Classifications

• • B—PERFORMING OPERATIONS; TRANSPORTING
  • B64—AIRCRAFT; AVIATION; COSMONAUTICS
  • B64B—LIGHTER-THAN AIR AIRCRAFT
  • B64B1/00—Lighter-than-air aircraft
  • B64B1/40—Balloons
  • B64B1/42—Construction or attachment of stabilising surfaces
• • B—PERFORMING OPERATIONS; TRANSPORTING
  • B64—AIRCRAFT; AVIATION; COSMONAUTICS
  • B64C—AEROPLANES; HELICOPTERS
  • B64C21/00—Influencing air flow over aircraft surfaces by affecting boundary layer flow
  • B64C21/10—Influencing air flow over aircraft surfaces by affecting boundary layer flow using other surface properties, e.g. roughness
• • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
  • F15—FLUID-PRESSURE ACTUATORS; HYDRAULICS OR PNEUMATICS IN GENERAL
  • F15D—FLUID DYNAMICS, i.e. METHODS OR MEANS FOR INFLUENCING THE FLOW OF GASES OR LIQUIDS
  • F15D1/00—Influencing flow of fluids
  • F15D1/10—Influencing flow of fluids around bodies of solid material
  • F15D1/12—Influencing flow of fluids around bodies of solid material by influencing the boundary layer
• • G—PHYSICS
  • G01—MEASURING; TESTING
  • G01W—METEOROLOGY
  • G01W1/00—Meteorology
  • G01W1/08—Adaptations of balloons, missiles, or aircraft for meteorological purposes; Radiosondes
• • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
  • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
  • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
  • Y02T50/00—Aeronautics or air transport
  • Y02T50/10—Drag reduction

Definitions

• the present invention relates to a device which has the aim of attenuating, or even eliminating, the parasitic movements to which the meteorological balloons are subjected during the ascent phase.
• the device is more specifically intended for closed type balloons whose envelope is made of an elastic material and which are used to measure the wind in the atmosphere, that is to say to measure the speed and direction of the wind.
• these balloons are followed either by a GPS positioner integrated in a radiosonde attached below the balloon, or by a tracking radar.
• the ball must follow the movements of the atmosphere as perfectly as possible, which is not the case with conventional balloons.
• An object of the present invention is to improve the quality of measurement of the wind of meteorological balloons having an inflatable envelope and provided with a probe of the GPS type, during their ascending phase.
• the balloon is provided with a device comprising an asperity integral with a portion of the wall of said balloon located in the upper hemisphere of said balloon during ascent, so that said asperity transmits to said balloon any aerodynamic force acting on it and that said roughness modifies the air streams marrying the external surface of said balloon to prevent said air streams stick to the surface of the lower hemisphere of said baJIon during ascent.
• the device according to the invention makes it possible to significantly increase the stability of a balloon during its ascent, this device being more specifically adapted to meteorological balloons of the closed type which have an elastic envelope.
• the air flow regime can be supercritical, which means that the air streams stick in a laminar way to the wall on a large fraction of the lower hemisphere of the balloon This regime causes instabilities in the movement and, consequently, poor tracking of the wind by the balloon It is therefore imperative that the speed is no longer supercritical and therefore that the air streams come off the wall of the balloon before arriving on the hemisphere
• the object of the present invention is to provide this separation in order to obtain good measurements of the wind speed
• the detachment of the air streams from the upper hemisphere of the balloon during the ascent phase is caused by means of a single asperity rigidly fixed to the wall of this upstream hemisphere (upper) of the balloon, the dimension of the separation roughness being chosen large enough so that the turbulent wake which forms behind it can act gradually on the adjacent nets and disturb the flow over very large portions of the balloon
• said roughness consists of an element forming a plate with sharp edges, the mean plane of which cuts the surface defined by said ball.
• said device further comprises a system comprising a mast, capable of connecting said roughness to said wall portion of said balloon, said mast being integral with said envelope of said balloon.
• the mast is able to be fixed on the ball and said astig ⁇ té is fixed on the mast.
• said mast has an internal shoulder formed by an external flange and said system- comprises an elastically deformable part, internal to said ball, able to be embedded in said mast so as to bear on said internal shoulder to wedge said envelope between said part and said mast, by which said mast is fixed on said wall portion of said balloon. It is understood that the mast must be deformable so that the flange encloses said mat and forms the internal shoulder.
• the elastically deformable part is inserted with the portion of balloon, not inflated, corresponding to the portion of wall located in the upper hemisphere, in the mast having a tubular shape at the origin. Then the lower part of the mast is clamped with the flange so as to form an internal shoulder on which is capable of pressing the elastically deformable part to wedge said portion of balloon against the shoulder.
• the mast is secured to the portion of the balloon.
• said plate member is able to be fixed in an adjustable manner on said mast, so as to give it a position relative to the balloon causing the minimum disturbance.
• said plate element has a cylindrical type curvature, the concavity of which is directed upstream of said air streams.
• the concave side of the plate element obstructs the air when the balloon is in the ascent phase.
• the plate element is pierced with orifices so as to create a grid turbulence capable of preventing said air streams from sticking to the surface of the hemisphere. lower of said balloon during ascent.
• said plate element has two parts, the mean planes of which form an angle less than 180 °.
• the roughness consists of two flat surfaces forming between them an angle which can be chosen at a any value, said surfaces being able to be of different dimensions so as to create, under the effect of the forces due to the speed of ascent, a torque tending to make the ball rotate and this, to better propagate laterally the turbulent disturbance of the wake .
• said plate element is fixed in said portion of the wall of said ball so that the mean plane of said element is inclined relative to the horizontal to cause the rotation of said ball around its vertical axis during the ascent phase.
• the plate element has a longitudinal slot.
• said roughness is made of one or more flat or concave surfaces which are used to disturb the flow in the upper part of the balloon during the climb, said surfaces being held rigidly integral with the wall of the ball.
• said roughness transmits the forces which it undergoes, it is rigid, relative to the aerodynamic constraints.
• said roughness is elastically deformable, and is made of a flexible material to be able to deform and not to damage the envelope of the balloon in the event of contact at the time of launch.
• FIG. 1 represents, in the general case, the device which is the subject of the invention, mounted on a meteorological balloon and the operation, during the ascent phase, of the asperity fixed on the upper hemisphere of the balloon
• - Figure 2 shows an embodiment in which the roughness consists of a plate with sharp edges pierced with orifices, integral with the envelope of the balloon and placed so that the angle it makes with the envelope allows it to obstruct the flow of air around the balloon, the plate itself being fixed on a part integral with the balloon envelope so that any force of aerodynamic origin on the plate directly affects the movement of the ball,
• FIG. 3 shows the attachment to the envelope of the balloon of the plate used to create a turbulent wake downstream to take off the air streams
• FIG. 4 represents a preferred embodiment according to the invention in which the roughness is this time made up of two flat plates which are made integral with the envelope by means of a part of the type of that shown in FIG. 3, these two plates forming a non-zero angle between them, having sharp edges and obstructing the flow of air around the balloon, and
• FIG 1 there is shown for the ascent phase the configuration of the device according to the invention and its operation.
• the wind speed measurement probe 1 is hooked under the balloon 4, by means of a wire 2, to the sleeve 3 used to fill the balloon with center O and elastic envelope 5.
• a non-deformable asperity As is rigidly fixed under the action of the aerodynamic forces which it undergoes.
• the air streams FAs meet the walls of the roughness As at a significant angle, which implies that the roughness is not too close to the upper pole Ps of the ball.
• the turbulent wake it is also necessary that this roughness is not located in the vicinity of the equator E of the balloon.
• the angle ⁇ made by 0, As with the vertical axis zz 'of the balloon will advantageously be limited to values which are not close to 0 ° or 90 °.
• the stabilization effect is all the more effective the greater the wake.
• FIG 2 is shown an embodiment according to the invention in which the roughness As consists of a plate P whose thickness is small compared to its other dimensions and which therefore constitutes an obstacle with sharp edges.
• This plate is fixed to a mast M secured to the envelope of the balloon.
• the plate P which has a generally rectangular shape, projects beyond the mast M and is oriented facing the flow of the air streams. Under these conditions, the wake behind the plate has, with respect to that of the mast M alone, dimensions which are much greater and a density which is much higher due to the sharp edges of the plate P. It follows that the stabilizing effect on the ball is more significant since the turbulent nets Ft disperse faster on the sides of the plate P than if there were only the mast M to obstruct.
• the plate P In order for the system to be effective, the plate P must be made of a material sufficiently rigid so that the aerodynamic pressure forces which it undergoes, and which are linked to the speed of rise of the balloon, are fully reflected on the balloon himself.
• the angular position of the plate P and of the mast M characterized by the angle ⁇ , have a value such that the threads FAs arriving there are then well detached from the envelope of the balloon.
• a series of orifices ⁇ are drilled therein so that the incident air streams FAs give, downstream, a grid turbulence which makes it possible to better take off the air and further increase stability.
• FIG 3 there is shown, according to the invention and by way of example, an embodiment of the mast-plate system used to unstick the air streams.
• the mast M shown in Figure 2 is in fact composed of a set of four parts.
• the first is a cylindrical sleeve which will advantageously be made of a material which is both rigid and deformable of the polyurethane foam type, this sleeve being made integral with the casing 5 by a system which will be detailed below.
• the part 7 is also made of a rigid but deformable material whose diameter is taken slightly smaller than that of the internal diameter of the sleeve 8 so that with the thickness of the envelope 5 between the part 7 and the sleeve 8 there is no play between the two pieces.
• the part 7 was introduced into the sleeve 8 also passing through a circular orifice 11 located on a flat part 6 which is therefore interposed between the envelope 5 of the balloon and the base 14 of the sleeve 8.
• the diameter of the circular orifice 11 must be less than the outside diameter of the sleeve 8 for the reasons which will appear subsequently.
• a groove 9 In the lower part of the outer surface of the sleeve 8 is hollowed out a groove 9 in which a collar or a retractable flange 10 is placed. Once tightened, the collar 10, taking into account the elasticity of the material constituting the sleeve 8, limits the internal diameter of said sleeve 8 to a value less than that of the part 7 which can then no longer escape downwards. his accommodation.
• the envelope 5 When the balloon 4 is inflated before its launch for the sounding, the envelope 5 therefore ensures, by its elastic tension forces, the separation of the mast M and of the plate P on itself, it being understood that the part 7 does not can escape through the orifice 11, which keeps the flat piece 6 interposed between the sleeve 8 and the balloon, the flat piece 6 serving to support the ball asperity As serving as an aerodynamic obstacle.
• a second embodiment according to the invention consists in replacing the collar 10 by an elastic bracelet in extension making one or more turns in the groove 9 and which, by the elastic forces which it exerts, prevents the part 7 from leaving the sleeve 8.
• Figure 4 there is shown, still in no way limiting, a second embodiment of the roughness forming obstacle As.
• two thin plates P1 and P2 are used which are made integral with a mast M2 fixed on the envelope 5.
• the plates P1 and P2 are oriented relative to the surface of the balloon. so as to obstruct the air streams FAs which arrive thereon and they form between them an angle ⁇ which may have an arbitrary value but more advantageously less than 180 °.
• FIG. 5 another embodiment of the obstacle has been shown, still according to the invention, which serves to detach the air streams from the surface of the balloon and therefore to ensure perfect stabilization thereof during the climb.
• the obstacle consists of two parallel plates Pa and Pb leaving between them a rectangular slot fr. The incident air streams pass partly through the slit fr and give rise, downstream, to the turbulent threads Ft which take off from the wall of the balloon.

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• Engineering & Computer Science (AREA)
• Aviation & Aerospace Engineering (AREA)
• Environmental & Geological Engineering (AREA)
• Mechanical Engineering (AREA)
• Physics & Mathematics (AREA)
• General Engineering & Computer Science (AREA)
• Fluid Mechanics (AREA)
• Life Sciences & Earth Sciences (AREA)
• Atmospheric Sciences (AREA)
• Biodiversity & Conservation Biology (AREA)
• Ecology (AREA)
• Environmental Sciences (AREA)
• Indicating Or Recording The Presence, Absence, Or Direction Of Movement (AREA)
• Toys (AREA)

Applications Claiming Priority (5)

Publications (1)

Family

ID=26212068

Family Applications (1)

Country Status (6)

Families Citing this family (7)

Citations (1)

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• 2000
  • 2000-01-04 FR FR0000047A patent/FR2793887B1/fr not_active Expired - Fee Related
  • 2000-05-18 US US09/926,527 patent/US6655206B1/en not_active Expired - Fee Related
  • 2000-05-18 JP JP2000618752A patent/JP2002544064A/ja not_active Withdrawn
  • 2000-05-18 EP EP00929629A patent/EP1185890A1/de not_active Withdrawn
  • 2000-05-18 AU AU47647/00A patent/AU4764700A/en not_active Abandoned
  • 2000-05-18 WO PCT/FR2000/001343 patent/WO2000070369A1/fr not_active Application Discontinuation

Patent Citations (1)

Non-Patent Citations (1)

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