SU1709690A1 - Vertical take-off and landing flying vehicle - Google Patents

Vertical take-off and landing flying vehicle

Info

Publication number
SU1709690A1
SU1709690A1 SU4676351/23A SU4676351A SU1709690A1 SU 1709690 A1 SU1709690 A1 SU 1709690A1 SU 4676351/23 A SU4676351/23 A SU 4676351/23A SU 4676351 A SU4676351 A SU 4676351A SU 1709690 A1 SU1709690 A1 SU 1709690A1
Authority
SU
USSR - Soviet Union
Prior art keywords
wing
flying vehicle
vertical take
sectors
air
Prior art date
Application number
SU4676351/23A
Other languages
Russian (ru)
Inventor
И.А. Ганган
А.М. Гусаковский
В.Н. Журавлев
М.А. Коваль
В.Н. Носик
В.И. Холявко
Original Assignee
Харьковский авиационный институт им.Н.Е.Жуковского
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 Харьковский авиационный институт им.Н.Е.Жуковского filed Critical Харьковский авиационный институт им.Н.Е.Жуковского
Priority to SU4676351/23A priority Critical patent/SU1709690A1/en
Application granted granted Critical
Publication of SU1709690A1 publication Critical patent/SU1709690A1/en

Links

Landscapes

  • Jet Pumps And Other Pumps (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)

Abstract

FIELD: aeronautical engineering. SUBSTANCE: vertical take-off and landing flying vehicle has wing 1 made in form of round biconvex disk, central radial slotted nozzle 2 connected with air-jet engine 4 by means of pipe line 3 which is provided with bypass valve 5. Arranged in nose portion of wing 1 is pilot cabin 6 and deflectable sectors are mounted over periphery of wing 1. Sectors are mounted on axles and brackets and turn with the aid of hydraulic cylinders. Air-jet engine 4 is mounted on vertical tail 11 above upper surface of wing 1. EFFECT: enhanced aerodynamic efficiency in cruising flight conditions. 4 dwg
SU4676351/23A 1989-04-11 1989-04-11 Vertical take-off and landing flying vehicle SU1709690A1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
SU4676351/23A SU1709690A1 (en) 1989-04-11 1989-04-11 Vertical take-off and landing flying vehicle

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
SU4676351/23A SU1709690A1 (en) 1989-04-11 1989-04-11 Vertical take-off and landing flying vehicle

Publications (1)

Publication Number Publication Date
SU1709690A1 true SU1709690A1 (en) 1996-04-10

Family

ID=60532221

Family Applications (1)

Application Number Title Priority Date Filing Date
SU4676351/23A SU1709690A1 (en) 1989-04-11 1989-04-11 Vertical take-off and landing flying vehicle

Country Status (1)

Country Link
SU (1) SU1709690A1 (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2493053C1 (en) * 2012-02-27 2013-09-20 Андрей Вячеславович Канунников Aircraft
RU2531432C2 (en) * 2012-12-04 2014-10-20 Александр Владимирович Амброжевич Development of vtol aircraft drive forces and aircraft to this end
MD4387C1 (en) * 2014-09-23 2016-07-31 Ион КОРОБЧАНУ Vertical takeoff and landing device for aircrafts (embodiments)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2493053C1 (en) * 2012-02-27 2013-09-20 Андрей Вячеславович Канунников Aircraft
RU2531432C2 (en) * 2012-12-04 2014-10-20 Александр Владимирович Амброжевич Development of vtol aircraft drive forces and aircraft to this end
MD4387C1 (en) * 2014-09-23 2016-07-31 Ион КОРОБЧАНУ Vertical takeoff and landing device for aircrafts (embodiments)

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