ES2185145T3 - Aeronave con un fuselaje construido en lo esencial como cuerpo ascensional aerostatico. - Google Patents

Aeronave con un fuselaje construido en lo esencial como cuerpo ascensional aerostatico.

Info

Publication number
ES2185145T3
ES2185145T3 ES98904030T ES98904030T ES2185145T3 ES 2185145 T3 ES2185145 T3 ES 2185145T3 ES 98904030 T ES98904030 T ES 98904030T ES 98904030 T ES98904030 T ES 98904030T ES 2185145 T3 ES2185145 T3 ES 2185145T3
Authority
ES
Spain
Prior art keywords
hull
aerostatic
ascensional
aircraft
fuselage
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.)
Expired - Lifetime
Application number
ES98904030T
Other languages
English (en)
Inventor
Hermann Kunkler
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
Application granted granted Critical
Publication of ES2185145T3 publication Critical patent/ES2185145T3/es
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C29/00—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft
    • B64C29/0008—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded
    • B64C29/0016—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded the lift during taking-off being created by free or ducted propellers or by blowers
    • B64C29/0033—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded the lift during taking-off being created by free or ducted propellers or by blowers the propellers being tiltable relative to the fuselage
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B63—SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
    • B63H—MARINE PROPULSION OR STEERING
    • B63H5/00—Arrangements on vessels of propulsion elements directly acting on water
    • B63H5/07—Arrangements on vessels of propulsion elements directly acting on water of propellers
    • B63H5/125—Arrangements on vessels of propulsion elements directly acting on water of propellers movably mounted with respect to hull, e.g. adjustable in direction, e.g. podded azimuthing thrusters
    • 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
    • B64C—AEROPLANES; HELICOPTERS
    • B64C11/00—Propellers, e.g. of ducted type; Features common to propellers and rotors for rotorcraft
    • B64C11/02—Hub construction
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C27/00—Rotorcraft; Rotors peculiar thereto
    • B64C27/22—Compound rotorcraft, i.e. aircraft using in flight the features of both aeroplane and rotorcraft
    • B64C27/28—Compound rotorcraft, i.e. aircraft using in flight the features of both aeroplane and rotorcraft with forward-propulsion propellers pivotable to act as lifting rotors
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C27/00—Rotorcraft; Rotors peculiar thereto
    • B64C27/52—Tilting of rotor bodily relative to fuselage
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D35/00—Transmitting power from power plants to propellers or rotors; Arrangements of transmissions
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Combustion & Propulsion (AREA)
  • Chemical & Material Sciences (AREA)
  • Ocean & Marine Engineering (AREA)
  • Tires In General (AREA)
  • Toys (AREA)
  • Elimination Of Static Electricity (AREA)
  • Vehicle Cleaning, Maintenance, Repair, Refitting, And Outriggers (AREA)
  • Forklifts And Lifting Vehicles (AREA)
  • Walking Sticks, Umbrellas, And Fans (AREA)
  • Transmission Devices (AREA)
  • Other Liquid Machine Or Engine Such As Wave Power Use (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
  • Handcart (AREA)
  • Fuses (AREA)
  • Fluid-Pressure Circuits (AREA)
  • Motor Power Transmission Devices (AREA)
  • Shafts, Cranks, Connecting Bars, And Related Bearings (AREA)

Abstract

UNA AERONAVE TIENE UN FUSELAJE DISEÑADO PRACTICAMENTE COMO CUERPO AEROSTATICO DE ELEVACION Y DISPOSITIVOS COMBINADOS DE ELEVACION Y PROPULSION UNIDOS AL FUSELAJE, DOTADOS DE HELICES Y QUE FORMAN UNIDADES DE ACCIONAMIENTO QUE PUEDEN BASCULAR ENTRE UNA POSICION DE ELEVACION, EN LA QUE EL PLANO DE ROTACION DE LA HELICE CORRESPONDIENTE SE ENCUENTRA PRACTICAMENTE HORIZONTAL, Y EL EJE ACCIONADO DEL ACCIONAMIENTO ASOCIADO QUE IMPULSA EL EJE DE LA HELICE ES PRACTICAMENTE VERTICAL, Y UNA POSICION DE PROPULSION, EN LA QUE EL PLANO DE ROTACION DE LA HELICE CORRESPONDIENTE ES PRACTICAMENTE VERTICAL Y EL EJE ACCIONADO DEL ACCIONAMIENTO CORRESPONDIENTE QUE IMPULSA EL EJE DE LA HELICE ES PRACTICAMENTE HORIZONTAL. EL PLANO DE ROTACION DE LA HELICE PUEDE GIRAR ALREDEDOR DEL EJE ACCIONADO DEL ACCIONAMIENTO CORRESPONDIENTE QUE IMPULSA EL EJE DE LA HELICE.
ES98904030T 1997-01-04 1998-01-02 Aeronave con un fuselaje construido en lo esencial como cuerpo ascensional aerostatico. Expired - Lifetime ES2185145T3 (es)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE19700182A DE19700182A1 (de) 1997-01-04 1997-01-04 Luftfahrzeug mit einem im wesentlichen als aerostatischem Auftriebskörper ausgebildeten Rumpf

Publications (1)

Publication Number Publication Date
ES2185145T3 true ES2185145T3 (es) 2003-04-16

Family

ID=7816849

Family Applications (1)

Application Number Title Priority Date Filing Date
ES98904030T Expired - Lifetime ES2185145T3 (es) 1997-01-04 1998-01-02 Aeronave con un fuselaje construido en lo esencial como cuerpo ascensional aerostatico.

Country Status (19)

Country Link
US (2) US6286783B1 (es)
EP (2) EP1160156B1 (es)
JP (1) JP2001507306A (es)
CN (2) CN1085973C (es)
AT (2) ATE328787T1 (es)
AU (1) AU717125B2 (es)
BR (1) BR9806838A (es)
CA (1) CA2276876A1 (es)
CZ (1) CZ233299A3 (es)
DE (3) DE19700182A1 (es)
DK (1) DK0948441T3 (es)
ES (1) ES2185145T3 (es)
ID (1) ID21900A (es)
IL (1) IL130655A (es)
PL (1) PL334353A1 (es)
PT (1) PT948441E (es)
RU (1) RU2196703C2 (es)
UA (1) UA49050C2 (es)
WO (1) WO1998029303A2 (es)

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EP1160156B1 (de) 2006-06-07
ID21900A (id) 1999-08-12
CN1085973C (zh) 2002-06-05
UA49050C2 (uk) 2002-09-16
PT948441E (pt) 2003-02-28
EP0948441B1 (de) 2002-10-02
IL130655A (en) 2003-04-10
CN1249720A (zh) 2000-04-05
US6467724B2 (en) 2002-10-22
DE59813586D1 (de) 2006-07-20
CA2276876A1 (en) 1998-07-09
DE19700182A1 (de) 1998-07-09
RU2196703C2 (ru) 2003-01-20
US20020003189A1 (en) 2002-01-10
EP0948441A2 (de) 1999-10-13
EP1160156A3 (de) 2003-05-21
EP1160156A2 (de) 2001-12-05
CZ233299A3 (cs) 1999-12-15
JP2001507306A (ja) 2001-06-05
DE59805790D1 (de) 2002-11-07
CN1123486C (zh) 2003-10-08
WO1998029303A2 (de) 1998-07-09
PL334353A1 (en) 2000-02-28
CN1392083A (zh) 2003-01-22
US6286783B1 (en) 2001-09-11
WO1998029303A3 (de) 1998-11-05
ATE328787T1 (de) 2006-06-15
WO1998029303B1 (de) 1999-10-07
AU717125B2 (en) 2000-03-16
WO1998029303A8 (de) 1999-11-11
DK0948441T3 (da) 2003-02-03
AU6206998A (en) 1998-07-31
IL130655A0 (en) 2000-06-01
ATE225279T1 (de) 2002-10-15
BR9806838A (pt) 2000-03-14

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