PL444951A1 - Pionowzlot - Google Patents

Pionowzlot

Info

Publication number
PL444951A1
PL444951A1 PL444951A PL44495123A PL444951A1 PL 444951 A1 PL444951 A1 PL 444951A1 PL 444951 A PL444951 A PL 444951A PL 44495123 A PL44495123 A PL 44495123A PL 444951 A1 PL444951 A1 PL 444951A1
Authority
PL
Poland
Prior art keywords
fixed
vertical take
landing aircraft
fuselage
rotors
Prior art date
Application number
PL444951A
Other languages
English (en)
Inventor
Krzysztof Szafran
Łukasz Jeziorek
Original Assignee
Sieć Badawcza Łukasiewicz - Instytut Lotnictwa
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 Sieć Badawcza Łukasiewicz - Instytut Lotnictwa filed Critical Sieć Badawcza Łukasiewicz - Instytut Lotnictwa
Priority to PL444951A priority Critical patent/PL444951A1/pl
Publication of PL444951A1 publication Critical patent/PL444951A1/pl

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
    • B64C29/02—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis vertical when grounded
    • 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
    • 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
    • B64C27/26—Compound rotorcraft, i.e. aircraft using in flight the features of both aeroplane and rotorcraft characterised by provision of fixed wings
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C39/00—Aircraft not otherwise provided for
    • B64C39/06—Aircraft not otherwise provided for having disc- or ring-shaped wings
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C39/00—Aircraft not otherwise provided for
    • B64C39/06—Aircraft not otherwise provided for having disc- or ring-shaped wings
    • B64C39/066—Aircraft not otherwise provided for having disc- or ring-shaped wings having channel wings
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C39/00—Aircraft not otherwise provided for
    • B64C39/06—Aircraft not otherwise provided for having disc- or ring-shaped wings
    • B64C39/068—Aircraft not otherwise provided for having disc- or ring-shaped wings having multiple wings joined at the tips

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Wind Motors (AREA)

Abstract

Przedmiotem zgłoszenia jest pionowzlot zawierający kadłub oraz co najmniej cztery silniki napędowe wyposażone w wirniki o stałych, równoległych osiach obrotu i charakteryzuje się tym, że do kadłuba (2) po jego przeciwległych bokach, zamocowana jest para stałych płatów nośnych (1) za pomocą łączników (4), przy czym każdy ze stałych płatów nośnych (1) stanowi zamknięty pierścień o profilu lotniczym, zawierający co najmniej dwa wsporniki (5), przy czym do każdego wspornika (5) zamocowany jest silnik napędowy (6), wyposażony w wirnik (7), przy czym cięciwa profilu lotniczego, każdego ze stałych płatów nośnych (1) jest zasadniczo równoległa do osi obrotu wirników (7).
PL444951A 2023-05-22 2023-05-22 Pionowzlot PL444951A1 (pl)

Priority Applications (1)

Application Number Priority Date Filing Date Title
PL444951A PL444951A1 (pl) 2023-05-22 2023-05-22 Pionowzlot

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
PL444951A PL444951A1 (pl) 2023-05-22 2023-05-22 Pionowzlot

Publications (1)

Publication Number Publication Date
PL444951A1 true PL444951A1 (pl) 2024-11-25

Family

ID=93609020

Family Applications (1)

Application Number Title Priority Date Filing Date
PL444951A PL444951A1 (pl) 2023-05-22 2023-05-22 Pionowzlot

Country Status (1)

Country Link
PL (1) PL444951A1 (pl)

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20110042509A1 (en) * 2009-08-24 2011-02-24 Bevirt Joeben Lightweight Vertical Take-Off and Landing Aircraft and Flight Control Paradigm Using Thrust Differentials
EP3597528A1 (en) * 2016-07-01 2020-01-22 Bell Helicopter Textron Inc. Aircraft with passenger pod assembly
EP4101757A1 (en) * 2020-02-04 2022-12-14 Subaru Corporation Vertical takeoff and landing aircraft

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20110042509A1 (en) * 2009-08-24 2011-02-24 Bevirt Joeben Lightweight Vertical Take-Off and Landing Aircraft and Flight Control Paradigm Using Thrust Differentials
EP3597528A1 (en) * 2016-07-01 2020-01-22 Bell Helicopter Textron Inc. Aircraft with passenger pod assembly
EP4101757A1 (en) * 2020-02-04 2022-12-14 Subaru Corporation Vertical takeoff and landing aircraft

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