WO2015091954A2 - Procédé et dispositif de transport d'un support publicitaire ou d'informations de grande superficie au moyen d'un petit appareil volant commandable à distance et support publicitaire ou d'informations correspondant - Google Patents

Procédé et dispositif de transport d'un support publicitaire ou d'informations de grande superficie au moyen d'un petit appareil volant commandable à distance et support publicitaire ou d'informations correspondant Download PDF

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Publication number
WO2015091954A2
WO2015091954A2 PCT/EP2014/078751 EP2014078751W WO2015091954A2 WO 2015091954 A2 WO2015091954 A2 WO 2015091954A2 EP 2014078751 W EP2014078751 W EP 2014078751W WO 2015091954 A2 WO2015091954 A2 WO 2015091954A2
Authority
WO
WIPO (PCT)
Prior art keywords
information
small aircraft
advertising
rotor
air
Prior art date
Application number
PCT/EP2014/078751
Other languages
German (de)
English (en)
Other versions
WO2015091954A3 (fr
Inventor
Ziad KABBANI
Original Assignee
Kabbani Ziad
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 Kabbani Ziad filed Critical Kabbani Ziad
Publication of WO2015091954A2 publication Critical patent/WO2015091954A2/fr
Publication of WO2015091954A3 publication Critical patent/WO2015091954A3/fr

Links

Classifications

    • G—PHYSICS
    • G09—EDUCATION; CRYPTOGRAPHY; DISPLAY; ADVERTISING; SEALS
    • G09F—DISPLAYING; ADVERTISING; SIGNS; LABELS OR NAME-PLATES; SEALS
    • G09F21/00—Mobile visual advertising
    • G09F21/06—Mobile visual advertising by aeroplanes, airships, balloons, or kites
    • G09F21/12—Mobile visual advertising by aeroplanes, airships, balloons, or kites the advertising matter being towed by the aircraft
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U10/00—Type of UAV
    • B64U10/10—Rotorcrafts
    • B64U10/13—Flying platforms
    • B64U10/14—Flying platforms with four distinct rotor axes, e.g. quadcopters
    • G—PHYSICS
    • G09—EDUCATION; CRYPTOGRAPHY; DISPLAY; ADVERTISING; SEALS
    • G09F—DISPLAYING; ADVERTISING; SIGNS; LABELS OR NAME-PLATES; SEALS
    • G09F19/00—Advertising or display means not otherwise provided for
    • G09F19/12—Advertising or display means not otherwise provided for using special optical effects
    • G09F19/18—Advertising or display means not otherwise provided for using special optical effects involving the use of optical projection means, e.g. projection of images on clouds
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U2101/00—UAVs specially adapted for particular uses or applications
    • B64U2101/20—UAVs specially adapted for particular uses or applications for use as communications relays, e.g. high-altitude platforms
    • B64U2101/24—UAVs specially adapted for particular uses or applications for use as communications relays, e.g. high-altitude platforms for use as flying displays, e.g. advertising or billboards
    • G—PHYSICS
    • G09—EDUCATION; CRYPTOGRAPHY; DISPLAY; ADVERTISING; SEALS
    • G09F—DISPLAYING; ADVERTISING; SIGNS; LABELS OR NAME-PLATES; SEALS
    • G09F13/00—Illuminated signs; Luminous advertising
    • G09F13/02—Signs, boards, or panels, illuminated by artificial light sources positioned in front of the insignia
    • G—PHYSICS
    • G09—EDUCATION; CRYPTOGRAPHY; DISPLAY; ADVERTISING; SEALS
    • G09F—DISPLAYING; ADVERTISING; SIGNS; LABELS OR NAME-PLATES; SEALS
    • G09F27/00—Combined visual and audible advertising or displaying, e.g. for public address
    • G09F27/005—Signs associated with a sensor

Definitions

  • the present invention relates to a method and device for transporting a large-area information or advertising space by means of a remotely controllable small aircraft and an associated information and / or advertising space Advertising space, in particular in the form of a flag.
  • the invention serves the presentation of an information or advertising space. The presentation takes place in particular by arranging the information or advertising space on a kind of flag, which is attached to a small aircraft. In contrast to advertising flags, which are carried behind aircraft, this is a flag, which is supported by a remotely controllable, helicopter-like small aircraft.
  • the present invention has the object, at least partially overcome the disadvantages known from the prior art and in particular to propose a method and apparatus for transporting an information or advertising space and an associated information or advertising space, with a use largely independent weather conditions or visibility. Furthermore, a presentation of the information or advertising space with little time and simple means should be possible, this presentation can also be used in limited areas and flexibly adapted to the existing spatial conditions.
  • the method according to the invention is directed to a transport of at least one information or advertising space by means of a remotely controllable, helicopter-like small aircraft, the information or advertising space being substantially below (at one level). half, not necessarily vertically below) of the small aircraft is kept substantially in a predetermined shape.
  • the small aircraft proposed here has in particular at least one substantially horizontally arranged rotor as a buoyancy means, so that a movement of the small aircraft in an exclusively vertical direction is possible.
  • the small aircraft is unmanned and is therefore steered in particular via a remote control.
  • it is suitable for the transport of loads of up to a maximum of 50 kg [kg], preferably up to a maximum of 10 kg, more preferably up to a maximum of 5 kg.
  • a remote control of the small aircraft over a distance of at most 500 m [meters] is possible, preferably at most 100 m.
  • the small aircraft is particularly suitable for ascending from a rest position (from a solid surface) into the air and lifting the surface attached to the small aircraft so that the small aircraft and the surface can move freely in the airspace.
  • the surface is held substantially by gravity below the small aircraft.
  • the information or advertising surface is preferably a type of lug which is held in a desired alignment with the direction of flight and / or wind direction by alignment means, in particular flow-guiding means.
  • Flag means, in particular, that the surface is flexible, that is to say in particular folding or rolling up or spreading it out. Flag also means that the surface is essentially two-dimensional, ie has a height and width, but only a small thickness. In particular, it is proposed that the surface has a height (parallel to gravity) in a range of 0.1 to 20 m, in particular of 1 to 3 m; and a width (perpendicular to gravity) in a range of 0.05 to 4 m, especially 0.2 to 1.5 m. The thickness is in particular 0.1 mm [millimeter] to 0.15 m.
  • information and advertising space can also be formed by a three-dimensional body, z. B. by a cube or cylinder (or the like).
  • the three-dimensional body of the information surface is (or comprises) a beamer which can project information and / or advertising on a surface remote from the body and the small aircraft, and in particular fixed surface.
  • a projector is a video projector (also a projector, digital projector, data-video projector) and thus a projector, the images from a visual output device (TV receiver, computer, DVD player, VCR, etc.) to an audience in an enlarged form can project a screen / surface remote from the beamer.
  • a propeller is arranged under the beamer and thus under the small aircraft, which is overflowed by the downwardly pressed air and is thus set in rotation.
  • the propeller is almost transparent and can be used for the projector as a projection screen.
  • a surface structure is arranged under the projector (circular, polygonal), which is substantially transparent and is used by the projector as a projection surface.
  • the three-dimensional body such as the surface and the flag, by alignment, in particular flow, in a desired orientation to the direction of flight and / or wind direction are kept.
  • any of the following items can be used:
  • a suspension device that connects the surface to the small aircraft so that the orientation of the small aircraft can be transferred to the surface.
  • an inflatable surface which is connected to the surface can be used as the flow-guiding means.
  • the flowable surface is thus affected by moving air (air flow, caused by movement of the small aircraft through the air space or by wind or by buoyancy means of the small aircraft) that an orientation of the Strömungsleitschs and thus the surface relative to the direction of the moving Air takes place.
  • the flow guiding means serves to reduce the flow resistance of the surface.
  • the flag is arranged and aligned so that it provides the air pressed by the small aircraft down a small or a certain attack surface, in particular the downwardly flowing air to stabilize the (planar) shape and / or the Orientation of the flag is used.
  • the flag is flat, ie the surface has substantially no curvature in the planes, which are formed by height and thickness and by the width and thickness of the surface.
  • the air displaced downwards by the buoyancy means of the small aircraft is used here to stabilize the shape and / or orientation of the flag.
  • the small aircraft has a plurality of buoyancy means, so that air flows on both sides of the flag (sides, which are arranged parallel to the plane, which is spanned by height and width) substantially downwards (parallel to gravity).
  • This air movement in particular together with a certain inherent rigidity of the flag, causes the flag maintains a flat shape.
  • the alignment of the surface is carried out automatically, self-regulating and / or remotely controlled.
  • the surface is rotatable about a vertical axis and that this rotation about the vertical axis is automatic, self-regulating (eg by air currents, see above) and / or remotely controlled.
  • this rotation about the vertical axis is automatic, self-regulating (eg by air currents, see above) and / or remotely controlled.
  • an upper limit of the information or advertising space is arranged at a distance of at least 2 m and at most 10 m, preferably at least 3 m, particularly preferably at least 4 m, to an underside of the small aircraft below the small aircraft.
  • the upper limit is formed by a frame or a holder to which the surface is connected. The distance proposed here ensures that the turbulences in the air caused by the driven means do not interfere with the surface, ie deformation of the surface by turbulent air flows is largely avoided.
  • the invention further relates to a device for transporting at least one information or advertising space by means of a remotely controllable, helicopter-like small aircraft with a holder or frame for receiving the information or advertising space, as well as a suspension device for hanging the holder or frame on the underside of the small aircraft ,
  • the information or advertising area can essentially be arranged below the small aircraft in a predetermined form.
  • the holder ensures, in particular, that the surface is not deformed by the suspension on the suspension device.
  • the frame encloses the surface, so that by the frame stiffening of the surface takes place.
  • struts can be provided in addition to frame or holder, which allow a further stiffening of the surface.
  • the following materials are proposed for holders, frames and struts:
  • Fiber material / composite material (with glass fibers and / or carbon fibers),
  • the invention further relates to a device for transporting at least one information or advertising space by means of a remotely controllable, helicopter-like small aircraft, wherein the information or advertising space is formed by at least one surface structure, which serves as a projection surface for a beamer, wherein a can be arranged below the small aircraft suspension device Beamer positioned above the surface structure, wherein the distance from the surface structure to the small aircraft is at least 7 m [meters] and the surface structure thus forms against the downwardly depressed air no flow resistance.
  • the surface structure under the small aircraft is essentially aligned horizontally.
  • the surface structure is arranged under the projector and fixed there via a frame with at least one strut.
  • the suspension device and / or on the holder or frame and / or on the information or advertising surface alignment in particular flow, arranged for aligning the information or advertising space in a desired orientation to the direction of flight and / or wind direction.
  • the information or advertising space or the holder or frame have at least one sensor for determining the orientation and / or the horizontal inclination of the information or advertising space.
  • the sensor in conjunction with suitable control means enables a predetermined orientation (eg, by rotation about a vertical / horizontal axis) and / or inclination of the surface relative to the vertical / horizontal axis to be automatically resumed.
  • the sensor can ensure that an inclination of the surface with respect to the vertical / horizontal axis remains within a predetermined range (eg at most 10 degrees in each direction). This inclination of the surface can be compensated in particular by movements of the small aircraft (speed in the horizontal direction, relative speed to prevailing winds, rotation of the surface about the vertical / horizontal axis, so that the area of attack of the surface is reduced in relation to winds).
  • the information or advertising surface is designed permeable to air, preferably reticulated with a plurality of openings, each having a first cross-sectional area of 1 to 10 mm 2 , preferably 2 to 6 mm 2 .
  • the first cross-sectional area of the openings forms at least 60% of the area, preferably at least 80%, particularly preferably at least 90% of the area.
  • the air resistance of the surface is reduced by the air permeability.
  • the device is thus less sensitive to air currents acting on the surface.
  • the small aircraft and / or the device comprises lighting means which also identify a position of the small aircraft / device in the dark. Furthermore, it is proposed that illuminants are provided so that the surface can be illuminated. tet is. Furthermore, it is proposed that the device comprises loudspeakers for the acoustic transmission of information.
  • an auto-pilot control function is provided, by which the small aircraft can maintain / reach / fly over / repeatedly approach or fly in a predetermined position / trajectory.
  • the invention is further directed to an information or advertising space, which is suitable for transport under a remotely controllable, helicopter-like small aircraft, the information or advertising space a second cross-sectional area of 1 to 20 m 2 [square meters], in particular from 1 to 4 m 2 and is permeable to air, preferably reticulated with a plurality of openings, each having a first cross-sectional area of 1 to 10 mm 2 , preferably 2 to 6 mm 2 .
  • the information or advertising space can be fixed in or on a holder or frame, preferably with an upper limit, and has means for stabilizing its shape and / or alignment means, in particular flow-guiding means, for aligning the information or advertising area in a desired orientation to the direction of flight and / or wind direction.
  • the information or advertising space includes its own further buoyancy means.
  • these buoyancy means serve exclusively to reduce the weight of the information or advertising surface or to increase the buoyancy.
  • another buoyant at least one of the following is designated:
  • the rotor has its own drive.
  • the information or advertising area comprises at least one own further buoyancy means, which uses the air pressed down by the small aircraft to generate buoyancy.
  • this buoyancy means serves exclusively to reduce the weight of the information or advertising surface or to increase the buoyancy.
  • the at least one further buoyant means is arranged on the suspension device and / or on the holder or frame and / or on the information or advertising surface.
  • a buoyancy agent is z.
  • B a first rotor, which is rotated by the compressed air downwards in rotation.
  • This first rotor is so arranged below the small aircraft that it is overflowed by the compressed air down.
  • this first rotor is connected via a mechanical connection (gear, belt, shaft) with a second rotor.
  • the second rotor is arranged so that it is not or only slightly overflowed by the compressed air down.
  • the first rotor is used to drive the second rotor.
  • the second rotor generates lift.
  • At least one first and one second rotor are arranged on the information or advertising surface as further buoyancy means.
  • the first rotor is rotated by the air pushed down by the small aircraft and turned over. carries this rotation on the second rotor.
  • the so rotated in rotation second rotor generates buoyancy for the information or advertising space.
  • the invention is further directed to an information or advertising space, which is formed by a propeller, which serves as a projection surface for a video projector.
  • the information or advertising space is suitable for transport under a remotely controllable, helicopter-like small aircraft, wherein the at least one propeller is arranged under the beamer and thus under the small aircraft and is overflowed by the pressed down air and thus set in rotation.
  • the propeller is almost transparent and can be used for the projector as a projection screen.
  • the propeller is thus used as a projection surface, which can also be viewed from the side of the propeller opposite the projector (ie from below the propeller).
  • the device is suitable for carrying out the method and the surface is part of the device.
  • the comments on the method apply equally to the device and the information or advertising space and vice versa.
  • FIGS. show particularly preferred embodiments, to which the invention is not limited.
  • the figures and in particular the illustrated proportions are only schematic.
  • Like reference numerals show like objects. Show it:
  • Fig. 1 a device in a side view
  • Fig. 2 the device of Figure 1 in a plan view.
  • 3 shows the device of Figures 1 and 2 in a side view.
  • 4 shows an embodiment of a flag;
  • 5 shows a further embodiment of a flag;
  • 6 shows a device with further buoyancy means;
  • 7 shows a device with a beamer;
  • FIG. 8 shows a device with a beamer and a propeller arranged underneath as a projection surface
  • FIG. 9 shows a device with a beamer and a surface structure arranged underneath as a projection surface.
  • the device 15 shows a device 15 in a side view in flight through the air space 27.
  • the device 15 comprises a small aircraft 2 that can be steered via a remote control 26.
  • the small aircraft 2 has an underside 14 with which the small aircraft 2 contacted the ground at rest.
  • a suspension device 13 is arranged, on which a holder 11 a surface 1 is arranged hanging.
  • the suspension device 13 is connected via two connections with the holder 11 and thus allows a fixed alignment 18 of the surface 1 to the small aircraft 2.
  • the suspension device 13 and also the holder 11 serves as an alignment means 5.
  • the holder 11 is at an upper boundary 10 of the surface 1 is arranged.
  • the area 1 is shown here as a flag 4.
  • the flag 4 has a substantially two-dimensional shape 3, wherein the second cross-sectional area 21 is formed by height 30 and width 31 of the area 1.
  • the surface is additionally stiffened by a brace 34 which extends along the vertical axis 33 (here central axis of the surface 1).
  • the brace 34 and a arranged on the lower boundary 38 holder 11 serve here as a means 22 for stabilizing the mold 3.
  • the arranged at the lower boundary 38 holder 11 additionally serves as an alignment means 5 for aligning the surface 1 to the direction of flight 7 and / or wind direction 8.
  • the upper Limit 10 of the surface 1 is arranged at a distance 23 to the bottom 14 of the small aircraft 2.
  • the surface 1 has openings 19 which are each formed by an air-permeable first cross-sectional area 20.
  • a frame 12 (only indicated here) can be used, which completely covers the surface 1.
  • the area 1 can z. B. by winds or by the airspeed of the small aircraft 2, so that the surface 1 has a slope 17 relative to the vertical axis 33 (see also in Fig. 3). This inclination 17, but also the orientation 18 can be detected by a sensor 16 and control means 39 and if necessary changed / compensated.
  • Fig. 2 shows the device 15 of Fig. 1 in a plan view. Surface 1 has been omitted in this illustration.
  • the device 15 here comprises four rotors 28 as buoyancy means 29.
  • the device 15 further comprises a suspension device 13 with two connections between device 15 and holder 11.
  • the device 15 can be controlled about the vertical axis 33 in an orientation 18, so that the surface 1 also occupies this orientation 18.
  • the device 15 moves in the direction of flight 7 through the air space 27.
  • FIG. 3 shows the device 15 from FIGS. 1 and 2 in another side view.
  • the narrow side of the area 1 shown by the height 30 and thickness 32 is formed.
  • a holder 11 is arranged as an alignment means 5.
  • the holder 11 comprises an additional weight 35, so that the holder 11 also serves as means 22 for stabilizing the mold 3 of the surface 1.
  • a light source 36 for illuminating the surface 1 is arranged on the holder 11 and loudspeaker 37.
  • the additional weight 35 in particular stabilizes the shape 3 of the surface 1 with respect to the turbulences 25 in the air 9 which are caused by the driving means 29.
  • Fig. 4 shows an embodiment of the flag 4 and the information or advertising space 1. This is attached via a suspension device 13 to the small aircraft 1 (not shown here).
  • the upper boundary 10 of the lug 4 is formed by a holder 11, which simultaneously serves as alignment means 5 and flow-guiding means 6.
  • the flag 4 has a height 30 and a maximum thickness 32. The thickness 32 is reduced continuously in the representation shown here to the lower left corner of the flag 4.
  • the flag 4 in particular a wing shape, so that the flag 4 on the one hand has a low flow resistance and on the other hand by the passing air 9 in their Form 3 is stabilized.
  • the surfaces of the lug 4 embodied as flow-guiding means 6 are shown here in simplified form as flat surfaces. In particular, a curved surface is proposed.
  • FIG. 5 shows a further embodiment of the lug 4 or of the information or advertising surface 1.
  • the thickness 32 decreases continuously starting from the upper right corner to the other three corners of the lug.
  • the information or advertising surface 1 here comprises further operating means 29, which use the compressed air from the small aircraft 2 down 9 to generate lift 44.
  • the further buoyancy means 29 are arranged here on the holder 11.
  • the further buoyancy means comprise a first rotor 41, which is set in rotation by the compressed air 9 of the lifting means 29 of the small aircraft 2.
  • this first rotor 41 is arranged below the small aircraft 2 in such a way that it is overflowed by the compressed air 9.
  • the first rotor 41 is connected to a second rotor 42 via a mechanical connection 43 (gear, belt, shaft).
  • the second rotor 42 is arranged so that it is not or only to a small extent overflowed by the, driven by the buoyancy means 29 of the small aircraft 2 down air 9.
  • the first rotor 41 is used to drive the second rotor 42.
  • the second rotor 42 like the rotors 28 of the small aircraft 2, generates lift 44.
  • Fig. 7 shows a device 15 with a projector 45.
  • the beamer 45th is arranged here on the holder 11.
  • the projector 45 is a video projector (also projector, digital projector, data-video projector) and thus a projector, the images from a visual output device (television receiver, computer, DVD player, VCR, etc.) for an audience in an enlarged form to a projected from the projector 45 away screen / surface 40 projected.
  • FIG 8 shows a device 15 with a projector 45 and a propeller 46 arranged underneath as the projection surface 47.
  • the propeller 46 is set in rotation by the downwardly pressed air 9 of the buoyancy means 29 of the small aircraft 2.
  • the propeller 46 is so arranged below the small aircraft 2, that he from the down compressed air 9 is overflowed.
  • the projector 45 projects images onto the almost transparent, rotating propeller blades of the propeller 46.
  • the propeller 46 is thus used as a projection surface 47, which can be viewed from the side of the propeller opposite the projector 45 (ie from below the propeller 46).
  • FIG. 9 shows a device 15 with a projector 45 and a surface structure 48 arranged underneath as a projection surface 47 for the projector 45.
  • the device 15 is transported by the small aircraft 2, wherein a suspension device 13 arranged below the small aircraft 2 above the projector 45 above the surface structure 48 is positioned, the distance 23 from the surface structure 48 to the small aircraft 2 is at least 7 m and the surface structure 48 thus forms no flow resistance to the downwardly compressed air 9.
  • the surface structure 48 is aligned horizontally here. However, an inclination to the horizontal is also possible.
  • the surface structure 48 is arranged below the projector 45 and fixed there via a frame 49 with at least one strut 50.

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  • Engineering & Computer Science (AREA)
  • Business, Economics & Management (AREA)
  • Accounting & Taxation (AREA)
  • Marketing (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Theoretical Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Remote Sensing (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Toys (AREA)
  • Vehicle Waterproofing, Decoration, And Sanitation Devices (AREA)

Abstract

La présente invention concerne un procédé de transport d'au moins un support (1) publicitaire ou d'informations au moyen d'un petit appareil volant (2) de type hélicoptère, commandable à distance. Le support (1) publicitaire ou d'informations est maintenu sensiblement sous le petit appareil volant (2), sensiblement dans une forme prédéfinie (3). La présente invention concerne en outre un dispositif (15) de transport d'au moins un support publicitaire ou d'informations, et un support (1) publicitaire ou d'informations.
PCT/EP2014/078751 2013-12-19 2014-12-19 Procédé et dispositif de transport d'un support publicitaire ou d'informations de grande superficie au moyen d'un petit appareil volant commandable à distance et support publicitaire ou d'informations correspondant WO2015091954A2 (fr)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE102013114513.2A DE102013114513A1 (de) 2013-12-19 2013-12-19 Verfahren und Vorrichtung zum Transport einer großflächigen Informations- oder Werbefläche mittels eines fernsteuerbaren Kleinfluggerätes und zugehörige Informations- oder Werbefläche
DE102013114513.2 2013-12-19

Publications (2)

Publication Number Publication Date
WO2015091954A2 true WO2015091954A2 (fr) 2015-06-25
WO2015091954A3 WO2015091954A3 (fr) 2015-09-24

Family

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PCT/EP2014/078751 WO2015091954A2 (fr) 2013-12-19 2014-12-19 Procédé et dispositif de transport d'un support publicitaire ou d'informations de grande superficie au moyen d'un petit appareil volant commandable à distance et support publicitaire ou d'informations correspondant

Country Status (2)

Country Link
DE (1) DE102013114513A1 (fr)
WO (1) WO2015091954A2 (fr)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN108190022A (zh) * 2018-02-11 2018-06-22 滁州职业技术学院 一种无人机机载条幅收放装置

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Publication number Priority date Publication date Assignee Title
DE1038900B (de) * 1955-02-02 1958-09-11 Franz Ipfelkofer Vorrichtung zur Vorfuehrung von Flugreklame mittels Hubschraubern
US3683530A (en) * 1970-09-30 1972-08-15 James G Robinson Aerial display sign
FR2127755A5 (fr) * 1971-02-26 1972-10-13 Delforge Gerard
WO2008037030A1 (fr) * 2006-09-29 2008-04-03 Itsatruck Pty Ltd Système de largage de bannière pour aéronef
DE102007054126A1 (de) * 2007-11-11 2009-05-20 Stefan Reich Unbemanntes Banner-tragendes Fluggerät und Verfahren zum Lufttransport eines Darstellungsobjekts
DE202008008098U1 (de) * 2008-06-17 2008-10-16 Treumann, Christian Fliegender, ferngesteuerter Werbeträger
CN102789667A (zh) * 2011-05-16 2012-11-21 李开超 四种悬浮式交通警告标志及六种标志系统
AT511607B1 (de) * 2011-08-24 2013-01-15 Kleinheinz Willibald Rudolf Schleppvorrichtung für ein werbebanner

Non-Patent Citations (1)

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Title
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WO2015091954A3 (fr) 2015-09-24
DE102013114513A1 (de) 2015-06-25

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