SU541426A3 - Крыло дл летательного аппарата - Google Patents

Крыло дл летательного аппарата

Info

Publication number
SU541426A3
SU541426A3 SU2058063A SU2058063A SU541426A3 SU 541426 A3 SU541426 A3 SU 541426A3 SU 2058063 A SU2058063 A SU 2058063A SU 2058063 A SU2058063 A SU 2058063A SU 541426 A3 SU541426 A3 SU 541426A3
Authority
SU
USSR - Soviet Union
Prior art keywords
aircraft wing
wing
aircraft
ftis
flaps
Prior art date
Application number
SU2058063A
Other languages
English (en)
Inventor
Майкл Петрашка Эдвард
Original Assignee
Роквелл Интернэшнл Корпорейшн (Фирма)
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 Роквелл Интернэшнл Корпорейшн (Фирма) filed Critical Роквелл Интернэшнл Корпорейшн (Фирма)
Application granted granted Critical
Publication of SU541426A3 publication Critical patent/SU541426A3/ru

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
    • B64C29/0041—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 jet motors

Description

менным отклонением обоих закрылков осуществл етс  управление на переходных режимах полета.

Claims (1)

1. Патент 1960.
ftiS.S
,/
SU2058063A 1973-09-05 1974-09-04 Крыло дл летательного аппарата SU541426A3 (ru)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US394581A US3860200A (en) 1973-09-05 1973-09-05 Airfoil

Publications (1)

Publication Number Publication Date
SU541426A3 true SU541426A3 (ru) 1976-12-30

Family

ID=23559560

Family Applications (1)

Application Number Title Priority Date Filing Date
SU2058063A SU541426A3 (ru) 1973-09-05 1974-09-04 Крыло дл летательного аппарата

Country Status (12)

Country Link
US (1) US3860200A (ru)
JP (1) JPS5526038B2 (ru)
BR (1) BR7407400D0 (ru)
CA (1) CA998376A (ru)
DE (1) DE2442036A1 (ru)
ES (1) ES429779A1 (ru)
FR (1) FR2242293B1 (ru)
GB (1) GB1468549A (ru)
IL (1) IL45349A (ru)
IT (1) IT1018972B (ru)
SE (1) SE412734B (ru)
SU (1) SU541426A3 (ru)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2630270C2 (ru) * 2016-02-09 2017-09-06 Степан Валентинович Суворов Самолет вертикального взлета и посадки

Families Citing this family (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5062588A (en) * 1989-02-08 1991-11-05 Boeing Of Canada Ltd. Segmented rotatable nozzles
US5076512A (en) * 1989-02-08 1991-12-31 Boeing Canada Ltd. Ventral segmented nozzles for promoting rapid temperature and pressure decay
US5697468A (en) * 1994-10-04 1997-12-16 Flarecraft Corporation Spoiler system for ground effect vehicles
US7802756B2 (en) 2000-02-14 2010-09-28 Aerovironment Inc. Aircraft control system
GB2397809A (en) * 2002-12-21 2004-08-04 Richard Cyril Adkins V/STOL aircraft with an ejector for providing vertical lift
FR2873096B1 (fr) * 2004-07-15 2007-11-23 Airbus France Sas Avion multimoteur
US7837141B2 (en) * 2006-03-22 2010-11-23 The Boeing Company Reaction drive rotor/wing variable area nozzle
DE102009010150B4 (de) * 2009-02-23 2013-09-19 Airbus Operations Gmbh System und Verfahren zur Notbelüftung einer Flugzeugkabine
US9573690B2 (en) * 2011-09-06 2017-02-21 Honeywell International Inc. Thrust recovery outflow valve with a single bi-fold door and method of controlling aircraft cabin pressure
US8998132B2 (en) * 2011-11-30 2015-04-07 Lockheed Martin Corporation Aerodynamic wing load distribution control
KR101287624B1 (ko) 2013-02-25 2013-07-23 주식회사 네스앤텍 착륙이 용이한 무인비행체
EP3363732B1 (en) * 2015-09-02 2020-10-14 Jetoptera, Inc. Ejector and airfoil configurations
USD868627S1 (en) 2018-04-27 2019-12-03 Jetoptera, Inc. Flying car
US10464668B2 (en) 2015-09-02 2019-11-05 Jetoptera, Inc. Configuration for vertical take-off and landing system for aerial vehicles
WO2019062256A1 (zh) * 2017-09-29 2019-04-04 清华大学 一种基于倾转涵道的单升力涵道垂直起降飞机
CN109911180A (zh) * 2019-04-15 2019-06-21 重庆恩斯特龙通用航空技术研究院有限公司 一种轻型飞机襟翼操纵装置

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
NL110393C (ru) * 1955-11-29 1965-01-15 Bertin & Cie
US3045947A (en) * 1959-04-24 1962-07-24 Bertin & Cie Ejectors, particularly for producing lift in aircraft
FR94023E (fr) * 1967-05-24 1969-06-20 Bertin & Cie Systeme sustentateur ou propulso sustentateur pour aéronefs.
US3664611A (en) * 1969-12-17 1972-05-23 Flight Dynamics Res Aerodynamic vehicle

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2630270C2 (ru) * 2016-02-09 2017-09-06 Степан Валентинович Суворов Самолет вертикального взлета и посадки

Also Published As

Publication number Publication date
ES429779A1 (es) 1976-08-16
FR2242293A1 (ru) 1975-03-28
DE2442036A1 (de) 1975-04-10
IT1018972B (it) 1977-10-20
CA998376A (en) 1976-10-12
BR7407400D0 (pt) 1975-07-08
AU7159474A (en) 1976-01-29
FR2242293B1 (ru) 1979-10-12
SE412734B (sv) 1980-03-17
SE7411190L (ru) 1975-03-06
IL45349A (en) 1980-02-29
GB1468549A (en) 1977-03-30
US3860200A (en) 1975-01-14
IL45349A0 (en) 1976-07-30
JPS5526038B2 (ru) 1980-07-10
JPS5054100A (ru) 1975-05-13

Similar Documents

Publication Publication Date Title
SU541426A3 (ru) Крыло дл летательного аппарата
SE395427B (sv) Flygvinge avsedd spec for ett nachtal mellan 0,7 och 1,0
CA961826A (en) Composite aerodynamic blade with twin-beam spar
IL38206A (en) Resilient connections system for the blade of a rotary wing aircraft
BR7404147D0 (pt) Meio de acionamento posicionador de numero de rotacoes regulado com comando
FR2346214A1 (fr) Aile d'aeronef a profil aerodynamique variable
FR2323577A1 (fr) Aile supersonique a ecoulement par remontee
CA1020531A (en) Synthetic aircraft turbine oil
SE406928B (sv) Bindemedel baserat pa en pullulanester och/eller pullulanester samt forfarande for framstellning av bindemedlet
CA930671A (en) Axial flow turbine structure
FR2139004A1 (fr) Cockpit pour simulateur d'avion.
CA947743A (en) Rotary wing aircraft with folding rotor blades
BE809947A (fr) Pneus d'avions
FI56693B (fi) Saett vid sammanlimning av trae eller en traefiberprodukt samt en av polyvinylklorid och cellulosapulver bestaoende blandprodukt
BE792688A (fr) Perfectionnements aux systemes de rotors d'helicopteres
SU445200A3 (ru) Жесткая втулка воздушного винта изменяемого шага несущего винта вертолета
CA980331A (en) Synthetic aircraft turbine oil
CH557189A (de) Modellflugzeug.
SU566028A1 (ru) Дроссельный делитель поток
FR2101001A1 (fr) Aile d'avion
SU343538A1 (ru) Крыло самолета изменяемой в полете геометрии
CA986319A (en) Gas turbine engine for subsonic flight
Starkey et al. Design and development of the xv-5 a v/stol aircraft and its pneumatically-coupled lift-fan propulsion system
AU477166B2 (en) Synthetic aircraft turbine oil
BE799270A (fr) Simulateurs de vol d'aeronefs,