MD4387C1 - Vertical takeoff and landing device for aircrafts (embodiments) - Google Patents

Vertical takeoff and landing device for aircrafts (embodiments)

Info

Publication number
MD4387C1
MD4387C1 MDA20140106A MD20140106A MD4387C1 MD 4387 C1 MD4387 C1 MD 4387C1 MD A20140106 A MDA20140106 A MD A20140106A MD 20140106 A MD20140106 A MD 20140106A MD 4387 C1 MD4387 C1 MD 4387C1
Authority
MD
Moldova
Prior art keywords
aircrafts
vertical takeoff
small base
uniformly
landing device
Prior art date
Application number
MDA20140106A
Other languages
Romanian (ro)
Russian (ru)
Other versions
MD4387B1 (en
Inventor
Ион КОРОБЧАНУ
Виорел КОРОБЧАНУ
Виктор КОРОБЧАНУ
Original Assignee
Ион КОРОБЧАНУ
Виорел КОРОБЧАНУ
Виктор КОРОБЧАНУ
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 Ион КОРОБЧАНУ, Виорел КОРОБЧАНУ, Виктор КОРОБЧАНУ filed Critical Ион КОРОБЧАНУ
Priority to MDA20140106A priority Critical patent/MD4387C1/en
Publication of MD4387B1 publication Critical patent/MD4387B1/en
Publication of MD4387C1 publication Critical patent/MD4387C1/en

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Abstract

The invention relates to the aircraft engineering, in particular to vertical takeoff and landing devices for aircrafts.The vertical takeoff and landing device for aircrafts, according to the first embodiment, comprises a frame (1), made in the shape of a truncated cone with a small base oriented downward relative to the plane of the aircraft. In the region of the small base tangentially, uniformly, in a helical line, at an angle relative to the longitudinal axis are installed energy sources, made in the form of jet engines (2). On the inner surface of the frame (1), above the energy sources, uniformly, in a helical line are installed blades (3), made with an aerodynamic contour, the aerodynamic planes of which are oriented at an angle of attack to the air flow. According to the second embodiment, in the region of the small base there are installed an energy source made in the form of an internal combustion engine and a centrifugal propeller.
MDA20140106A 2014-09-23 2014-09-23 Vertical takeoff and landing device for aircrafts (embodiments) MD4387C1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
MDA20140106A MD4387C1 (en) 2014-09-23 2014-09-23 Vertical takeoff and landing device for aircrafts (embodiments)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
MDA20140106A MD4387C1 (en) 2014-09-23 2014-09-23 Vertical takeoff and landing device for aircrafts (embodiments)

Publications (2)

Publication Number Publication Date
MD4387B1 MD4387B1 (en) 2015-12-31
MD4387C1 true MD4387C1 (en) 2016-07-31

Family

ID=55068707

Family Applications (1)

Application Number Title Priority Date Filing Date
MDA20140106A MD4387C1 (en) 2014-09-23 2014-09-23 Vertical takeoff and landing device for aircrafts (embodiments)

Country Status (1)

Country Link
MD (1) MD4387C1 (en)

Citations (18)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2547266A (en) * 1947-10-02 1951-04-03 Irving M Hoglin Fluid-jet-sustained aircraft
US2944762A (en) * 1955-12-12 1960-07-12 Thompson Ramo Wooldridge Inc Aircraft
US3073109A (en) * 1948-12-29 1963-01-15 Curtiss Wright Corp Supersonic diffuser and control therefor
GB948067A (en) * 1959-10-16 1964-01-29 Bertin & Cie Improvements in fluid-flow diffusers and apparatus embodying such diffusers
GB1190774A (en) * 1967-04-05 1970-05-06 Rolls Royce Improvements relating to the Silencing of Gas Turbine Engines
US3604663A (en) * 1969-07-15 1971-09-14 Custer Channel Wing Corp Jet engine thrust enhancer
US3697020A (en) * 1970-09-14 1972-10-10 Chandler Evans Inc Vertical lift machine
US3831884A (en) * 1973-02-27 1974-08-27 W Schellin Methods and device for generating lift
US4117992A (en) * 1976-10-28 1978-10-03 Vrana Charles K Vertical lift device
FR2619354A1 (en) * 1987-08-11 1989-02-17 Bernadat Georges Vertical take-off and landing aircraft
RU2005660C1 (en) * 1992-04-10 1994-01-15 Сергей Федорович Брагин Device for creating lift force in vertical take-off and landing aircraft
SU1709690A1 (en) * 1989-04-11 1996-04-10 Харьковский авиационный институт им.Н.Е.Жуковского Vertical take-off and landing flying vehicle
RU2182670C2 (en) * 1996-03-28 2002-05-20 Дзе Боинг Компани Air intake of internal compression supersonic engine
US6666403B1 (en) * 2002-02-11 2003-12-23 Robert E. Follensbee Force-producing apparatus
RU2347089C1 (en) * 2007-06-13 2009-02-20 Институт теоретической и прикладной механики им. С.А. Христиановича СО РАН (ИТПМ СО РАН) Supersonic axisymmetric air intake (versions)
CN102493894A (en) * 2011-11-18 2012-06-13 南京航空航天大学 Nozzle exhaust mixing method and device based on pneumatic tab technique
US20130177392A1 (en) * 2009-08-11 2013-07-11 Northrop Grumman Corporation Aircraft Airflow Modulation System and Method
US20140127001A1 (en) * 2011-06-01 2014-05-08 Rolls-Royce Deutschland Ltd & Co Kg Gas-turbine engine with a telescopic air inlet in the engine lining

Patent Citations (18)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2547266A (en) * 1947-10-02 1951-04-03 Irving M Hoglin Fluid-jet-sustained aircraft
US3073109A (en) * 1948-12-29 1963-01-15 Curtiss Wright Corp Supersonic diffuser and control therefor
US2944762A (en) * 1955-12-12 1960-07-12 Thompson Ramo Wooldridge Inc Aircraft
GB948067A (en) * 1959-10-16 1964-01-29 Bertin & Cie Improvements in fluid-flow diffusers and apparatus embodying such diffusers
GB1190774A (en) * 1967-04-05 1970-05-06 Rolls Royce Improvements relating to the Silencing of Gas Turbine Engines
US3604663A (en) * 1969-07-15 1971-09-14 Custer Channel Wing Corp Jet engine thrust enhancer
US3697020A (en) * 1970-09-14 1972-10-10 Chandler Evans Inc Vertical lift machine
US3831884A (en) * 1973-02-27 1974-08-27 W Schellin Methods and device for generating lift
US4117992A (en) * 1976-10-28 1978-10-03 Vrana Charles K Vertical lift device
FR2619354A1 (en) * 1987-08-11 1989-02-17 Bernadat Georges Vertical take-off and landing aircraft
SU1709690A1 (en) * 1989-04-11 1996-04-10 Харьковский авиационный институт им.Н.Е.Жуковского Vertical take-off and landing flying vehicle
RU2005660C1 (en) * 1992-04-10 1994-01-15 Сергей Федорович Брагин Device for creating lift force in vertical take-off and landing aircraft
RU2182670C2 (en) * 1996-03-28 2002-05-20 Дзе Боинг Компани Air intake of internal compression supersonic engine
US6666403B1 (en) * 2002-02-11 2003-12-23 Robert E. Follensbee Force-producing apparatus
RU2347089C1 (en) * 2007-06-13 2009-02-20 Институт теоретической и прикладной механики им. С.А. Христиановича СО РАН (ИТПМ СО РАН) Supersonic axisymmetric air intake (versions)
US20130177392A1 (en) * 2009-08-11 2013-07-11 Northrop Grumman Corporation Aircraft Airflow Modulation System and Method
US20140127001A1 (en) * 2011-06-01 2014-05-08 Rolls-Royce Deutschland Ltd & Co Kg Gas-turbine engine with a telescopic air inlet in the engine lining
CN102493894A (en) * 2011-11-18 2012-06-13 南京航空航天大学 Nozzle exhaust mixing method and device based on pneumatic tab technique

Also Published As

Publication number Publication date
MD4387B1 (en) 2015-12-31

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Legal Events

Date Code Title Description
FG4A Patent for invention issued
KA4A Patent for invention lapsed due to non-payment of fees (with right of restoration)
MM4A Patent for invention definitely lapsed due to non-payment of fees