WO2012135876A2 - Nouveau type d'aérostat futuriste - Google Patents

Nouveau type d'aérostat futuriste Download PDF

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Publication number
WO2012135876A2
WO2012135876A2 PCT/AT2012/000075 AT2012000075W WO2012135876A2 WO 2012135876 A2 WO2012135876 A2 WO 2012135876A2 AT 2012000075 W AT2012000075 W AT 2012000075W WO 2012135876 A2 WO2012135876 A2 WO 2012135876A2
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WO
WIPO (PCT)
Prior art keywords
airship
propellers
types
fuselage
wings
Prior art date
Application number
PCT/AT2012/000075
Other languages
German (de)
English (en)
Other versions
WO2012135876A3 (fr
Inventor
Firooz Kita
Original Assignee
Firooz Kita
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 Firooz Kita filed Critical Firooz Kita
Priority to ATA9101/2012A priority Critical patent/AT521768B1/de
Priority to DE112012001360.3T priority patent/DE112012001360B4/de
Publication of WO2012135876A2 publication Critical patent/WO2012135876A2/fr
Publication of WO2012135876A3 publication Critical patent/WO2012135876A3/fr

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Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64B—LIGHTER-THAN AIR AIRCRAFT
    • B64B1/00—Lighter-than-air aircraft
    • B64B1/06—Rigid airships; Semi-rigid airships
    • B64B1/24—Arrangement of propulsion plant
    • B64B1/30—Arrangement of propellers
    • B64B1/32—Arrangement of propellers surrounding hull
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64B—LIGHTER-THAN AIR AIRCRAFT
    • B64B1/00—Lighter-than-air aircraft
    • B64B1/06—Rigid airships; Semi-rigid airships
    • B64B1/20—Rigid airships; Semi-rigid airships provided with wings or stabilising surfaces
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64B—LIGHTER-THAN AIR AIRCRAFT
    • B64B1/00—Lighter-than-air aircraft
    • B64B1/06—Rigid airships; Semi-rigid airships
    • B64B1/22—Arrangement of cabins or gondolas
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64B—LIGHTER-THAN AIR AIRCRAFT
    • B64B1/00—Lighter-than-air aircraft
    • B64B1/06—Rigid airships; Semi-rigid airships
    • B64B1/24—Arrangement of propulsion plant
    • B64B1/30—Arrangement of propellers
    • B64B1/34—Arrangement of propellers of lifting propellers
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64B—LIGHTER-THAN AIR AIRCRAFT
    • B64B1/00—Lighter-than-air aircraft
    • B64B1/68—Water flotation gear
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U10/00—Type of UAV
    • B64U10/30—Lighter-than-air aircraft, e.g. aerostatic aircraft
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64B—LIGHTER-THAN AIR AIRCRAFT
    • B64B2201/00—Hybrid airships, i.e. airships where lift is generated aerodynamically and statically

Definitions

  • This idea and invention relates to methods of making novel airships that do not operate as known conventional, classic and traditional types of e.g. Zeppelin airships (ovate short or long) look like, but with a multiple wide and Wider hull, for example. about three corner-like (fig.1, 2,5,7 etc,) or round and oval etc, with more than one large inner gas tank and or balloons as well as with several propellers including other modern and necessary instruments and equipment as well as larger passenger Saloon (for more passengers) and good chamber (storage compartment) and various cabins are equipped.
  • These airships (LS) are no longer a classic gondle used (hang in the lower part of the airship).
  • the PV cells and panels are selected from special lightweight solar cells (PV photovoltaic) with higher efficiency and best with flexible and lightweight PV panels / Panellen and used.
  • This PV cell type e.g. As a stable thicker film is installed on the surfaces of the fuselage of the airship (Large surface part of the fuselage and surface of the wings is covered with such solar panels / foil, Fig.1 / 2).
  • the special PV foils are made of high quality and flexible materials / foils (elastic), antistatic, stable, transparent with necessary coatings against cold, heat and agreed for different climate, high, etc used these LS types.
  • This PV system generates and procures the necessary power consumption of the whole or a Large part of the airship especially for the propeller drive (engines etc,) and other equipment as well as for the instruments, hydraulic systems and lighting, etc., with one or more storage devices and systems (such as batteries).
  • This LS with its particularly sophisticated design and aerodynamic shape and equipment, can also rise above 20,000 feet in height and, as well known on the market as LS and cargo airships, can also be e.g. carry more than 60,000 square meters of helium and payload of 500 tons over 2km in the air.
  • This Novel Design and Types of Airships allows these to reach even greater distances (reach) with more overall load (total weight) at a faster speed. It is also very important that these types of airships play a major role as the most environmentally friendly transport vehicles in the world (compared to aircraft, no emissions, no noise, no particulate matter and CO 2 pollution etc.). In addition, these LS are a very interesting and attractive experience for passengers (tourists) as well as for the transport industry with many advantages and larger sources of revenue (cargo load / goods transport).
  • LS types are at least two turbines (propellers) on the rear til of the hull (right and left, Fig. 2/1) and in some types of LS in addition e.g. one or two turbines (propellers) are installed in the front part of the fuselage (Fig. 2/8) or on / on / in the wing / wings / wings (Fig. 5/2 and Fig. 8/2).
  • movable types of propellers may move in different directions depending on the type and types of LS (Figs. 9.1 / 1 and 1.1, Fig. 10/4) and in horizontal or vertical form be positioned (eg, Fig. 9). They allow all types of LS to lift vertically or vertically to land, to ascend at different heights, to continue horizontal driving (depending on weather conditions), to stand on one point in the air (high and level) like helicopters, to either right and or Left maneuvering (also in combination with various moving wings / wings) and are also responsible for balancing the airship.
  • propellers / turbines can also be rotated in any direction to achieve the desired direction (Fig.9 / 1 and 9.1 / 1 & 1.1).
  • a flat bottom of the fuselage (Figs. 1/11, Fig. 5/1, 10/5, etc.) allows all of these types of LS series to be combined with a full nose aerodynamic design of the flying vessel (which is different from the conventional types of LS types such as Zeppelin etc) are even safer and faster to drive.
  • the entire various wings of the LS types including all propellers (turbines and drives) and use of light and flame-retardant gas in containers (eg helium) as well as lightweight but stable construction materials such as aluminum, composite (carbon) and glass fiber, PE fiber etc, are also other reasons (instruments / materials / appliances etc) that rose for providing additional power for higher, more stability, more safety and more speed this LS Types as well as for the long-distance purposes are responsible.
  • indoor and outdoor sheath are also known as various composites / composites such as aluminum (aluminum composite), carbon fiber, special intelligence-mixed textiles with other fibers, fire retardant / fire retardant materials and fiber, which are lightweight and stable and non-flammable materials, windows (windows) and all walls and floor constructions and materials are of course selected and used from the latest materials (known in the art, technologies and materials).
  • various composites / composites such as aluminum (aluminum composite), carbon fiber, special intelligence-mixed textiles with other fibers, fire retardant / fire retardant materials and fiber, which are lightweight and stable and non-flammable materials, windows (windows) and all walls and floor constructions and materials are of course selected and used from the latest materials (known in the art, technologies and materials).
  • An unmanned or manned scientific or military type of these LS can also be used for environmental observation purposes as well as for topography and or drones and cruising etc.
  • Great advantage of such species are with lowest noise (almost no), invisible radar (possibilities) and ability to ascend at the targeted altitude (allowed and possible altitude for LS) and to remain at a desired altitude,
  • the focus of this idea and invention relates to various shapes and designs of airships, constructed and built with Wider Shape of hull with a flat base, and equipped with more than one Giant Gas tanks (in right and left of the airship) and in the center of the airship a conventional aircraft-like large cabin eg in 1 & 2 and 3 levels (Fig.1 / 1, Fig.2 / 6, Fig.3 / 1, Fig.6 / 1, Fig.5 / 3, Fig.7.1 / 1, Fig.9.1 / 9, etc.,).
  • LS designs were purposely designed as e.g. in the form of eagle and butterfly ( Figure 5), etc. Designed and engineered to achieve multiple benefits that is possible only in these forms including Aerodynamic designs of the hull.
  • Various forms of wings and drives (movable and stable propellers, turbines) etc. are also additional elements for mentioned advantages of this type of airships (LS).
  • the propellers / turbines / motors and most of LS's built-in equipment and instruments are electrically driven (use of electricity, solar energy, stored power / batteries, etc.) and as hybrid drives can use additional fuels / fuels with lowest pollutants (eg environmentally friendly fuels / Spriten / Biofuel / Biofuel Etc).
  • Some or all drives / propellers / engines used have dual fuel function (hybrid) with little fuel consumption and exhaust gases.
  • wind catchers can play an important role. They can be operated by Manuel until LS has landed safely at least in a desired or unified field or on the water, and to be located and rescued by rescue team.
  • a solar energy panels (photovoltaic cells in flat and flexible form for fixation on the, not straight and full-body LS fuselage) are also responsible for manufacturing necessary electricity (electricity), which are installed on the upper part of the airship fuselage. These LS are therefore also very quiet and have almost no noise.
  • gondolas are built in mostly airships and hot air balloons in the lower part of the airship (hanging cabin), not only for technical reasons, but also with an advantage that on slow and almost noiseless driving can look closely at the environment and observe
  • These airbags will allow these airships to land vertically on the water without lowering the LS into the water. It is also possible, in normal circumstances and for specific purposes, to use these air cushions as props (such as seaplanes) for landing and picking up the airstrip on the runway (water or in fields such as at an airport, and or at ports etc.). When lifting and flying these retractable air cushions are pulled in and encapsulated in their place (Fig.3 / 8).
  • these inflatable air cushions are equipped with pressed air capsule or with air compressors. If required, these air cushions as Balonette, can be inflated by propellers (turbines). These air cushions are also well-agreed for landing on the runways or on the fields etc. In that case you do not need any other supports (Fig.3 / 6).
  • All approved fire extinguishing materials, equipment and systems including sprinklers are installed in LS and preinstalled.
  • Flight instruments etc, anti-lightning system and equipment, air conditioning and oxygen capsules and equipment for accidents, catering system, drinking water and washing water are present on board for other purposes.
  • Inflatable Ambulance (Enables automatic and manual) with Necessary communication. - and Transmitter / Signal Equipments etc. are always installed or available on the board (as most of LS).
  • the butterfly-shaped airships ( Figure 5) are also constructed with the same configurations and equipment and also have an aircraft-shaped cab installed in the center of the wings ( Figure 5/3). If damaged part of LS, you can repair the damaged container or equipment and instruments by connection between cabin and the inner part of the LS shell / hull (Corridor Fig. 5/6) simply this.
  • helium is a hard-to-burn and lightweight gas which is e.g. in these types of airships (as in others) can be used. It is generally no longer heavy and fast combustible oxygen used in airships.
  • this LS with several individual and safe-insulated gas containers / balloons or balloons in different sizes and shapes (eg Fig. 3/9, Fig. 4/9, Fig.6 / 3, 3.1, Fig. 5/5. 7/2, Fig.7.1 / 3, Fig.8 / 4, Fig.10 / 2, 10.1 / 1 & 3) are equipped / equipped, hardly all containers and balloons are damaged at once. Therefore, the rest of the balloons (gas containers) allow the LS to continue driving until the LS is safely landed.
  • Fig. 3/9, Fig. 4/9, Fig.6 / 3, 3.1, Fig. 5/5. 7/2, Fig.7.1 / 3, Fig.8 / 4, Fig.10 / 2, 10.1 / 1 & 3 are equipped / equipped, hardly all containers and balloons are damaged at once. Therefore, the rest of the balloons (gas containers) allow the LS to continue driving until the LS is safely landed.
  • the entire construction and container materials etc, are made and used by special high quality lightweight but very stable and refractory materials, fiber, composite and fabrics. These in case of damage, as mentioned, even during the trip are repairable.
  • Several rescue parachutes (Figure 14) are installed on the upper fuselage for more safety of the airship, these can be operated and activated manually as well as safely and safely to prevent the lanyard from accidents or sudden falls in height (for various reasons) slower to land on the ground or on the water. These screens (e.g., Fig.14 / 1) can be used over and over again.
  • the parachutes are made of special modern and high quality fibers and materials as well as refractory materials.
  • Runway is not necessary for this type of airship. These LSs can easily and easily land on the water and fields or runways perpendicular to and from there vertical lift and continue traveling.
  • Fig.2 and Fig.9.1 shows several rotatable propellers / drive motors (Fig.1 / 1 and 1, 1, Fig.9.1 / 1 and 1.1) for vertical cancel, - or land.
  • Front propellers (Fig.1 / 1, 1, Fig.9.1 / 1.1) or right and left propellers / turbine (Fig. 10/4, Fig.8 / 2) can turn right and / or left and up or down.
  • propellers can operate backwards and forwards (Lins or right turn the blades of the propellers) (e.g., Figures 7/1, 1.1.1.2 and Figure 9).
  • Propellers are e.g. installed in front and / or rear surfaces of the fuselage (Fig. 2 and Fig. 9.1). At least two (each in one side of the fuselage eg Fig. 2/2 & 1, 1 and 9/1 & 1 & 1) or outside the fuselage (Fig. 1/10, Fig. 5/2 and Fig. 8, Fig. 2) .10 / 4) is used in some new LS types (as drawn). These propellers will assist the LS in raising and landing vertically and maneuvering, right and left, up and down, and are also responsible for balancing the ship in all conditions.
  • the medium small double or just one turbine / propeller (Figs. 1.7, 13, Fig.9.1 / 8 and Fig.10 / 7.10.Fig.1 / 7 and Fig11 / 3 and Fig. 13/3), which are stable (immobile) or only right and left movable, are an additional force to allow the LS to drive faster.
  • LS For other types of LS at least two rear rotary propellers are provided (Fig.1.1 / 10) which are installed on the back of the LS fuselage. These types of propellers are best for smaller LS models because they can generate less power. Of course these propellers can also be used with other types of turbines and propellers together on these new types of airships.
  • FIG. 1 shows a novel LS (airship) with 4 turbines (propellers) which is shown in this state with closed gaps (4, 4.1) including small medium turbines (7) and various movable wings and wings (5,6,8, 14) and upper part of passenger cabin (1) and covered hull with solar cells (2) and eg window types (12) and a schematic diagram of left side of the LS (Fig.1.2), flat-shaped lower part of the fuselage (1)
  • Fig. 2 shows almost the same LS (Fig.) With 4 turbines (propellers) which is shown in this drawing with open gaps (Fig. 1 and Fig. 1). In this condition, LS can be lifted vertically or landed.
  • Fig.2 / 1, 4, 8) show push-on gap covers (sliding covers) and arm of the propellers for moving up and down which has been designated in Fig. 9 (an example).
  • Fig.3 shows When landing on the ports (airports, etc.) or on land, a special type of supports (feet) such as. (Fig.3 / 6,7) used. These sideways retractable braces are built in below LS (Fig. 3/7) and upon landing will be opened as shown and with rotation (Hydraulic and Manuel, as far as reaching in intended and Stable position) will enable LS on the Ground to land vertically.
  • the sideways retractable stairs (Fig. 3/3) also have the same function as the supports / feet (Fig./6) in both sides of passenger cabins (Fig.3 / 1) and are operated Hydraulically or Manually.
  • FIG. 4 shows several gas containers (Fig. 4/9) with a cracked (Fig. 4/16) and partitions as security walls (made of refractory materials and eg aluminum framework, etc.) for separating the individual of gas containers (Fig. 4/12) , in case of accident or outbreak of fire etc, fire extinguisher (Fig.4 / 15).
  • These measures are used in all types of these airships (this application) (no matter small LS or Large LS and manned or unmanned, with multiple or few gas tanks, etc.).
  • These isolation walls (partitions) also between gas tanks and cabins provide more safety of the LS and crew and passengers as well as preventing fire outbreak or damage in accidents and help e.g. during repair work.
  • Fig.5 Shows a LS Model (butterfly form) with rotatable side propellers (2) Hull (5) covered with solar cells (or without), and access (6) between cabin (3) and inner parts of LS / gas container compartment (5) and under part of the hull (1) upper and lower cabins (4, 4.1).
  • Figure 6 shows a large type of LS model with several gas tanks of different sizes and shapes (3., 3.1) and four turbines / propellers (two front and two in the back) and one example shows propellers in the lower part of the LS (the same movable propeller (2) in top or bottom (2.1), and a plurality of movable airfoils (4).
  • Fig.6.1 Shows a schematic representation of function of the movable propellers / propulsion / turbines in 3 Three different positions (1.1 and 1.2 and 1.3).
  • FIG. 7 shows a schematic representation of the hull and shape of a LS model (1) with at least 4 large gas containers (here only design and model / shape of LS was drawn), solar cells (2) and wing (3) nose of the LS cabins (4).
  • Fig.7.1 shows a LS model with at least 4 large gas tanks (3) and double deck cabin (1), or in 3 levels with middle cabins, windows (2) and wing / wing (4)
  • Figure 8 shows a LS model with at least 2 large gas tanks (4) and cabin (1) with 2 side propellers / turbines (2) as well as wings, adjustable tail, levels with middle cabins).
  • Fig. 9 shows e.g. only one rotary propeller / turbine on the fuselage of the LS in vertical and forward position (1, 4) is.
  • In horizontal position back to place 2 with the help of hydraulic arm "7" of the turbine / propeller
  • will be responsible for canceling the LS additional with all other propellers of the LS
  • a sliding bare void cover (6, 3)
  • vertical wing Hydrofoil, with rudder "5"
  • Fig.9.1 shows schematic representation of a LS in the air with a total of 6 turbines / propellers in vertical position and in the direction of travel (2x “1” in the rear, and 2x "1.1” in the front part of the fuselage including 2 x small medium turbines “8” ), various wings (5) and upper passenger cabin (9) windows (10), solar panels cover the LS fuselage (12) LS shell and body (11), turbine / propeller shaft / space (2, 2.1) and slide - on lids (3 ) and hydraulic arm of the turbine (7).
  • Fig.10 shows schematic representation of a LS with a total of 4 turbines / propellers in the vertical position and in the direction of travel (two “4" in the sides and two small medium turbines “7"), which the two propellers (4) in right and left and Top and bottom or transverse turn and maneuver (for directional changes and for determination of different driving directions), with two large left and right gas tanks (2) and various wings (3) and passenger cabin (1) LS shell and body (5),
  • FIG. 10 shows a schematic representation of an airship (LS) with a total of 4 large and small turbines / propellers in the vertical position and in the direction of travel (two “5" in the upper part of the fuselage and in a fair position in the lower part of the LS (5), and two small central turbines "7"), with two large left and right gas tanks (1 including 6 other gas tanks of various shapes and sizes (1, 2 and 1.3) and various hydrofoils and wings (6) and passenger cabin (4) and, for example, clothing and fixation of the gas containers (8).
  • LS airship
  • Figure 11 shows a schematic representation of an airship (LS) with a total of 4 large and small turbines / propellers in vertical position and in direction of travel (two “5" in the upper part of the fuselage and in fair position in lower part of the LS (5), and two small medium turbines "3"), with 12 different left and right Gas tanks of various shapes and sizes (2, and 2.1) and various wings / wings and wings (6) and passenger cabin (4).
  • LS airship
  • Fig. 12 shows a symbolic drawing in one of these types of airships, e.g. Use of several special type of sails / wind catcher ( Figures 14 and 14/1) installed and installed on the hull of the LS could be operated on demand or in wind situation in certain and adjusted altitude and wind direction Manuel. These windscreens (Fig. 12/1) are movable (around themselves and possible to turn around due to wind and direction selection).
  • This type of sailing can be used Manuel and as an auxiliary propulsion and power for LS. It is clear that wind direction towards or in the direction of travel is crucial for its intended use. In order for these airships to be able to operate a shorter or long haul even without the help of other propulsion and energy sources (propellers and turbines) 100% environmentally friendly and without C02 and pollutants etc. such as a pitched sail in unified situations.
  • Fig. 13 shows a schematic diagram of a large LS with at least 4 turbines / propellers in various large (2 and 3) with multiple activated and inflated airbags (1) in under the LS (as rescue tools and or landing support) on the water.
  • Fig. 14 shows a schematic representation of an LS with activated several rescue screens (1), which are installed on the fuselage of the LS and preinstalled.
  • These rescue umbrellas are designed as additional rescue measures and are made from the strongest and best-matched lightweight materials and are manually activated and opened. These umbrellas are multiple and further usable. These umbrellas have special noctilucent colors for rescue measures. Firooz Kita

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Remote Sensing (AREA)
  • Toys (AREA)
  • Filling Or Discharging Of Gas Storage Vessels (AREA)
  • Laminated Bodies (AREA)

Abstract

La présente invention concerne un aérostat présentant une forme plate, de type avion, différente de la forme de cigare, et comprenant une cabine allongée, placée de façon centrale, et deux surfaces sustentatrices placées des deux côtés de ladite cabine. Plusieurs chambres ou récipients à gaz délimités ou séparés les uns des autres sont prévus, au moins un, de préférence plusieurs, de ceux-ci se trouvant dans chacune des deux surfaces sustentatrices. Au moins un élément moteur, de préférence une hélice, se trouve dans la zone avant, dans la zone arrière et sur la face supérieure de l'aérostat. L'élément moteur peut être basculé ou escamoté dans ou à travers des orifices traversants ou des évidements prévus dans l'aérostat ou dans les surfaces sustentatrices de l'aérostat.
PCT/AT2012/000075 2011-03-22 2012-03-22 Nouveau type d'aérostat futuriste WO2012135876A2 (fr)

Priority Applications (2)

Application Number Priority Date Filing Date Title
ATA9101/2012A AT521768B1 (de) 2011-03-22 2012-03-22 Neue Art von zukünftigen Luftschiffen
DE112012001360.3T DE112012001360B4 (de) 2011-03-22 2012-03-22 Neue Art von zukünftigen Luftschiffen

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
ATA409/2011 2011-03-22
AT4092011 2011-03-22

Publications (2)

Publication Number Publication Date
WO2012135876A2 true WO2012135876A2 (fr) 2012-10-11
WO2012135876A3 WO2012135876A3 (fr) 2013-03-28

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AT (1) AT521768B1 (fr)
DE (1) DE112012001360B4 (fr)
WO (1) WO2012135876A2 (fr)

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CN104941201A (zh) * 2015-05-21 2015-09-30 东莞市诸葛流智能系统有限公司 一种会漂浮飞行的多功能电子玩具
WO2016074019A1 (fr) * 2014-11-14 2016-05-19 Christopher Betts Dirigeable perfectionné
WO2017178899A3 (fr) * 2017-07-27 2018-06-07 Wasfi Alshdaifat Transporteur aérien multitâche
WO2019092471A1 (fr) * 2017-11-13 2019-05-16 Total Sa Procédé de transport d'une charge utile vers un emplacement cible, et dirigeable hybride associé
DE102013011861B4 (de) 2013-07-16 2023-07-06 Horst Balter Ballon/Heißluftballon/Zeppelin/Ballon bzw. Heißluftballon/Zeppelin-Kombination aus einem oder mehreren Auftriebskörpern zu einem Gesamtsystem

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Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102013011861B4 (de) 2013-07-16 2023-07-06 Horst Balter Ballon/Heißluftballon/Zeppelin/Ballon bzw. Heißluftballon/Zeppelin-Kombination aus einem oder mehreren Auftriebskörpern zu einem Gesamtsystem
WO2016074019A1 (fr) * 2014-11-14 2016-05-19 Christopher Betts Dirigeable perfectionné
GB2547177A (en) * 2014-11-14 2017-08-09 Betts Christopher An improved airship
AU2015345982B2 (en) * 2014-11-14 2019-09-05 Christopher Betts An improved airship
CN104941201A (zh) * 2015-05-21 2015-09-30 东莞市诸葛流智能系统有限公司 一种会漂浮飞行的多功能电子玩具
WO2017178899A3 (fr) * 2017-07-27 2018-06-07 Wasfi Alshdaifat Transporteur aérien multitâche
WO2019092471A1 (fr) * 2017-11-13 2019-05-16 Total Sa Procédé de transport d'une charge utile vers un emplacement cible, et dirigeable hybride associé
US11753135B2 (en) 2017-11-13 2023-09-12 Total Sa Method for transporting a payload to a target location, and related hybrid airship

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AT521768B1 (de) 2020-07-15
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DE112012001360B4 (de) 2021-12-23
WO2012135876A3 (fr) 2013-03-28

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