BE1002132A5 - AIRSHIP AEROSTAT. - Google Patents

AIRSHIP AEROSTAT. Download PDF

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Publication number
BE1002132A5
BE1002132A5 BE8701393A BE8701393A BE1002132A5 BE 1002132 A5 BE1002132 A5 BE 1002132A5 BE 8701393 A BE8701393 A BE 8701393A BE 8701393 A BE8701393 A BE 8701393A BE 1002132 A5 BE1002132 A5 BE 1002132A5
Authority
BE
Belgium
Prior art keywords
aerostat
axis
envelope
pivoting
possibly
Prior art date
Application number
BE8701393A
Other languages
French (fr)
Inventor
Michel Yvan Kuzmek
Original Assignee
Brussels Consulting Group S A
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 Brussels Consulting Group S A filed Critical Brussels Consulting Group S A
Priority to BE8701393A priority Critical patent/BE1002132A5/en
Priority to FR8906091A priority patent/FR2630397B1/en
Application granted granted Critical
Publication of BE1002132A5 publication Critical patent/BE1002132A5/en

Links

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
    • B64B1/36—Arrangement of jet reaction apparatus for propulsion or directional control

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Toys (AREA)
  • Arrangement Or Mounting Of Propulsion Units For Vehicles (AREA)

Abstract

Aérostat dirigeable (1) destiné à être utilisé dans un espace délimité (34), comportant une enveloppe (2) qui est gonflée à l'aide d'un gaz et éventuellement au moins un moteur de propulsion (4), ladite enveloppe (2) portant au voisinage d'au moins une (9a) de ses extrémités (9a, 9b), au moins un moteur de manoeuvre dont l'axe (A-A) peut former un angle alpha avec l'axe directionnel (B-B) de l'aérostat, caractérisé en ce que ledit moteur de manoeuvre (10) est monté sur un ensemble (49) orientable dans une direction perpendiculaire à la direction de l'axe de propulsion (B-B) de telle sorte que lorsque ledit moteur de manoeuvre est en service il fait surbir à l'aérostat (1) un pivotement (V) autour d'un axe (C-C) sensiblement vertical, ce pivotement étant éventuellement combiné avec un mouvement de translation vers l'avant, vers l'arrière, vers le haut, vers le bas et/ou latéral.Dirigible aerostat (1) intended to be used in a defined space (34), comprising an envelope (2) which is inflated with the aid of a gas and possibly at least one propulsion engine (4), said envelope (2 ) bearing in the vicinity of at least one (9a) of its ends (9a, 9b), at least one operating motor whose axis (AA) can form an angle alpha with the directional axis (BB) of the aerostat, characterized in that said maneuvering motor (10) is mounted on an assembly (49) orientable in a direction perpendicular to the direction of the propulsion axis (BB) so that when said maneuvering motor is in service it makes the aerostat (1) overturn a pivoting (V) around a substantially vertical axis (CC), this pivoting possibly being combined with a translational movement forwards, backwards, upwards, down and / or sideways.

BE8701393A 1987-12-04 1987-12-04 AIRSHIP AEROSTAT. BE1002132A5 (en)

Priority Applications (2)

Application Number Priority Date Filing Date Title
BE8701393A BE1002132A5 (en) 1987-12-04 1987-12-04 AIRSHIP AEROSTAT.
FR8906091A FR2630397B1 (en) 1987-12-04 1989-05-02 AIRSHIP AEROSTAT

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
BE8701393A BE1002132A5 (en) 1987-12-04 1987-12-04 AIRSHIP AEROSTAT.

Publications (1)

Publication Number Publication Date
BE1002132A5 true BE1002132A5 (en) 1990-07-24

Family

ID=3883007

Family Applications (1)

Application Number Title Priority Date Filing Date
BE8701393A BE1002132A5 (en) 1987-12-04 1987-12-04 AIRSHIP AEROSTAT.

Country Status (2)

Country Link
BE (1) BE1002132A5 (en)
FR (1) FR2630397B1 (en)

Families Citing this family (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH04169397A (en) * 1990-10-31 1992-06-17 Sosuke Omiya Airship
JP2928771B1 (en) * 1998-01-28 1999-08-03 株式会社電通テック Captive balloon
CA2856901C (en) 2006-10-20 2017-08-29 Lta Corporation Lenticular airship
US8297550B2 (en) 2007-08-09 2012-10-30 Lta Corporation Lenticular airship and associated controls
US8894002B2 (en) 2010-07-20 2014-11-25 Lta Corporation System and method for solar-powered airship
USD670638S1 (en) 2010-07-20 2012-11-13 Lta Corporation Airship
CA2830799A1 (en) 2011-03-31 2012-10-04 Lta Corporation Airship including aerodynamic, floatation, and deployable structures
AU2014377667A1 (en) 2013-11-04 2016-05-19 Lta Corporation Cargo airship
RU2578911C1 (en) * 2014-11-18 2016-03-27 Анатолий Тимофеевич Кожанов Aircraft

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR1434544A (en) * 1965-04-15 1966-04-08 Device forming a movable toy in air or the like and its various applications
FR2250670A1 (en) * 1973-11-09 1975-06-06 Commissariat Energie Atomique Three point undercarriage for dirigible balloon - has front steering and driving wheel or float forming anchoring device
US4402475A (en) * 1978-10-19 1983-09-06 Airships International, Inc. Thrusters for airship control

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR1434544A (en) * 1965-04-15 1966-04-08 Device forming a movable toy in air or the like and its various applications
FR2250670A1 (en) * 1973-11-09 1975-06-06 Commissariat Energie Atomique Three point undercarriage for dirigible balloon - has front steering and driving wheel or float forming anchoring device
US4402475A (en) * 1978-10-19 1983-09-06 Airships International, Inc. Thrusters for airship control

Also Published As

Publication number Publication date
FR2630397A1 (en) 1989-10-27
FR2630397B1 (en) 1993-06-18

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Legal Events

Date Code Title Description
RE Patent lapsed

Effective date: 20031231