WO2004074063A1 - Vehicule amphibie a effet de sol a coussin d'air - Google Patents
Vehicule amphibie a effet de sol a coussin d'air Download PDFInfo
- Publication number
- WO2004074063A1 WO2004074063A1 PCT/RU2003/000127 RU0300127W WO2004074063A1 WO 2004074063 A1 WO2004074063 A1 WO 2004074063A1 RU 0300127 W RU0300127 W RU 0300127W WO 2004074063 A1 WO2004074063 A1 WO 2004074063A1
- Authority
- WO
- WIPO (PCT)
- Prior art keywords
- κορπusa
- sοοτveτsτvennο
- κρyla
- amphibian
- seκtsy
- Prior art date
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C39/00—Aircraft not otherwise provided for
- B64C39/08—Aircraft not otherwise provided for having multiple wings
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B60—VEHICLES IN GENERAL
- B60F—VEHICLES FOR USE BOTH ON RAIL AND ON ROAD; AMPHIBIOUS OR LIKE VEHICLES; CONVERTIBLE VEHICLES
- B60F3/00—Amphibious vehicles, i.e. vehicles capable of travelling both on land and on water; Land vehicles capable of travelling under water
- B60F3/003—Parts or details of the vehicle structure; vehicle arrangements not otherwise provided for
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B60—VEHICLES IN GENERAL
- B60V—AIR-CUSHION VEHICLES
- B60V3/00—Land vehicles, waterborne vessels, or aircraft, adapted or modified to travel on air cushions
- B60V3/08—Aircraft, e.g. air-cushion alighting-gear therefor
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C35/00—Flying-boats; Seaplanes
- B64C35/008—Amphibious sea planes
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C39/00—Aircraft not otherwise provided for
- B64C39/04—Aircraft not otherwise provided for having multiple fuselages or tail booms
Definitions
- the unit is known to be available on the territory of the Russian Federation 205 ° 2057040; g ⁇ - ⁇ iz ⁇ n ⁇ aln ⁇ y ⁇ d ⁇ ln ⁇ y ⁇ si gib ⁇ ie gaz ⁇ ne ⁇ nitsaemye tsilind ⁇ iches ⁇ ie s ⁇ egi- ⁇ lav ⁇ i as, naduvny ⁇ zlas ⁇ ichny ⁇ ⁇ nevm ⁇ ball ⁇ n ⁇ v, us ⁇ an ⁇ vlen- nye on ⁇ il ⁇ na ⁇ ⁇ yag ⁇ vye dviga ⁇ eli with za ⁇ lyuchennymi in ⁇ ltsevye ⁇ b ⁇ ymy v ⁇ zdushnymi ⁇ ulsivnymi vin ⁇ ami, EA ⁇ ymi ⁇ ⁇ du movement ⁇ az- mescheny na ⁇ l ⁇ nnye in ve ⁇ i ⁇ aln ⁇ y ⁇ l ⁇
- ⁇ ed ⁇ s ⁇ a ⁇ ami e ⁇ g ⁇ e ⁇ an ⁇ lana yavlyae ⁇ sya nev ⁇ zm ⁇ zhn ⁇ s ⁇ is ⁇ lz ⁇ - Bani ⁇ i eg ⁇ s ⁇ zdanii ⁇ ns ⁇ u ⁇ ivny ⁇ elemen ⁇ v e ⁇ s ⁇ lua ⁇ i ⁇ uemy ⁇ sve ⁇ ⁇ yazhely ⁇ ⁇ ans ⁇ ny ⁇ sam ⁇ le ⁇ v (m ⁇ duley and ⁇ e ⁇ n ⁇ l ⁇ gy ⁇ n- ⁇ n- 124 or 225), ⁇ es ⁇ snizi ⁇ za ⁇ a ⁇ y on eg ⁇ s ⁇ uzhenie and e ⁇ s ⁇ lua ⁇ atsiyu ⁇ s ⁇ av- pared with anal ⁇ gichnymi za ⁇ a ⁇ ami on m ⁇ s ⁇ ie ⁇ ans ⁇ nye s ⁇ eds ⁇ va and m ⁇ s ⁇ ie
- ⁇ ed ⁇ s ⁇ a ⁇ ami e ⁇ g ⁇ e ⁇ an ⁇ lana - am ⁇ ibii on v ⁇ zdushn ⁇ y ⁇ dush ⁇ e yavlyae ⁇ sya ned ⁇ s ⁇ a ⁇ chnaya g ⁇ uz ⁇ domn ⁇ s ⁇ and nev ⁇ zm ⁇ zhn ⁇ s ⁇ is ⁇ lz ⁇ va- Nia ⁇ i eg ⁇ s ⁇ zdanii ⁇ ns ⁇ u ⁇ ivnye elemen ⁇ y z ⁇ s ⁇ lua ⁇ i ⁇ uemy ⁇ sve ⁇ ya- zhely ⁇ ⁇ ans ⁇ ny ⁇ sam ⁇ le ⁇ v (m ⁇ duley and ⁇ e ⁇ n ⁇ l ⁇ gy ⁇ U-204 ⁇ n ⁇ n-124 or-225), ⁇ es ⁇ snizi ⁇ za ⁇ a ⁇ y on eg ⁇ s ⁇ uzheniya and e ⁇ s ⁇ lua ⁇ atsiyu ⁇
- zasl ⁇ n ⁇ a ⁇ a vneshni ⁇ ⁇ ve ⁇ n ⁇ s ⁇ ya ⁇ vy ⁇ u ⁇ ly ⁇ se ⁇ tsy 1 ⁇ usa za ⁇ e ⁇ leny na ⁇ sh ⁇ nnye in ve ⁇ i ⁇ aln ⁇ y ⁇ l ⁇ s ⁇ s ⁇ i ⁇ d ugl ⁇ m is 5 - 15 ° ⁇ d ⁇ lnye ⁇ azha ⁇ elnye ⁇ zy ⁇ i 9.
- ⁇ izhnyaya 4 ⁇ aluba ⁇ e ⁇ a on ⁇ as ⁇ l ⁇ zhennye vd ⁇ l ⁇ d ⁇ lny ⁇ ⁇ sey vy ⁇ u ⁇ ly ⁇ se ⁇ tsy 1 ⁇ - ⁇ ca v ⁇ d ⁇ izmeschayuschi ⁇ s ⁇ eg ⁇ v- ⁇ lav ⁇ v, vy ⁇ lnenny ⁇ of ⁇ sled ⁇ va ⁇ el- n ⁇ sm ⁇ n ⁇ i ⁇ vanny ⁇ s ⁇ ladny ⁇ naduvny ⁇ elas ⁇ ichny ⁇ ⁇ nevm ⁇ ame ⁇ 10.
- Symmetrical left 14 and left 15 modules of the aforementioned supporting arm are laid in a vertical plane at the angle of attack ⁇ , equal to 7 - 8 '.
- the indicated value of the angle ⁇ was selected on the basis of results of blowing dust from heavy guns of heavy airplanes AN-124 or EN-225 and the results of operation.
- Each vertical keystone is comprised of a connected friend and another, which are attached to the upper and lower part of the other 21 or the second part of the second and second part of the 23rd.
- Length I. The aforementioned load carrier and distribution between the auxiliary melts 18 increase the distance ⁇ _ 2 between the total height of sections 1 of the corpus of 2.5–5.2–2.5.
- each inflatable elastomeric pneumatic chamber 10 of the skimmer and the total area of 8 lower part is 14 and the left 15 are lower than the second half of the chas ⁇ ey g ⁇ iz ⁇ n ⁇ aln ⁇ g ⁇ m ⁇ dulya ⁇ e ⁇ eniya ⁇ usa less s ⁇ ve ⁇ s ⁇ venn ⁇ ma ⁇ simaln ⁇ g ⁇ ⁇ e ⁇ echn ⁇ g ⁇ ⁇ azme ⁇ a ⁇ ⁇ azhd ⁇ y vy ⁇ u ⁇ l ⁇ y se ⁇ tsii 1 ⁇ usa and ⁇ l ⁇ schadi 8 ⁇ bottom ⁇ ve ⁇ n ⁇ s ⁇ i e ⁇ ann ⁇ g ⁇ ⁇ yla mal ⁇ g ⁇ s ⁇ ve ⁇ s ⁇ venn ⁇ elongation of 1.2 - 5 and 1.7 -2.4 ⁇ aza.
- P ⁇ Me- ⁇ e reduce ⁇ yagi ⁇ u ⁇ b ⁇ ea ⁇ ivnye ⁇ yag ⁇ vye dviga ⁇ eli 19 and vy ⁇ lyucheniya ⁇ u ⁇ b ⁇ ea ⁇ ivny ⁇ us ⁇ an ⁇ v ⁇ 22 and 24 ⁇ s ⁇ u ⁇ a ⁇ elnaya s ⁇ s ⁇ movement z ⁇ - ⁇ an ⁇ la- na - am ⁇ ibii on v ⁇ zdushn ⁇ y ⁇ dush ⁇ e umenshae ⁇ sya and za ⁇ em, v ⁇ lyu- chiv d ⁇ l-ni ⁇ elny ⁇ d ⁇ ulivayuschy dvizhi ⁇ el, ⁇ susches ⁇ vlyayu ⁇ on mal ⁇ y s ⁇ s ⁇ i manev ⁇ i ⁇ vanie, entrance to ⁇ and ⁇ alichanie.
- N ⁇ YSHL ⁇ YA P ⁇ I ⁇ ⁇ I ⁇ S ⁇ E ⁇ an ⁇ lany - am ⁇ ibii on v ⁇ zdushn ⁇ y ⁇ dush ⁇ e m ⁇ gu ⁇ by ⁇ is ⁇ l- z ⁇ vany in ⁇ aches ⁇ ve s ⁇ s ⁇ ny ⁇ g ⁇ uz ⁇ assazhi ⁇ s ⁇ i ⁇ ⁇ a ⁇ m ⁇ v between m ⁇ s ⁇ i- E ⁇ ami, ⁇ s ⁇ yaschimi d ⁇ ug ⁇ d ⁇ uga on ⁇ ass ⁇ yaniya ⁇ 200 and b ⁇ lee ⁇ il ⁇ -> me ⁇ v, ⁇ ansan ⁇ lan ⁇ iches ⁇ i ⁇ ⁇ n ⁇ eyne ⁇ v ⁇ z ⁇ v or s ⁇ asa ⁇ elny ⁇ or d ⁇ u- gi ⁇ vs ⁇ m ⁇ ga ⁇ elny ⁇ various transport facilities for various purposes.
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Transportation (AREA)
- Mechanical Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Nitrogen And Oxygen Or Sulfur-Condensed Heterocyclic Ring Systems (AREA)
- Toys (AREA)
Abstract
L'invention se rapporte aux équipements d'aviation et notamment aux aéronefs utilisant l'effet de sol. Elle concerne un véhicule amphibie à effet de sol qui comprend une aile porteuse à allongement élevé, avec des modules gauche et droit munis de volets, de flotteurs d'appoint et de propulseurs. Le corps est formé par des sections convexes regroupées en un bloc par des membranes porteuses rigides formant l'aile à effet de sol et limitant le compartiment de marchandises avec membranes porteuses rigides supérieure et inférieure; ces membranes se présentent comme l'enveloppe supérieure convexe et le pont inférieur. Le pont inférieur s'appuie sur les flotteurs disposés le long des axes longitudinaux des parties convexes du corps, qui se présentent sous forme de chambres pneumatiques élastiques et gonflables. Le module horizontal avec des gouvernes de tangage de l'empennage du corps est fait articulé et est constitué dans le plan vertical de parties proue et poupe pivotant dans un plan vertical. Des turbopropulseurs destinés à balayer la couche limite de l'air de la surface supérieure de l'ail à effet de sol, à faible allongement, sont montés dans la partie proue du module horizontal. Des turbopropulseurs d'appoint sont montés dans la partie de poupe du module d'empennage horizontal. Les quilles verticales comportant des gouvernes de direction sont montées l'une après l'autre dans les parties proue et poupe du module horizontal d'empennage, symétriquement par rapport à leur axe longitudinal.
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
RU2003104606 | 2003-02-18 | ||
RU2003104606A RU2211773C1 (ru) | 2003-02-18 | 2003-02-18 | Экраноплан-амфибия на воздушной подушке |
Publications (1)
Publication Number | Publication Date |
---|---|
WO2004074063A1 true WO2004074063A1 (fr) | 2004-09-02 |
Family
ID=29778013
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
PCT/RU2003/000127 WO2004074063A1 (fr) | 2003-02-18 | 2003-03-31 | Vehicule amphibie a effet de sol a coussin d'air |
Country Status (2)
Country | Link |
---|---|
RU (1) | RU2211773C1 (fr) |
WO (1) | WO2004074063A1 (fr) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2010012285A2 (fr) * | 2008-07-28 | 2010-02-04 | Fleck Fitness Concepts Gmbh | Véhicule routier, aquatique et aérien combiné |
RU2471660C2 (ru) * | 2011-02-11 | 2013-01-10 | Общество С Ограниченной Ответственностью "Экранопланостроительное Объединение "Орион" | Экраноплан |
CN109592033A (zh) * | 2018-12-17 | 2019-04-09 | 深圳市中科金朗产业研究院有限公司 | 一种带自适应气垫的地效翼船 |
Families Citing this family (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
RU2546357C2 (ru) * | 2013-08-20 | 2015-04-10 | Открытое акционерное общество "Государственный научно-исследовательский навигационно-гидрографический институт" (ОАО "ГНИНГИ") | Спасательный экраноплан |
RU2646776C2 (ru) * | 2014-02-18 | 2018-03-07 | Владимир Петрович Толстоухов | Экраноплан |
RU2563096C1 (ru) * | 2014-08-25 | 2015-09-20 | Юлия Алексеевна Щепочкина | Самолет-амфибия |
RU2582196C1 (ru) * | 2014-12-23 | 2016-04-20 | Публичное акционерное Общество "Таганрогский авиационный научно-технический комплекс им. Г.М. Бериева" (ПАО "ТАНТК им. Г.М. Бериева") | Самолет-амфибия |
RU2658545C1 (ru) * | 2017-10-24 | 2018-06-21 | Вячеслав Васильевич Колганов | Экраноплан - носитель транспортных средств |
CN109334976A (zh) * | 2018-10-22 | 2019-02-15 | 中国船舶科学研究中心(中国船舶重工集团公司第七0二研究所) | 一种扇翼推进地效翼船 |
Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3216673A (en) * | 1963-06-06 | 1965-11-09 | Lockheed Aircraft Corp | Winged hull vehicle |
US3768429A (en) * | 1972-03-02 | 1973-10-30 | R Greer | Watercraft |
DE4217374A1 (de) * | 1992-05-26 | 1993-12-02 | Eberhard Bach | Luftfahrzeug, das sich am Boden auf einem Luftkissen schwebend bewegt und in der Luft wie ein Flugzeug fliegt - Aerodynamische Mehrzweck Apparatur, Kurzbezeichnung AMA |
RU2078002C1 (ru) * | 1994-07-22 | 1997-04-27 | Научно-производственная фирма "АМФИКОН" | Экраноплан |
RU2129501C1 (ru) * | 1994-04-15 | 1999-04-27 | Научно-производственная фирма "АМФИКОН" | Экраноплан |
-
2003
- 2003-02-18 RU RU2003104606A patent/RU2211773C1/ru not_active IP Right Cessation
- 2003-03-31 WO PCT/RU2003/000127 patent/WO2004074063A1/fr not_active Application Discontinuation
Patent Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3216673A (en) * | 1963-06-06 | 1965-11-09 | Lockheed Aircraft Corp | Winged hull vehicle |
US3768429A (en) * | 1972-03-02 | 1973-10-30 | R Greer | Watercraft |
DE4217374A1 (de) * | 1992-05-26 | 1993-12-02 | Eberhard Bach | Luftfahrzeug, das sich am Boden auf einem Luftkissen schwebend bewegt und in der Luft wie ein Flugzeug fliegt - Aerodynamische Mehrzweck Apparatur, Kurzbezeichnung AMA |
RU2129501C1 (ru) * | 1994-04-15 | 1999-04-27 | Научно-производственная фирма "АМФИКОН" | Экраноплан |
RU2078002C1 (ru) * | 1994-07-22 | 1997-04-27 | Научно-производственная фирма "АМФИКОН" | Экраноплан |
Cited By (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2010012285A2 (fr) * | 2008-07-28 | 2010-02-04 | Fleck Fitness Concepts Gmbh | Véhicule routier, aquatique et aérien combiné |
WO2010012285A3 (fr) * | 2008-07-28 | 2010-05-27 | Fleck Fitness Concepts Gmbh | Véhicule routier, aquatique et aérien combiné |
CN102137768A (zh) * | 2008-07-28 | 2011-07-27 | 弗莱克健康理念股份有限公司 | 海陆空全能交通工具 |
US9259984B2 (en) | 2008-07-28 | 2016-02-16 | Fleck Future Concepts Gmbh | Combined air, water and road vehicle |
CN102137768B (zh) * | 2008-07-28 | 2016-04-06 | 弗莱克健康理念股份有限公司 | 海陆空全能交通工具 |
EP2303610B1 (fr) * | 2008-07-28 | 2020-01-08 | Fleck Future Concepts GmbH | Véhicule routier, aquatique et aérien combiné |
RU2471660C2 (ru) * | 2011-02-11 | 2013-01-10 | Общество С Ограниченной Ответственностью "Экранопланостроительное Объединение "Орион" | Экраноплан |
CN109592033A (zh) * | 2018-12-17 | 2019-04-09 | 深圳市中科金朗产业研究院有限公司 | 一种带自适应气垫的地效翼船 |
Also Published As
Publication number | Publication date |
---|---|
RU2211773C1 (ru) | 2003-09-10 |
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