210 accor- ding to a first embodiment of the invention. The air modulator
210 has a tubular element on which an array of openings is arranged. In the illustrated section of the air modulator 210 one exemplifying opening in the form of a slot 515 is included. This slot 515 has a width dimension W and a length L dimension, where the length dimension L is several factors larger than the width dimension W. Preferably, the width dimension W lies in a range from approximately 0, 1 mm to approximately 10 mm (more preferably, 0,3 mm < W < 2,0 mm), and the length dimension L lies in a range from approximately 30 mm to approximately 300 mm.
The tubular element includes a modulating member 520 that extends along a substantial portion of an interior of the tubular element. The modulating member 520 has a polygon shaped cross section, such a hexagon or a pentagon. However, any other re- gular or irregular cross section shape is conceivable according to the invention. Nevertheless, the modulating member 520 is rotatable around its symmetry axis 525 (or, if the cross section shape is irregular, center-of-gravity axis). Therefore, the cross section shape must allow the modulating member 520 to rotate freely within the tubular element of the air modulator 210.
A transmission line connects the modulating member 520 to a control unit 230 (see also figure 2a), such that this unit, by means of a control signal CM, may control the member 520 to produce a desired oscillating output of air. Specifically, these air oscillations are created when an amount of air located in a interspace between the modulating member 520 and the tubular element is pushed out through the slot 515'each time an edge of the element 520 passes the slot 515. Thus, a constant rotation speed and a regular cross section shape of the modulating member 520 causes equally large amounts of air to be emitted each time. However, a variation of the rotation speed results in a corresponding variation of the air oscillation frequency, and an irregular cross section shape of the modulating member 520 produces an air pulsation pattern which has a lower repetition rate than what is given by the distance between to consecutive edges of the modulating member 520. As will be described below with reference to figures 6b, 7a and 8b, the openings in the air modulator's 210 array of openings may also have non- slot shaped profiles, such as circular, oval, polygon etc.
According to one embodiment of the invention, the control unit 230 is adapted to control the air oscillating frequency of the air exiting from each slot 515 in a range from approximately 5 Hz to approximately 500 Hz. The most desirable range is 10 - 60 Hz. It is further preferable if the oscillating frequency depends on a current vehicle speed. Therefore, as mentioned above, the control unit 230 may receive a velocity signal V representing a speed of the vehicle, in response thereto, control the modulating member 520, such that a relatively high vehicle speed results in a comparatively high output air oscillation frequency, and vice versa, a relatively low vehicle speed results in a comparatively low output air oscillation frequency.
Figure 6a shows a section of a proposed air modulator 210 according to a second embodiment of the invention. Here, the air modulator 210 includes at least one diaphragm 620, which is arranged in a cavity 625 adjoining at least one opening in the above-mentioned array of openings. Preferably, corresponding cavities and diaphragms are arranged behind each opening (here in the form of slots 615) in the air modulator's 210 array of openings. Nevertheless, in case the openings are slots, each slot 615 has a width dimension W and a length L dimension, where the length dimension L is several factors larger than the width dimension W. Preferably, the width dimension W lies in a range from approximately 0, 1 mm to approximately 10 mm (more preferably 0,3-2,0 mm), and the length dimension L lies in a range from approximately 30 mm to approximately 300 mm. Moreover, as can be seen in the figure 6a, all the slots 615 in the array of openings are positioned next to one another along an essentially straight line 630, which is parallel to each slot's 615 length dimension L.
The air modulator 210 is connected to a control unit 230, and the diaphragm 620 is adapted to vibrate in response to a control signal CM from the control unit 230, so as to produce the os- cillating output of air. In similarity with the embodiment of the invention described above with reference to the figure 5a, the control signal CM may in turn be correlated with a velocity signal V representing a speed of the vehicle onto which the air modulator 210 is mounted.
Figure 5b shows a section of the air modulator 210 according to the above-described first embodiment of the invention, however where the tubular element is connected to a compressed air system 250 via an air conduit. Thus, via this conduit, an active airflow P is supplied to the tubular element. Such an active air- flow P enables a net amount of air to added the airflow that surrounds a vehicle, and thus accomplished an enhancement of the performance of the proposed airflow control system.
According to one embodiment of the invention, the control unit 230 receives a velocity signal V, which represents a speed of the vehicle onto which the air modulator 210 is mounted. The control unit 230 then controls the air modulator 210 in response to the velocity signal V, such that a peak-to-peak amplitude of a speed of the air exiting from each opening 515 is equivalent to approximately 0,5 time to approximately 10 times the speed. Figure 6b shows the air modulator 210 according to the above- described second embodiment of the invention, however where the openings 715 in the array of openings are holes, i.e. apertures with an approximately equal opening dimension D in all directions. Hence, the openings 715 may have a circular, oval or polygon shape. Preferably, the opening dimension D lies in a range from approximately 0,1 mm to approximately 10 mm, or more preferably 0,3 mm - 2,0 mm. Moreover; an air conduit connects the cavity 625 to a compressed air system 250. Thus, analogous to the embodiment described above with reference to the figure 5b, an active airflow P is accomplished.
Figure 7a shows a section of the air modulator 210 according to a third embodiment of the invention, wherein an array of openings 215 contains a number of openings 715 arranged next to one another along an essentially straight line 530. Here, the air modulator 210 is represented by a set of valves 710, 720, 730 and 740 respectively. Namely, each opening 715 is connected to an air conduit, which is further connected to one of the valves 710, 720, 730 and 740. Each of these valves, in turn, 710, 720, 730 and 740 is connected to a compressed air system 250 via one or more further air conduits, so that an active airflow P can be received. Each valve 710, 720, 730 and 740 is controllable by a control unit 230 in response to a control signal CM. Thereby, the openings 715 may be controlled to emit synthetic air vortices according to what has been described above.
Figure 7b shows a section of the air modulator 210 according to the third embodiment of the invention, however, where a sub-set of openings 615 are connected to a common air chamber 71 1 , 721 , 731 and 741 respectively. A respective valve 710, 720, 730 and 740 controls an active airflow P to each air chamber 71 1 , 721 , 731 and 741 . The valves 710, 720, 730 and 740 are, in turn, are controlled in response to a control signal CM from a control unit 230. The active airflow P is fed to the valves 710, 720, 730 and 740 from a compressed air system 250 via one or more air conduits. Hence, the control unit 230 may control the openings 615 to emit synthetic air vortices according to what has been described above.
Naturally, instead of having valves that are common for more than one opening as shown in the figures 7a and 7b, a separate valve may equally well be employed to control the airflow from each opening.
According to another preferred embodiment of the invention, an active air flow P may be supplied to the openings of the air modulator 210 alternately either from a first air system providing air at a pressure such that air flows out of the air modulator openings, or from a second air system providing air at a pressure such that air is sucked in through the air modulator openings. Thereby, the active air flow P may be controlled so that its average pressure level attains a desired value.
Finally, we now refer to figures 8a, 8b and 8c in order to underline the fact that, according to the invention, a large number of different configurations of the slot array 215 are conceivable.
Figure 8a illustrates an array of openings 215 where a number of slot shaped openings 615, e.g. six, are arranged next to one another along an at least essentially straight line 630, which is parallel to each slot's 615 length dimension L. Here, the length sides of the slots 615 form the essentially straight line 630.
Figure 8b illustrates another array of openings 215 where a number of openings in the form of holes 715 are arranged next to one another along an at least essentially straight line 630. In this case, however, only few of the holes 715 actually lie on this line 630. The remaining holes 715 are slightly displaced with respect to the essentially straight line 630.
Figure 8c illustrates yet another slot array 215 where a number of openings in the form of slots 615 are arranged next to one another along an at least essentially straight line 630, which is parallel to each slot's 615 length dimension L. Here, some of the slots 615 are slightly displaced with respect to the essentially straight line 630, whereas the length sides of other slots 615 are aligned with this line 630.
Naturally, many different opening configurations in addition to the above-described configurations may also be applied according to the invention, for instance configurations where at least one extended opening (e.g. slot shaped) is slightly angled in relation to the essentially straight line 630.
Irrespective of how the openings are arranged relative to one another, it is preferable if the openings are physically protected when they are not in use, i.e. when the vehicle is stationary, or travels below a threshold speed. In order to accomplish this, protective shields may be provided, which are controllable in response to a velocity signal that represents the speed of the vehicle, so that the shields either cover or expose the openings to the exterior depending on a current vehicle speed.
The term "comprises/comprising" when used in this specification is taken to specify the presence of stated features, integers, steps or components. However, the term does not preclude the presence or addition of one or more additional features, integers, steps or components or groups thereof.
The invention is not restricted to the described embodiments in the figures, but may be varied freely within the scope of the claims.

Claims

Claims
1 . An airflow control system for assembly on a ground vehicle (100) in order to modify an air flow (F) around the vehicle (100), such that when the vehicle (100) travels at a particular speed the drag on the vehicle (100) is lower than if the vehicle (100) had traveled at this speed without the system, characterized in that the system comprises: an air modulator (210) having an array of openings (215) including a number of openings (515, 615, 715) which are arran- ged next to one another along an essentially straight line (630); and a control unit (230) adapted to control the air modulator (210) to output oscillating air from each opening (515, 615, 715) such that air vortices (150) are created outside the opening (515, 615, 715), where the air vortices (150) have spin axes that in proximity to the opening (515, 615, 715) are essentially parallel to the essentially straight line (630).
2. The airflow control system according to claim 1 , characterized in that the array of openings (215) includes a number of slots (515, 615), each slot having a width (W) and a length (L) dimension where the length dimension (L) is several factors larger than the width dimension (W), the slots (515, 615) are arranged next to one another along an essentially straight line (630) parallel to each slot's length dimension (L).
3. The airflow control system according to claim 2, characterized in that the slot width dimension (W) lies in an interval from approximately 0,1 mm to approximately 10 mm.
4. The airflow control system according to any one of the claims 2 or 3, characterized in that the slot length dimension (L) lies in an interval from approximately 30 mm to approximately 300 mm.
5. The airflow control system according to claim 1 , characterized in that the array of openings (215) includes a number of holes (715), each hole (715) having an opening dimension (D) in an interval from approximately 0,1 mm to approximately 10 mm.
6. The airflow control system according to any one or the preceding claims, characterized in that the air modulator (210) comprises a tubular element on which the array of openings (215) is arranged, the tubular element including a modulating member (520) extending along a substantial portion of an inte- rior of the tubular element, the modulating member (520) has a polygon shaped cross section, and the modulating member (520) is rotatable around its symmetry axis (525) in response to a control signal (CM) from the control unit (230) so as to produce the oscillating output of air.
7. The airflow control system according to any one or the claims 1 - 5, characterized in that the air modulator (210) comprises at least one diaphragm (620) arranged in a cavity (625) adjoining at least one of the openings (615) in the array of openings (215), each of the least one diaphragm (620) is adapted to vibrate in response to a control signal (CM) from the control unit (230) so as to produce the oscillating output of air.
8. The airflow control system according to any one or the claims 1 - 5, characterized in that the air modulator (210) comprises at least one valve (710, 720, 730, 740) arranged to emit an active airflow (P) from a compressed air system (250) in response to a control signal (CM) from the control unit (230) so as to produce the oscillating output of air.
9. The airflow control system according to any one of the preceding claims, characterized in that the control unit (230) is adapted to control an air oscillating frequency of the air exiting from the array of openings (215) in a range from approximately 5 Hz to approximately 500 Hz.
10. A ground vehicle (100) having a body with an outer surface comprising a general front surface (110), a main upper surface (120), a bottom surface (1 15), two side surfaces (130a; 130b) and a rear surface (140), characterized in that the vehicle (100) comprises at least one airflow control system according to any one of the claims 1 - 8, where the air modulator (210) of each of the at least one system is arranged on the vehicle (100) with the array of openings (215) having such an orientation rela- tive to the outer surface that when the vehicle (100) travels at a particular speed an amount of vortex shedding behind the rear surface (140) is lower than if the vehicle (100) had traveled at this speed without the at least one system.
11. The ground vehicle (100) according to claim 10, characteri- zed in that one of the at least one airflow control system has its air modulator (210c) arranged essentially along an intersection line between the main upper surface (120) and the rear surface (140).
12. The ground vehicle according to any one of the claims 10 or 1 1 , characterized in that one of the at least one airflow control system has its air modulator (210a) arranged essentially along an intersection line between the general front surface (110) and the main upper surface (140).
13. The ground vehicle (100) according to any one of the claims 10 - 1 1 , characterized in that the vehicle (100) compri- ses at least two airflow control systems of which a first system has its air modulator (210b1 ) arranged essentially along a first intersection line between a first side (130b) of the side surfaces and the rear surface (140), and a second system has its air modulator (210d1) arranged essentially along a second intersection line between a second side (13Od) of the side surfaces and the rear surface (140).
14. The ground vehicle (100) according to any one of the claims 10 - 13, characterized in that each of the at least one airflow control system has its air modulator (210, 210a, 210b1 , 210b2, 210c, 210d1 , 210d2, 21 Oe) arranged on the vehicle (100) with the essentially straight line (630) of the respective array of openings (215) oriented essentially perpendicular to a forward driving direction (DF) of the vehicle (100).
15. The ground vehicle (100) according to claim 14, characterized in that each of the at least one airflow control system has its air modulator (210, 210a, 210b1 , 210b2, 210c, 210d1 , 210d2, 21 Oe) arranged on the vehicle (100) with the array of openings (215) oriented such that each opening (515, 615, 715) emits air in a main direction (A) having an angle (ocj) to the forward driving direction (DF) in an interval from approximately 90 degrees to approximately 175 degrees.
16. The ground vehicle (100) according to any one of the claims 10 - 15, characterized in that the control unit (230) is adapted to: receive a velocity signal (V) representing a speed of the vehicle (100); and control the air modulator (210) in response to the velocity signal (V), such that a relatively high vehicle speed results in a comparatively high output air oscillation frequency and a relatively low vehicle speed results in a comparatively low output air oscillation frequency.
17. The ground vehicle (100) according to any one of the claims 10 - 16, characterized in that the control unit (230) is adapted to: receive a velocity signal (V) representing a speed of the vehicle (100); and control the air modulator (210) in response to the velocity signal (V), such that a peak-to-peak amplitude of a speed of the air exiting from each opening (515, 615, 715) is equivalent to approximately 0,5 time to approximately 10 times the speed.
18. The ground vehicle (100) according to any one of the claims 10 - 17, characterized in that the vehicle (100) compri- ses a compressed air system (250) which is connected to the air modulator (210) of at least one of the at least one air flow control system for supply of an active air flow (P) to the array of openings (215).
19. The ground vehicle (100) according to any one of the claims 10 - 18, characterized in that the vehicle (100) comprises at least one flow amplification surface (120, 130b, 160, 160b, 160c, 16Od, 16Oe) which is arranged on the vehicle (100) downstream of at least one of the at least one air modulator (210, 210a, 210b1 , 210b2, 210c, 210d1 , 210d2, 21 Oe) relative to the air flow (F), and the at least one flow amplification surface (120, 130b, 160, 160b, 160c, 16Od, 16Oe) is adapted to augment the air vortices (150).
PCT/SE2006/000031 2005-01-27 2006-01-09 Improvement of the aerodynamic properties of ground vehicles WO2006080873A1 (en)

Priority Applications (5)

Application Number Priority Date Filing Date Title
EP06700063A EP1841639B1 (en) 2005-01-27 2006-01-09 Improvement of the aerodynamic properties of ground vehicles
AT06700063T ATE485994T1 (en) 2005-01-27 2006-01-09 IMPROVING THE AERODYNAMIC CHARACTERISTICS OF GROUND VEHICLES
US11/813,188 US7794011B2 (en) 2005-01-27 2006-01-09 Aerodynamic properties of ground vehicles
DE602006017799T DE602006017799D1 (en) 2005-01-27 2006-01-09 IMPROVEMENT OF AERODYNAMIC PROPERTIES OF FLOOR VEHICLES
US12/853,975 US20110031777A1 (en) 2005-01-27 2010-08-10 Aerodynamic properties of ground vehicles

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
SE0500206-8 2005-01-27
SE0500206A SE528351C2 (en) 2005-01-27 2005-01-27 Improvements in the aerodynamic characteristics of land vehicles

Related Child Applications (1)

Application Number Title Priority Date Filing Date
US12/853,975 Continuation US20110031777A1 (en) 2005-01-27 2010-08-10 Aerodynamic properties of ground vehicles

Publications (1)

Publication Number Publication Date
WO2006080873A1 true WO2006080873A1 (en) 2006-08-03

Family

ID=36740796

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/SE2006/000031 WO2006080873A1 (en) 2005-01-27 2006-01-09 Improvement of the aerodynamic properties of ground vehicles

Country Status (6)

Country Link
US (2) US7794011B2 (en)
EP (2) EP1841639B1 (en)
AT (1) ATE485994T1 (en)
DE (1) DE602006017799D1 (en)
SE (1) SE528351C2 (en)
WO (1) WO2006080873A1 (en)

Cited By (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2008135968A1 (en) * 2007-05-02 2008-11-13 Ramot At Tel Aviv University Ltd. Methods and apparatus for reduction of aerodynamic drag
WO2009116932A1 (en) * 2008-03-17 2009-09-24 Semcon Caran Ab Improvement of the aerodynamic properties of ground vehicles
FR2946951A1 (en) * 2009-06-23 2010-12-24 Renault Sas BODY COMPONENT OF MOTOR VEHICLE WITH AIR BLOWING.
WO2011153185A2 (en) * 2010-06-01 2011-12-08 Henderson Industries, Llc Devices and methods for reducing vehicle drag
WO2012051134A2 (en) * 2010-10-15 2012-04-19 Henderson Industries, Llc Devices and methods for reducing vehicle drag
US8342595B2 (en) 2010-05-06 2013-01-01 SmartTruckSystems, LLC Devices and methods for reducing vehicle drag
FR2980155A1 (en) * 2011-09-19 2013-03-22 Bruno Sagnier Rotary aerodynamic device for vehicle e.g. lorry, has cylinder rotating under action of force of air moved by displacement of vehicle, so that air is circularly moved towards rear of vehicle for reducing suction cone and aerodynamic drag
WO2014076517A1 (en) * 2012-11-13 2014-05-22 Renault Trucks Aerodynamic system for a vehicle, vehicle equipped with such an aerodynamic system, and method for reducing a vehicle drag
WO2015087104A1 (en) * 2013-12-11 2015-06-18 Renault Trucks Aerodynamic system for a vehicle, vehicle equipped with such an aerodynamic system, and method for reducing a vehicle drag

Families Citing this family (20)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7618086B2 (en) 2005-12-01 2009-11-17 Thomas Scott Breidenbach Aerodynamic drag reducing apparatus
US8360509B2 (en) 2007-05-17 2013-01-29 Advanced Transit Dynamics, Inc. Rear-mounted aerodynamic structure for truck cargo bodies
US8100461B2 (en) 2007-05-17 2012-01-24 Advanced Transit Dynamics, Inc. Rear-mounted aerodynamic structure for truck cargo bodies
US8133293B2 (en) * 2009-03-06 2012-03-13 Paccar Inc Air cleaner boattail
WO2013043890A1 (en) 2011-09-20 2013-03-28 Advanced Transit Dynamics, Inc. Rear-mounted retractable aerodynamic structure for cargo bodies
US9440689B1 (en) 2011-09-20 2016-09-13 Stemco Lp Aerodynamic structures secured to the underbody of cargo bodies
US9873466B2 (en) * 2011-09-23 2018-01-23 Aero Industries, Inc. Drag reducing device
EP2771239A4 (en) * 2011-10-27 2015-12-09 Univ Ramot Synchronization of fluidic actuators
WO2013063479A1 (en) 2011-10-27 2013-05-02 Advanced Transit Dynamics, Inc. Rear-mounted aerodynamic structures for cargo bodies
US8770649B2 (en) 2011-10-29 2014-07-08 Alexander Praskovsky Device, assembly, and system for reducing aerodynamic drag
DE102011120971A1 (en) 2011-12-13 2013-06-13 Daimler Ag Omni bus has chassis/framework having flexible, changeable skin which is movable between retracted design position and bus extended position is based on speed of bus for adjusting aerodynamics of bus
EP2872378A1 (en) 2012-07-11 2015-05-20 Advanced Transit Dynamics, Inc. Retractable aerodynamic structures for cargo bodies and methods of controlling positioning of the same
JP6184103B2 (en) * 2013-01-19 2017-08-23 本田技研工業株式会社 Saddle riding
WO2015017678A2 (en) 2013-07-31 2015-02-05 Ridge Corporation Device for reducing vehicle aerodynamic resistance
SE538160C2 (en) 2014-02-07 2016-03-22 Creo Dynamics Ab Trailers and side skirts provided with arrangements for reducing air resistance
DE102015102741A1 (en) * 2015-02-26 2016-09-01 Dr. Ing. H.C. F. Porsche Aktiengesellschaft Air guiding device and method for operating the same
GB2536214B (en) * 2015-03-05 2020-05-27 Elogab O Engine system and method of generating electricity from an internal combustion engine
US12005969B2 (en) 2016-04-07 2024-06-11 Fleetaero, Llc Vehicle aerodynamic improvement apparatus and system
CN110282034A (en) * 2019-07-29 2019-09-27 北京航空航天大学 Improve the shipping car air force damping device in flow field using jet stream
CN111959620A (en) * 2020-07-23 2020-11-20 南昌大学 A anti side air current interference device of bionical fin structure for passenger train

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4455045A (en) * 1981-10-26 1984-06-19 Wheeler Gary O Means for maintaining attached flow of a flowing medium
US4671474A (en) * 1984-06-21 1987-06-09 The Boeing Company Fluid control apparatus and method utilizing cellular array containing mini-vortex flow patterns
US5374013A (en) 1991-06-07 1994-12-20 Bassett; David A. Method and apparatus for reducing drag on a moving body
US5407245A (en) 1988-11-07 1995-04-18 Daimler-Benz Ag Process and device for reducing the drag in the rear region of a vehicle, for example, a road or rail vehicle or the like
US5908217A (en) 1995-07-17 1999-06-01 Georgia Tech Research Corporation Pneumatic aerodynamic control and drag-reduction system for ground vehicles

Family Cites Families (54)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US925141A (en) * 1907-11-23 1909-06-15 Albert E Smith Dust-guard.
US926971A (en) * 1908-10-17 1909-07-06 George A Ahrens Means for reducing air resistance on vehicles.
US1580577A (en) * 1923-11-26 1926-04-13 Baumann Ernst Karl Alexander Aeroplane
US1871396A (en) * 1928-06-08 1932-08-09 Edward A Stalker Means of reducing the fluid resistance of automobile bodies
US1903818A (en) * 1932-03-02 1933-04-18 Bernhard G Jutting Wing lift system for aircraft
US2037942A (en) * 1935-10-28 1936-04-21 Edward A Stalker Means of reducing the fluid resistance of propelled vehicles
GB616163A (en) * 1943-01-19 1949-01-18 Groupement Francais Pour Le Developpement Des Recherches Aeronautiques Means for avoid separation and turbulence in fluids moving with respect to solid surfaces
US2514695A (en) * 1948-12-31 1950-07-11 Edwin A Dempsey Vehicle body and attachment therefor
US2894703A (en) * 1954-05-27 1959-07-14 Research Corp Boundary layer control system
US2844337A (en) * 1956-11-23 1958-07-22 North American Aviation Inc Aircraft control arrangement incorporating deflectable surface and boundary layer control jets
US3062483A (en) * 1958-09-17 1962-11-06 Power Jets Res & Dev Ltd Aerofoil boundary layer control systems
US2973922A (en) * 1959-04-10 1961-03-07 Power Jets Res & Dev Ltd Jet propelled aircraft
US3410510A (en) * 1963-12-23 1968-11-12 Papst Hermann Boundary layer control
US3374971A (en) * 1965-08-02 1968-03-26 American Standard Inc Fluid dynamic drag reduction
FR1512563A (en) * 1966-12-29 1968-02-09 Renault Device for reducing the resistance to advancement of motor vehicles
US3999797A (en) * 1974-04-01 1976-12-28 Systems, Science And Software Airvane device for bluff vehicles and the like
US4057280A (en) * 1974-09-05 1977-11-08 Aerovironment Inc. Aerodynamic drag reduction devices for surface vehicles
JPS5241490B2 (en) * 1974-10-18 1977-10-19
US3934923A (en) * 1975-03-07 1976-01-27 Aerovironment Inc. Air decelerator for truck cab
US4006932A (en) * 1975-07-21 1977-02-08 The United States Of America As Represented By The Secretary Of The Department Of Transportation Inflatable drag reducer for land vehicles
US4113299A (en) * 1976-10-04 1978-09-12 Johnson David W Rotating magnus tubes
US4320920A (en) * 1980-05-09 1982-03-23 Goudey Robert B Air deflector duct
US4343506A (en) * 1980-08-05 1982-08-10 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Low-drag ground vehicle particularly suited for use in safely transporting livestock
US4502724A (en) * 1980-10-16 1985-03-05 Grenadier R Miles Vehicle payload lightener
US4437698A (en) * 1982-08-09 1984-03-20 Tantalo Anthony T Fuel saving device for increasing fuel mileage on a moving vehicle
GB2188397B (en) * 1984-09-13 1988-12-29 Rolls Royce A low drag surface construction
JP2658718B2 (en) * 1992-02-20 1997-09-30 三菱自動車工業株式会社 Structure to reduce the amount of mud deposited on the back of van type vehicles
FR2695097A1 (en) * 1992-08-31 1994-03-04 Bonnotte Michel Vehicle having arrangement for reduction of ambient frictional resistance to forward movement - arrangement includes reducing compression of ambient fluid such as air or water by moving belts or ducts modifying speed relative to surroundings
US5758823A (en) * 1995-06-12 1998-06-02 Georgia Tech Research Corporation Synthetic jet actuator and applications thereof
US5813625A (en) * 1996-10-09 1998-09-29 Mcdonnell Douglas Helicopter Company Active blowing system for rotorcraft vortex interaction noise reduction
US6186412B1 (en) * 1998-10-05 2001-02-13 Ramot University Authority For Applied Research And Industrial Development Generating dynamically controllable oscillatory fluid flow
DE19912140C2 (en) * 1999-03-18 2001-04-26 Daimler Chrysler Ag Motor vehicle with flow influencing means for reducing the air resistance
CA2300714A1 (en) * 2000-03-10 2001-09-10 James C. Hayes Vertical wings on fluid vehicule with stabilizing torque system of jets to utilize fluid energy for forward motion, that is, sailing in fluid like air or water
US6742616B2 (en) * 2000-06-20 2004-06-01 Michael F. Leban Hybrid air boost vehicle and method for making same
AU2002255688A1 (en) * 2001-03-10 2002-09-24 Georgia Tech Research Corporation Modification of fluid flow about bodies and surfaces through virtual aero-shaping of airfoils with synthetic jet actuators
FR2858794B1 (en) 2003-08-13 2006-12-01 Peugeot Citroen Automobiles Sa SYSTEM FOR REDUCING AERODYNAMIC EFFORTS OF A MOTOR VEHICLE AND MOTOR VEHICLE EQUIPPED WITH SUCH A SYSTEM
ITTO20031019A1 (en) 2003-12-18 2005-06-19 Fiat Ricerche MOTOR VEHICLE WITH AERODYNAMIC FLOW CONTROL DEVICE USING SYNTHETIC JETS.
US20080008771A1 (en) * 2004-05-27 2008-01-10 Children's Hospital Medical Center Nitric Oxide Dioxygenase Inhibitors
US7255309B2 (en) * 2004-07-14 2007-08-14 The Boeing Company Vernier active flow control effector
US7510149B2 (en) * 2004-08-02 2009-03-31 Lockheed Martin Corporation System and method to control flowfield vortices with micro-jet arrays
US7537182B2 (en) * 2004-09-23 2009-05-26 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Simultaneous multiple-location separation control
US9908617B2 (en) * 2005-07-25 2018-03-06 The Boeing Company Active flow control for transonic flight
US7967258B2 (en) * 2005-10-06 2011-06-28 Lockheed Martin Corporation Dual bimorph synthetic pulsator
US8007030B2 (en) * 2006-01-30 2011-08-30 Richard Wood Frame extension device for reducing the aerodynamic drag of ground vehicles
WO2007090146A1 (en) * 2006-01-31 2007-08-09 Alcoa Inc. Vortex generator
US7874525B2 (en) * 2006-05-04 2011-01-25 Lockheed Martin Corporation Method and system for fully fixed vehicle control surfaces
US7748664B2 (en) * 2006-08-23 2010-07-06 Lockheed Martin Corporation High performance synthetic valve/pulsator
US7641262B2 (en) * 2006-10-19 2010-01-05 Nusbaum Howard G Retractable air deflection apparatus for reduction of vehicular air drag
US7980516B2 (en) * 2006-12-20 2011-07-19 The Boeing Company Ultra-low friction air pump for creating oscillatory or pulsed jets
US7625034B1 (en) * 2008-04-04 2009-12-01 Fitzgerald James P Cargo vehicle with drag reduction
US8091951B1 (en) * 2008-04-04 2012-01-10 Fitzgerald James P Cargo vehicle with drag reduction
US20110095564A1 (en) * 2009-10-23 2011-04-28 Chen Shih Hsiung Nozzle-typed drag-reducing structure for vehicle
US8336828B2 (en) * 2009-11-12 2012-12-25 The Boeing Company Traversing jet actuator
US8561935B2 (en) * 2010-09-17 2013-10-22 Karl F. Milde, Jr. STOL and/or VTOL aircraft

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4455045A (en) * 1981-10-26 1984-06-19 Wheeler Gary O Means for maintaining attached flow of a flowing medium
US4671474A (en) * 1984-06-21 1987-06-09 The Boeing Company Fluid control apparatus and method utilizing cellular array containing mini-vortex flow patterns
US5407245A (en) 1988-11-07 1995-04-18 Daimler-Benz Ag Process and device for reducing the drag in the rear region of a vehicle, for example, a road or rail vehicle or the like
US5374013A (en) 1991-06-07 1994-12-20 Bassett; David A. Method and apparatus for reducing drag on a moving body
US5908217A (en) 1995-07-17 1999-06-01 Georgia Tech Research Corporation Pneumatic aerodynamic control and drag-reduction system for ground vehicles

Cited By (21)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2008135968A1 (en) * 2007-05-02 2008-11-13 Ramot At Tel Aviv University Ltd. Methods and apparatus for reduction of aerodynamic drag
US9193398B2 (en) 2007-05-02 2015-11-24 Ramot At Tel-Aviv University Ltd. Methods and apparatus for reduction of aerodynamic drag
US8616615B2 (en) 2007-05-02 2013-12-31 Ramot At Tel-Aviv University Ltd. Methods and apparatus for reduction of aerodynamic drag
US8550120B2 (en) 2007-05-02 2013-10-08 Ramot At Tel-Aviv University Ltd. Apparatus and method for oscillating fluid jets
WO2009116932A1 (en) * 2008-03-17 2009-09-24 Semcon Caran Ab Improvement of the aerodynamic properties of ground vehicles
FR2946951A1 (en) * 2009-06-23 2010-12-24 Renault Sas BODY COMPONENT OF MOTOR VEHICLE WITH AIR BLOWING.
EP2266867A1 (en) * 2009-06-23 2010-12-29 Renault S.A.S. Vehicle body element having air blowing apparatus
US8251436B2 (en) 2010-05-06 2012-08-28 Henderson Industries, Llc Devices and methods for reducing vehicle drag
US9056636B2 (en) 2010-05-06 2015-06-16 Smarttruck Systems, Llc Devices and methods for reducing vehicle drag
US8342595B2 (en) 2010-05-06 2013-01-01 SmartTruckSystems, LLC Devices and methods for reducing vehicle drag
US8491036B2 (en) 2010-05-06 2013-07-23 Smarttruck Systems, Llc Devices and methods for reducing vehicle drag
US8684447B2 (en) 2010-05-06 2014-04-01 SmartTruck Systems, Inc. Devices and methods for reducing vehicle drag
US8783757B2 (en) 2010-05-06 2014-07-22 Smarttruck Systems, Llc Devices and methods for reducing vehicle drag
WO2011153185A3 (en) * 2010-06-01 2012-04-05 Henderson Industries, Llc Devices and methods for reducing vehicle drag
WO2011153185A2 (en) * 2010-06-01 2011-12-08 Henderson Industries, Llc Devices and methods for reducing vehicle drag
AU2011261579B2 (en) * 2010-06-01 2014-09-04 Transtex Llc Devices and methods for reducing vehicle drag
WO2012051134A3 (en) * 2010-10-15 2012-07-19 Henderson Industries, Llc Devices and methods for reducing vehicle drag
WO2012051134A2 (en) * 2010-10-15 2012-04-19 Henderson Industries, Llc Devices and methods for reducing vehicle drag
FR2980155A1 (en) * 2011-09-19 2013-03-22 Bruno Sagnier Rotary aerodynamic device for vehicle e.g. lorry, has cylinder rotating under action of force of air moved by displacement of vehicle, so that air is circularly moved towards rear of vehicle for reducing suction cone and aerodynamic drag
WO2014076517A1 (en) * 2012-11-13 2014-05-22 Renault Trucks Aerodynamic system for a vehicle, vehicle equipped with such an aerodynamic system, and method for reducing a vehicle drag
WO2015087104A1 (en) * 2013-12-11 2015-06-18 Renault Trucks Aerodynamic system for a vehicle, vehicle equipped with such an aerodynamic system, and method for reducing a vehicle drag

Also Published As

Publication number Publication date
DE602006017799D1 (en) 2010-12-09
EP2258607A1 (en) 2010-12-08
SE528351C2 (en) 2006-10-24
US20110031777A1 (en) 2011-02-10
EP1841639B1 (en) 2010-10-27
US7794011B2 (en) 2010-09-14
ATE485994T1 (en) 2010-11-15
US20090146452A1 (en) 2009-06-11
EP1841639A1 (en) 2007-10-10
SE0500206L (en) 2006-07-28

Similar Documents

Publication Publication Date Title
US7794011B2 (en) Aerodynamic properties of ground vehicles
US9193398B2 (en) Methods and apparatus for reduction of aerodynamic drag
US7922235B1 (en) Drag reduction system for vehicles
US7255387B2 (en) Vortex strake device and method for reducing the aerodynamic drag of ground vehicles
US20070235590A1 (en) Vortex generator
US20110148142A1 (en) Rear aerodynamic device for a vehicle and vehicle equipped with such a device
US5863090A (en) Pneumatic aerodynamic force-augmentation, control and drag-reduction devices for racing cars and high-performance sports cars
US20050040637A1 (en) Undercarriage flow control device and method for reducing the aerodynamic drag of ground vehicles
US20060103167A1 (en) Systems and methods for reducing the aerodynamic drag on vehicles
US20060232102A1 (en) Truck streamlining
WO2009116932A1 (en) Improvement of the aerodynamic properties of ground vehicles
US5340190A (en) Air-flow management device
CN113226899A (en) Improved system for aerodynamic aspects of a land vehicle, in particular a truck or the like
US11142260B2 (en) Flow restricting deflector
EP2607214A1 (en) Ground vehicle with aerodynamical oscillator
JP2002308154A (en) Front lower structure for vehicle
WO2014076517A1 (en) Aerodynamic system for a vehicle, vehicle equipped with such an aerodynamic system, and method for reducing a vehicle drag
US20140076419A1 (en) Self adjusting deturbulator enhanced flap and wind deflector
EP0932542B1 (en) Pneumatic aerodynamic control for cars
AU2007275575B2 (en) Wide area base bleed/injection apparatus for reducing aerodynamic drag of bluff body vehicles
WO2015087104A1 (en) Aerodynamic system for a vehicle, vehicle equipped with such an aerodynamic system, and method for reducing a vehicle drag
RU2270125C2 (en) Road vehicle body (versions)
JP2023069384A (en) Undercover for vehicle
KR20080055137A (en) Rear spoiler for automobile
CN118475508A (en) Vehicle aerodynamics

Legal Events

Date Code Title Description
121 Ep: the epo has been informed by wipo that ep was designated in this application
WWE Wipo information: entry into national phase

Ref document number: 2006700063

Country of ref document: EP

WWE Wipo information: entry into national phase

Ref document number: 2491/KOLNP/2007

Country of ref document: IN

WWP Wipo information: published in national office

Ref document number: 2006700063

Country of ref document: EP

WWE Wipo information: entry into national phase

Ref document number: 11813188

Country of ref document: US