EP0872413A2 - Volume flottant utile - Google Patents

Volume flottant utile Download PDF

Info

Publication number
EP0872413A2
EP0872413A2 EP98810136A EP98810136A EP0872413A2 EP 0872413 A2 EP0872413 A2 EP 0872413A2 EP 98810136 A EP98810136 A EP 98810136A EP 98810136 A EP98810136 A EP 98810136A EP 0872413 A2 EP0872413 A2 EP 0872413A2
Authority
EP
European Patent Office
Prior art keywords
balloon
floating
interior
space according
carrier
Prior art date
Legal status (The legal status 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 status listed.)
Granted
Application number
EP98810136A
Other languages
German (de)
English (en)
Other versions
EP0872413B1 (fr
EP0872413A3 (fr
Inventor
Robert HÄFELFINGER
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Individual
Original Assignee
Individual
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 Individual filed Critical Individual
Publication of EP0872413A2 publication Critical patent/EP0872413A2/fr
Publication of EP0872413A3 publication Critical patent/EP0872413A3/fr
Application granted granted Critical
Publication of EP0872413B1 publication Critical patent/EP0872413B1/fr
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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Classifications

    • E—FIXED CONSTRUCTIONS
    • E04—BUILDING
    • E04H—BUILDINGS OR LIKE STRUCTURES FOR PARTICULAR PURPOSES; SWIMMING OR SPLASH BATHS OR POOLS; MASTS; FENCING; TENTS OR CANOPIES, IN GENERAL
    • E04H15/00—Tents or canopies, in general
    • E04H15/20—Tents or canopies, in general inflatable, e.g. shaped, strengthened or supported by fluid pressure
    • E04H15/22—Tents or canopies, in general inflatable, e.g. shaped, strengthened or supported by fluid pressure supported by air pressure inside the tent
    • 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
    • G09F21/08—Mobile visual advertising by aeroplanes, airships, balloons, or kites the advertising matter being arranged on the aircraft
    • G09F21/10—Mobile visual advertising by aeroplanes, airships, balloons, or kites the advertising matter being arranged on the aircraft illuminated

Definitions

  • the present invention relates to a floating Usable space as it is in the preamble of the independent claim 1 is defined.
  • usable space is understood as one unit, the one essentially enclosed, accessible space, in the people present in the room e.g. Screenings of all Art, for example film or slide projections, theater, Musical performances, etc., can be presented or the e.g. also for residential purposes, as a restaurant or for others Can be used.
  • a usable space must be created type mentioned at the beginning, which is stable at low wind strength hovers in the air and a larger one visible from the ground Advertising space and a more usable interior than has a comparable large spherical airship.
  • the essence of the invention is that in a floating Usable space with a carrier balloon filled with carrier gas, in which a walk-in interior is integrated, the carrier balloon is a vertically aligned ellipsoid and the walkable one Interior arranged in the lower part of the carrier balloon is.
  • the vertical orientation of the ellipsoid carrier balloon and the arrangement of the interior in the lower part of the carrier balloon has a stable hovering behavior when there is no wind Episode. Because the gas space above the interior is comparatively is higher than that of a spherical airship the floating useful space according to the invention is either a higher one Grasp payload, or the spherical airship must have a much larger diameter, what with a flatter and therefore not optimal interior is connected. What the advertising space concerns, so is an upright Ellipsoid a larger part of the outer surface from the floor visible than with a ball.
  • the accessible interior space is preferably under excess pressure standing balloon with variable volume, with which the expansion of the carrier gas in higher Flight heights can be compensated.
  • an upgrade can be made of the floating useful space at relatively high flight altitudes, e.g. 1000 m, connected optically for the passengers interesting volume changes of the interior will.
  • the interior is designed as a screening room in which, in addition to projection means to project images onto the inside of a flexible inner balloon cover or inner cover and / or headlights and / or speakers also arranged reclining seats are that the guests a comfortable viewing of the on Projected inner balloon envelope or inner envelope above them Images allowed.
  • the floating utility space advantageously has a lock, entering and exiting the accessible interior while maintaining overpressure in the interior, the lock preferably as a lounge designed for a variety of guests and one or has several viewing windows. Guests can then alternately during a balloon flight as desired enjoy the view, possibly at a catering bar take something and watch the demonstrations inside to bring to mind.
  • a pilot cabin can be arranged below the carrier balloon be hung on the interior or on the lock is, e.g. by means of a ball joint. It is an advantage this pilot cabin is buoyant so that the Place floating utility space on a river or lake can.
  • the envelope of the carrier balloon at least partially from one transparent material. This way the outside the interior can be made visible from the outside, so that the entire floating utility room has an optical offers an interesting impression and on the outside of the Interior advertising can be attached.
  • the floating utility room can be used as a captive balloon be trained in what is fast, safe and with little Personnel expenses related to getting on and off the balloon and loading and unloading of passengers.
  • the floating utility space shown includes a carrier balloon 1 with a partially transparent carrier balloon envelope 11.
  • the carrier balloon 1 is filled with a lifting gas, e.g. non-flammable helium, filled.
  • a lifting gas e.g. non-flammable helium
  • Inside the carrier balloon 1 is an interior 2 in the form of an inner balloon an inner balloon envelope 21 arranged, which at the same time as Usable space and serves as a balloon with which to expand of the carrier gas can be compensated for at higher flight altitudes.
  • the interior 2 is filled with air that is under one is slightly overpressure, using air conditioning comfort for people is guaranteed.
  • Lock 3 is provided with viewing windows 31.
  • a pilot cabin 4 with windows 41 for the pilot is articulated on the lock 3 hung.
  • the floating utility space is attached to the carrier balloon 1 Drive devices 6 driven and controlled.
  • the drive devices 6 can, for example, air nozzles or include electric motors around the floating utility space to rotate or move in one direction.
  • the usable space is here via three pillars on floor 100 supported, only in the present sectional view the two pillars 71 and 72 are visible.
  • the carrier balloon 1 is fixed to the floor 100.
  • A is used to connect the pilot cabin 4 and the lock 3 Ball joint 5, to which a tube 50 connects, through the climbed down from the lock 3 into the pilot cabin 4 can be.
  • a water tank 42 is arranged to hold ballast water serves.
  • the lock designed as a lounge 3 has a catering bar 32.
  • the interior 2 is provided with reclining seats 22, which the guests convenient viewing of the inner balloon envelope 21 images projected above them.
  • a staircase 7 To enter the lock 3 from the outside is a staircase 7, provided that at the same time as a third pillar next to the Legs 71 and 72 are used.
  • the access on the lock side to stairs 7 and 28 are with lock doors 34 and 33, respectively Mistake.
  • Within the tube 50 is a conductor 51 for Descending into the pilot cabin 4 arranged. Means the viewing window 31, catering bar 32 and seats 35 the lock 3 is designed as a lounge.
  • the pilot cabin 4 is in a part 43 for technical Devices and a pilot part 44 with the control device 45 divided.
  • the is floating Usable space designed as a captive balloon. It includes one Carrier balloon 101 with a carrier balloon envelope 111 and ropes 180.
  • the carrier balloon 101 is in turn with a Lifting gas, e.g. non-flammable helium, filled.
  • a Lifting gas e.g. non-flammable helium
  • At the bottom Part of the carrier balloon 101 is through a flexible inner shell 121 an interior 102 separated, the same time serves as a usable space and as a ballonet with which to expand of the carrier gas can be compensated for at higher flight altitudes.
  • the interior 102 filled with air that is under a slight positive pressure, and the interior or balloon volume is electrical powered blower, air lines with valves and a control device adapted to the respective flight altitude.
  • the inner shell 121 is here in three different Positions shown, the three different interior volumes have as a consequence.
  • the floating work space is anchored via a winch 191 attached to the ground or on a raft with winch rope 192, with one at the bottom of the carrier balloon 101 attached nose cone 194 in a conical funnel 193 a coupling 190 with movable holding fingers for locking or release of the nose cone 194 are pulled can.
  • winch 191 the ascent and descent of the floating utility space can be controlled.
  • the floating utility room is anchored with the rope 180.
  • a sliding staircase 107 is used for getting in and out of passengers.

Landscapes

  • Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Architecture (AREA)
  • Theoretical Computer Science (AREA)
  • General Physics & Mathematics (AREA)
  • Marketing (AREA)
  • Business, Economics & Management (AREA)
  • Fluid Mechanics (AREA)
  • Accounting & Taxation (AREA)
  • Civil Engineering (AREA)
  • Structural Engineering (AREA)
  • Toys (AREA)
  • Tents Or Canopies (AREA)
  • Piezo-Electric Or Mechanical Vibrators, Or Delay Or Filter Circuits (AREA)
EP98810136A 1997-03-17 1998-02-19 Volume flottant utile Expired - Lifetime EP0872413B1 (fr)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
CH63297 1997-03-17
CH63297 1997-03-17
CH632/97 1997-03-17

Publications (3)

Publication Number Publication Date
EP0872413A2 true EP0872413A2 (fr) 1998-10-21
EP0872413A3 EP0872413A3 (fr) 2000-04-12
EP0872413B1 EP0872413B1 (fr) 2002-08-28

Family

ID=4191544

Family Applications (1)

Application Number Title Priority Date Filing Date
EP98810136A Expired - Lifetime EP0872413B1 (fr) 1997-03-17 1998-02-19 Volume flottant utile

Country Status (4)

Country Link
US (1) US6116538A (fr)
EP (1) EP0872413B1 (fr)
AT (1) ATE222870T1 (fr)
DE (1) DE59805282D1 (fr)

Families Citing this family (20)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7156342B2 (en) * 2004-09-27 2007-01-02 Ltas Holdings, Llc Systems for actively controlling the aerostatic lift of an airship
US20080035787A1 (en) * 2006-08-08 2008-02-14 Thompson Mark N Lighter-than-air gas handling system and method
US7487936B2 (en) * 2006-10-23 2009-02-10 Ltas Holdings, Llc Buoyancy control system for an airship
US20080179453A1 (en) * 2007-01-26 2008-07-31 Thompson Mark N Modular airship system and method
US8857758B2 (en) 2008-05-15 2014-10-14 King Fahd University Of Petroleum And Minerals Lighter-than-air vehicle for shading
US9845141B2 (en) 2012-12-07 2017-12-19 Raven Industries, Inc. Atmospheric balloon system
US9193480B2 (en) 2012-12-07 2015-11-24 Raven Industries, Inc. High altitude balloon system
US9694910B2 (en) 2013-02-22 2017-07-04 World View Enterprises Inc. Near-space operation systems
US9497392B2 (en) 2014-03-18 2016-11-15 Dennis Jason Stelmack Method of transporting and recording imagery of a plurality of similar objects to near space
US20160221661A1 (en) 2015-02-02 2016-08-04 Derek Lee Bohannon Tendon sleeve for high-altitude balloon and system for making the same
US10787268B2 (en) 2015-03-09 2020-09-29 World View Enterprises Inc. Rigidized assisted opening system for high altitude parafoils
US9834296B1 (en) 2015-05-05 2017-12-05 X Development Llc Ballonet deployment control paneling system
US9540091B1 (en) 2016-02-11 2017-01-10 World View Enterprises Inc. High altitude balloon systems and methods
US10124875B1 (en) 2017-01-09 2018-11-13 World View Enterprises Inc. Continuous multi-chamber super pressure balloon
US10336432B1 (en) 2017-01-09 2019-07-02 World View Enterprises Inc. Lighter than air balloon systems and methods
JP6643417B2 (ja) * 2018-08-02 2020-02-12 Ｈａｐｓモバイル株式会社 システム、制御装置及び軽航空機
JP6663468B1 (ja) * 2018-10-15 2020-03-11 Ｈａｐｓモバイル株式会社 制御装置、プログラム、システム及び制御方法
CN112324237A (zh) * 2019-08-05 2021-02-05 宋智勇 一种悬浮式帐篷或蓬盖
US11084564B1 (en) * 2020-02-03 2021-08-10 Space Perspective Inc. Aerospace vehicle system and method of operation
US20210309358A1 (en) * 2020-04-06 2021-10-07 Workhorse Group Inc. Flying vehicle systems and methods

Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO1992006002A1 (fr) 1990-09-27 1992-04-16 Hakan Colting Ballon dirigeable et procede de controle de vol

Family Cites Families (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US701510A (en) * 1901-12-09 1902-06-03 Peter Samorski Air-ship.
US1078614A (en) * 1912-12-11 1913-11-18 Adolf Donath Aeronautical apparatus.
US1170367A (en) * 1915-04-27 1916-02-01 Lafayette C Van Duzer Airship.
US1430393A (en) * 1921-03-05 1922-09-26 Lynde Carleton John Dirigible
US1478382A (en) * 1921-12-23 1923-12-25 Rochus Max Zu Lynar Pa Chimang Airship
US2707603A (en) * 1952-09-06 1955-05-03 Gen Mills Inc Balloon with rigid fins
US3432122A (en) * 1967-06-19 1969-03-11 Goodyear Aerospace Corp Combination ballonet and dilation system for balloons
US3933326A (en) * 1973-08-09 1976-01-20 Schauffler Peter P Observation/interpretation system
DE3628133A1 (de) * 1986-08-19 1988-02-25 Scheib Artur Sonnenstrahlenenergienutzung durch photovoltaische zellen auf fesselballon
US4762295A (en) * 1986-11-25 1988-08-09 General Electric Company Aerostat structure with conical nose
US4773617A (en) * 1987-03-05 1988-09-27 Mccampbell Burton L Lighter-than-air craft
US5813627A (en) * 1997-03-31 1998-09-29 Huntington; Mary K. Balloon support apparatus for hot air balloon ride

Patent Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO1992006002A1 (fr) 1990-09-27 1992-04-16 Hakan Colting Ballon dirigeable et procede de controle de vol

Also Published As

Publication number Publication date
EP0872413B1 (fr) 2002-08-28
EP0872413A3 (fr) 2000-04-12
ATE222870T1 (de) 2002-09-15
DE59805282D1 (de) 2002-10-02
US6116538A (en) 2000-09-12

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