HUP9802787A1 - Flying equipment with radial gas cells positioned around self weight compensating rotating wing. - Google Patents

Flying equipment with radial gas cells positioned around self weight compensating rotating wing.

Info

Publication number
HUP9802787A1
HUP9802787A1 HU9802787A HUP9802787A HUP9802787A1 HU P9802787 A1 HUP9802787 A1 HU P9802787A1 HU 9802787 A HU9802787 A HU 9802787A HU P9802787 A HUP9802787 A HU P9802787A HU P9802787 A1 HUP9802787 A1 HU P9802787A1
Authority
HU
Hungary
Prior art keywords
gas cells
positioned around
self weight
around self
rotating wing
Prior art date
Application number
HU9802787A
Other languages
Hungarian (hu)
Inventor
Gábor Fazakas
Original Assignee
Gábor Fazakas
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 Gábor Fazakas filed Critical Gábor Fazakas
Priority to HU9802787A priority Critical patent/HUP9802787A1/en
Publication of HU9802787D0 publication Critical patent/HU9802787D0/en
Priority to AU15786/00A priority patent/AU1578600A/en
Priority to PCT/HU1999/000091 priority patent/WO2000032469A1/en
Publication of HUP9802787A1 publication Critical patent/HUP9802787A1/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
    • 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
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C27/00—Rotorcraft; Rotors peculiar thereto
    • B64C27/20—Rotorcraft characterised by having shrouded rotors, e.g. flying platforms

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Testing Of Balance (AREA)
  • Magnetic Bearings And Hydrostatic Bearings (AREA)

Abstract

A találmány arra a célra szőlgáló repülőszerkezet, hőgy légi útőnextrém nagyságrendű terheket emeljenek és szállítsanak. A szükségesemelőerőt a tömegközéppőntban elhelyezett főrgószárnyak állítják elő.A főrgószárny körül elhelyezett, példáűl héliűmmal töltött, gázcellákfelhajtóereje a repülőszerkezet önsúlyával tart egyensúlyt. Aszállítőtt terhet a tömegközéppőnt alatt elhelyezett főgókészülékilletve kőnténer hőrdőzza. A teher emelését a főrgószárnyakőn ébredőszükséges mértékű felhajtóerő végzi. A főrgószárnyak (1) ahajtóműtartó vázőn (3) és a tangenciális küllőn (4) keresztül a gyűrűstartóhőz (5) kapcsőlódva, arról sűgárirányban kiindűló alakőskerettartók (8) közé főgőtt gázcellákkal (13) egy repülőegységetalkőtnak. Az állandó jellegű stabilizáló nyőmatékőt főlyadékgirőszkóp(7) biztősítja. ŕThe invention is a flying structure designed for that purpose, to lift and transport loads of extremely large sizes. The necessary lifting force is produced by the rotor blades located at the center of mass. The buoyancy of the gas cells placed around the rotor blade, for example filled with helium, balances with the self-weight of the aircraft structure. The delivered load is heated by the boiler placed below the center of mass or by the stone counter. The lifting of the load is carried out by the necessary amount of buoyancy on the rotor blade. The rotor blades (1) are connected to the engine support frame (3) and the tangential spoke (4) by the ring support (5), and are heated between the radial frame supports (8) with gas cells (13) of an aircraft unit. The permanent stabilizing pressure is ensured by the main gyroscope (7). ŕ

HU9802787A 1998-12-01 1998-12-01 Flying equipment with radial gas cells positioned around self weight compensating rotating wing. HUP9802787A1 (en)

Priority Applications (3)

Application Number Priority Date Filing Date Title
HU9802787A HUP9802787A1 (en) 1998-12-01 1998-12-01 Flying equipment with radial gas cells positioned around self weight compensating rotating wing.
AU15786/00A AU1578600A (en) 1998-12-01 1999-11-29 Hybrid toroidal airship
PCT/HU1999/000091 WO2000032469A1 (en) 1998-12-01 1999-11-29 Hybrid toroidal airship

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
HU9802787A HUP9802787A1 (en) 1998-12-01 1998-12-01 Flying equipment with radial gas cells positioned around self weight compensating rotating wing.

Publications (2)

Publication Number Publication Date
HU9802787D0 HU9802787D0 (en) 1999-01-28
HUP9802787A1 true HUP9802787A1 (en) 2000-09-28

Family

ID=89997457

Family Applications (1)

Application Number Title Priority Date Filing Date
HU9802787A HUP9802787A1 (en) 1998-12-01 1998-12-01 Flying equipment with radial gas cells positioned around self weight compensating rotating wing.

Country Status (3)

Country Link
AU (1) AU1578600A (en)
HU (1) HUP9802787A1 (en)
WO (1) WO2000032469A1 (en)

Families Citing this family (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE10141838C1 (en) * 2001-08-27 2002-11-28 Guenter Osang Air ship has controllable lift produced by rotating blades arranged in the form of a torus between air-permeable annular disks joined together alternately at the inner and outer diameter and producing a flow similar to a vortex ring
FR2831518B1 (en) * 2001-10-30 2004-01-30 Voliris AIRCRAFT TYPE AIRCRAFT WITH AUXILIARY SUPPORT
FR2851224B1 (en) * 2003-02-18 2006-01-13 Andre Dejoux HYBRID AIRCRAFT COMPRISING A TORQUE ALIGNMENT SYSTEM AND A CENTRAL ROTARY VESSEL
US20070102570A1 (en) * 2003-02-24 2007-05-10 Luffman Charles R Aircraft
AT500009A1 (en) * 2003-10-03 2005-10-15 Franz Autherith MISSILES
RU2545147C2 (en) * 2010-05-19 2015-03-27 Михаил Владимирович Гольцев Hybrid aerostatic airborne vehicle
DE102012105803B4 (en) * 2012-06-29 2022-11-03 Dieter Herz vehicle
RU2501709C1 (en) * 2012-12-05 2013-12-20 Лариса Константиновна Бородина Air driven flying vehicle
US10287000B2 (en) * 2014-07-25 2019-05-14 Hyalta Aeronautics, Inc. Hybrid lighter-than-air vehicle
US20180281916A1 (en) * 2014-11-14 2018-10-04 Christopher Betts An improved airship
CN105818954A (en) * 2016-04-13 2016-08-03 林文庆 Spherical unmanned airship based on dual remote control system
WO2021191974A1 (en) * 2020-03-23 2021-09-30 日本電信電話株式会社 Propeller guard and unmanned aerial vehicle
CN115447752A (en) * 2021-06-08 2022-12-09 刘焕章 Flying boat
RU2769036C1 (en) * 2021-12-03 2022-03-28 Федеральное государственное казенное образовательное учреждение высшего образования "Московский пограничный институт Федеральной службы безопасности Российской Федерации" Unmanned aerial vehicle with electric power generation

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3083934A (en) * 1961-10-12 1963-04-02 Edward G Vanderlip Rotary wing aircraft
FR2366989A1 (en) * 1976-06-28 1978-05-05 Nazare Edgard Airship for goods or passengers - has annular gondola supported below toroidal ring which is rotatable about central lift generating propeller
US4023751A (en) * 1976-07-28 1977-05-17 Richard Walter A Flying ship
US4114837A (en) * 1977-03-24 1978-09-19 Skagit Corporation Air transport and lifting vehicle
US4606515A (en) * 1984-05-29 1986-08-19 Hickey John J Hybrid annular airship
AU588312B2 (en) * 1985-05-06 1989-09-14 Hystar Aerospace Development Corporation Air vehicle
GB2229155B (en) * 1989-03-13 1992-06-10 Vladimir Mihajlovic Sky platform
HUP9700713A3 (en) 1997-04-07 1999-12-28 Fazakas Gabor Airship with toroid-shaped gas cell and central rotating wing

Also Published As

Publication number Publication date
HU9802787D0 (en) 1999-01-28
AU1578600A (en) 2000-06-19
WO2000032469A1 (en) 2000-06-08

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