SI0948441T1 - Aircraft with a fuselage substantially designed as an aerostatic lifting body - Google Patents

Aircraft with a fuselage substantially designed as an aerostatic lifting body

Info

Publication number
SI0948441T1
SI0948441T1 SI9830294T SI9830294T SI0948441T1 SI 0948441 T1 SI0948441 T1 SI 0948441T1 SI 9830294 T SI9830294 T SI 9830294T SI 9830294 T SI9830294 T SI 9830294T SI 0948441 T1 SI0948441 T1 SI 0948441T1
Authority
SI
Slovenia
Prior art keywords
aircraft
lifting body
substantially designed
fuselage substantially
aerostatic lifting
Prior art date
Application number
SI9830294T
Other languages
Slovenian (sl)
Inventor
Hermann K�NKLER
Original Assignee
Kuenkler Hermann
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
Priority claimed from DE19700182A external-priority patent/DE19700182A1/en
Application filed by Kuenkler Hermann filed Critical Kuenkler Hermann
Publication of SI0948441T1 publication Critical patent/SI0948441T1/en

Links

Classifications

    • 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
    • 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
    • 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
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Ocean & Marine Engineering (AREA)
SI9830294T 1997-01-04 1998-01-02 Aircraft with a fuselage substantially designed as an aerostatic lifting body SI0948441T1 (en)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
DE19700182A DE19700182A1 (en) 1997-01-04 1997-01-04 Aircraft with a fuselage designed essentially as an aerostatic buoyancy body
EP98904030A EP0948441B1 (en) 1997-01-04 1998-01-02 Aircraft with a fuselage substantially designed as an aerostatic lifting body
PCT/EP1998/000015 WO1998029303A2 (en) 1997-01-04 1998-01-02 Aircraft with a fuselage substantially designed as an aerostatic lifting body

Publications (1)

Publication Number Publication Date
SI0948441T1 true SI0948441T1 (en) 2003-04-30

Family

ID=26032964

Family Applications (1)

Application Number Title Priority Date Filing Date
SI9830294T SI0948441T1 (en) 1997-01-04 1998-01-02 Aircraft with a fuselage substantially designed as an aerostatic lifting body

Country Status (1)

Country Link
SI (1) SI0948441T1 (en)

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