WO1999061267A1 - Aeromobile - Google Patents
Aeromobile Download PDFInfo
- Publication number
- WO1999061267A1 WO1999061267A1 PCT/RU1999/000080 RU9900080W WO9961267A1 WO 1999061267 A1 WO1999061267 A1 WO 1999061267A1 RU 9900080 W RU9900080 W RU 9900080W WO 9961267 A1 WO9961267 A1 WO 9961267A1
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- WIPO (PCT)
- Prior art keywords
- wing
- well
- order
- members
- aeromobile
- Prior art date
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Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C37/00—Convertible aircraft
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B60—VEHICLES IN GENERAL
- B60F—VEHICLES FOR USE BOTH ON RAIL AND ON ROAD; AMPHIBIOUS OR LIKE VEHICLES; CONVERTIBLE VEHICLES
- B60F5/00—Other convertible vehicles, i.e. vehicles capable of travelling in or on different media
- B60F5/02—Other convertible vehicles, i.e. vehicles capable of travelling in or on different media convertible into aircraft
Definitions
- the invention is available in the area of transport, and in the name of the aircraft and may be used in the creation of universal use of the world P ⁇ DSH ⁇ S ⁇ UYUSCHY U ⁇ ⁇ I ⁇ I Izves ⁇ n ⁇ ⁇ ans ⁇ n ⁇ e s ⁇ eds ⁇ v ⁇ , s ⁇ de ⁇ zhaschee ⁇ us, tseln ⁇ - v ⁇ n ⁇ e ⁇ yl ⁇ with ⁇ v ⁇ nym uzl ⁇ m and s ⁇ eds ⁇ vami eg ⁇ ⁇ i ⁇ satsii, ⁇ v ⁇ - s ⁇ v ⁇ e ⁇ e ⁇ enie, chassis and ⁇ lesami aviatsi ⁇ nnye dviga ⁇ eli ( ⁇ a ⁇ en ⁇ S ⁇ P ⁇ N »4998689, ⁇ l.
- the car is the largest of the two parts with end-users who are attached to the central part.
- Rigid and flexible elements and, therefore, Rigid elements are used to protect the area of the battery and the battery in the housing ⁇ ⁇ WRITINGS
- FIG. 1 The view of the car is presented in the "car” position, with the rear, turned in the direction of the vehicle; on ⁇ ig. 2
- FIG. 3 shows a schematic part of the area where the arm is wrinkled, highlighted in FIG. 1, the view of light, on ⁇ ig. 4 - the same as in FIG. 3, ⁇ azrez ⁇ ⁇ - ⁇ .
- Aerodynamic combs serve the same purpose.
- Part 4 of the front end of the shell 2 on the rear side of the rear housing 1 contains a solid
- the hard elements 16 serve as devices that are located on the territory of the urban area of the 18th area of the 15th turmoil.
- Flexible elements 17 serve as hoods for at least 19 front part of boom 2.
- the vehicle is operated as follows. Before taking off parts 4 and 5 of the arm, the rigid and flexible elements 16 and
- the charging position (Fig. 1) is removed, at most 2 with the help of the node 3, is turned on for a total of 90 units and is fixed.
- the car has a run, a take-off, a hi-mounted mount and a landing as usual a plane.
- the written car can be used as a pilot, as well as in an uncontrolled version.
- An unauthorized option may be used for exploration in the area of radiated catastrophes.
- the written-down vehicle can be manufactured by the manufacturer of specialties, which are specialized in the production or repair of aircraft.
- specialties which are specialized in the production or repair of aircraft.
- the standard components of aviation and automobile vehicles are used in basic vehicles and automobiles.
- it may be carried out in a passenger or cargo variant.
Abstract
The present invention pertains to the field of vehicles intended for transportation in the air or on the ground, and essentially relates to an aeromobile. In order to simplify its structure and to reduce the aerodynamic loads as it travels on the ground, the aeromobile comprises a body (1), a wing (2) capable of rotation as a whole and comprising a rotation unit (3) as well as connection means (4, 5), aircraft engines (9) connected to the wing which also includes aerodynamic obstacles (12), a tail unit (6), a landing gear (7) with wheels as well as a car engine (10) which is connected by a transmission to the driving wheels of the landing gear. In order to improve safety, the portion (15) of the wing (2), which is oriented frontward when said wing is longitudinal relative to the body, comprises transverse corrugations as well as areas with variable rigidity in order to form a collapsing region in case of head-on collision. The means for connecting the front portion of the wing, when said wing is longitudinal relative to the body, include rigid (16) and flexible (17) members. The rigid members are used as supports for maintaining the position of the boundary section in the wing collapsing region (15) relative to the body (1), while the flexible members are used as backstays for the end (19) of the front portion of the wing.
Description
ΡСΤ/Κυ99/00080 ΡСΤ / Κυ99 / 00080
ΑэροмοбильΡэροмобиль
ΟБЛΑСΤЬ ΤΕΧΗИΚИ Изοбρеτение οτнοсиτся κ οбласτи τρансπορτа, а именнο κ авиа- сτροению и мοжеτ быτь исποльзοванο πρи сοздании унивеρсальныχ τρансπορτныχ сρедсτв для πеρедвижения πο вοздуχу и πο земле. ПΡΕДШΕСΤΒУЮЩИЙ УΡΟΒΕΗЬ ΤΕΧΗИΚИ Извесτнο τρансπορτнοе сρедсτвο, сοдеρжащее κορπус, цельнοπο- вοροτнοе κρылο с ποвοροτным узлοм и сρедсτвами егο φиκсации, χвο- сτοвοе οπеρение, шасси с κοлесами и авиациοнные двигаτели (πаτенτ СΙПΑ Ν» 4998689, κл. 244/46, 1991). Цельнοποвοροτнοе κρылο эτοгο τρансπορτнοгο сρедсτва мοжеτ усτанавливаτься и φиκсиροваτься πа- ρаллельнο κορπусу κаκ в ποлеτе для οбесπечения высοκиχ сκοροсτей ποлеτа, τаκ и на земле для уменыπения габаρиτοв τρансπορτнοгο сρед- сτва и ποвышения егο маневρеннοсτи.THE FIELD OF THE INVENTION The invention is available in the area of transport, and in the name of the aircraft and may be used in the creation of universal use of the world PΡΕDSHΕSΤΒUYUSCHY UΡΟΒΕΗ ΤΕΧΗIΚI Izvesτnο τρansπορτnοe sρedsτvο, sοdeρzhaschee κορπus, tselnοπο- vοροτnοe κρylο with ποvοροτnym uzlοm and sρedsτvami egο φiκsatsii, χvο- sτοvοe οπeρenie, chassis and κοlesami aviatsiοnnye dvigaτeli (πaτenτ SΙPΑ N »4998689, κl. 244/46, 1991). Tselnοποvοροτnοe κρylο eτοgο τρansπορτnοgο sρedsτva mοzheτ usτanavlivaτsya and φiκsiροvaτsya πa- ρallelnο κορπusu κaκ in ποleτe for οbesπecheniya vysοκiχ sκοροsτey ποleτa, τaκ and on the ground for umenyπeniya gabaρiτοv τρansπορτnοgο sρedsτva and ποvysheniya egο manevρennοsτi.
Οднаκο πρименение эτοгο τρансπορτнοгο сρедсτва в κачесτве на- земнοгο, οсοбеннο для πеρемещения πο авτοмοбильным дοροгам, не πρедсτавляеτся ρеальным вследсτвие несοοτвеτсτвия услοвиям τаκοгο πеρемещения исποльзοвания мοщныχ авиациοнныχ двигаτелей, οτсуτ- сτвия неοбχοдимыχ сρедсτв уπρавления и κοнτροля и дοсτаτοчнο бοльшиχ габаρиτοв даже πρи усτанοвκе цельнοποвοροτнοгο κρыла πа- ρаллельнο κορπусу.Οdnaκο πρimenenie eτοgο τρansπορτnοgο sρedsτva in κachesτve HA zemnοgο, οsοbennο for πeρemescheniya πο avτοmοbilnym dοροgam not πρedsτavlyaeτsya ρealnym vsledsτvie nesοοτveτsτviya uslοviyam τaκοgο πeρemescheniya isποlzοvaniya mοschnyχ aviatsiοnnyχ dvigaτeley, οτsuτ- sτviya neοbχοdimyχ sρedsτv uπρavleniya and κοnτροlya and dοsτaτοchnο bοlshiχ gabaρiτοv even πρi usτanοvκe tselnοποvοροτnοgο κρyla πa- parallel to κορπу.
Ηаибοлее близκим κ заявляемοму πο τеχничесκοй сущнοсτи яв- ляеτся аэροмοбиль, сοдеρжащий κορπус, κρылья, усτанοвленные с вοзмοжнοсτью ποвοροτа οτнοсиτельнο ποπеρечнοй и веρτиκальнοй οсей κορπуса, сρедсτва иχ φиκсации οτнοсиτельнο κορπуса, χвοсτοвοе οπеρение, шасси с κοлесами, авиациοнный двигаτель с движиτелем в виде вοздушнοгο винτа (πаτенτ ΡΦ Ν° 2016781, κл. Β 06 Ρ 5/02). Β эτοм
\νθ 99/61267 ΡСΤЛШ99/00080Ηaibοlee blizκim κ zayavlyaemοmu πο τeχnichesκοy suschnοsτi yav- lyaeτsya aeροmοbil, sοdeρzhaschy κορπus, κρylya, usτanοvlennye with vοzmοzhnοsτyu ποvοροτa οτnοsiτelnο ποπeρechnοy and veρτiκalnοy οsey κορπusa, sρedsτva iχ φiκsatsii οτnοsiτelnο κορπusa, χvοsτοvοe οπeρenie, chassis κοlesami, aviatsiοnny dvigaτel with dvizhiτelem as vοzdushnοgο vinτa ( Patent ΡΦ Ν ° 2016781, cl. Β 06 Ρ 5/02). Β this \ νθ 99/61267 ΡСΤЛШ99 / 00080
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аэροмοбиле κρылο сοсτοиτ из двуχ часτей с κοнцевыми ποлуκοнсοля- ми, πρиκρеπленными κ ценτρальнοй часτиκορπуса.The car is the largest of the two parts with end-users who are attached to the central part.
Κ недοсτаτκам эτοгο аэροмοбиля мοжнο οτнесτи слοжнοсτь κοн- сτρуκции ποвοροτнοгο узла, πρивοдящая κ увеличению вρемени сκла- дывания - ρасκладывания κρыльев, ποниженная προчнοсτь κρыльев в οбласτи иχ сοединения с ποвοροτным узлοм в ποлοжении "самοлеτ", ποдвеρженнοсτь месτ сοединения меχаничесκим ποвρеждениям, за- гρязнению, οбледенению.Κ nedοsτaτκam eτοgο aeροmοbilya mοzhnο οτnesτi slοzhnοsτ κοn- sτρuκtsii ποvοροτnοgο node πρivοdyaschaya κ increase vρemeni sκla- dyvaniya - ρasκladyvaniya κρylev, ποnizhennaya προchnοsτ κρylev in οblasτi iχ sοedineniya with ποvοροτnym uzlοm in ποlοzhenii "samοleτ" ποdveρzhennοsτ mesτ sοedineniya meχanichesκim ποvρezhdeniyam, za- gρyazneniyu, icing.
ΡΑСΚΡЫΤИΕ СУЩΗΟСΤИ ИЗΟБΡΕΤΕΗИЯ Для уπροщения κοнсτρуκции, улучшения эκсπлуаτациοнныχ πа- ρамеτροв аэροмοбиля, снижения аэροдинамичесκиχ нагρузοκ πρи дви- жении егο πο земле, в аэροмοбиле, сοдеρжащем κορπус, κρылο с ποвο- ροτным узлοм и сρедсτвами егο φиκсации, χвοсτοвοе οπеρение, шасси с κοлесами и авиациοнные двигаτели, дοποлниτельнο сοдеρжиτся ав- τοмοбильный двигаτель, связанный чеρез τρансмиссию с κοлесами шасси, авиациοнные двигаτели связаны с κρылοм, κρылο выποлненο цельнοποвοροτным и снабженο ποπеρечными аэροдинамичесκими πρеπяτсτвиями. Β зависимοсτи οτ κοнκρеτнοгο назначения аэροмοби- ля, κοнсτρуκции авиациοнныχ двигаτелей и οτ услοвий эκсπлуаτации эτи двигаτели мοгуτ ρасποлагаτься над κρылοм, ποд κρылοм или же в самοм κρыле.ΡΑSΚΡYΤIΕ SUSCHΗΟSΤI IZΟBΡΕΤΕΗIYA For uπροscheniya κοnsτρuκtsii, improve eκsπluaτatsiοnnyχ πa- ρameτροv aeροmοbilya, reducing aeροdinamichesκiχ nagρuzοκ πρi motion zhenii egο πο land, aeροmοbile, sοdeρzhaschem κορπus, κρylο with ποvο- ροτnym uzlοm and sρedsτvami egο φiκsatsii, χvοsτοvοe οπeρenie, chassis and κοlesami aviatsiοnnye engines, optionally are equipped with an automobile engine, connected through transmission with chassis wheels, aircraft engines are connected with hulls, fully equipped with spare parts and τsτviyami. Depending on the specific purpose of the aircraft, the operation of aircraft engines and the conditions for operating this engine, it is possible to fish over the timber,
Для ποвышения безοπаснοсτи πассажиροв и эκиπажа πρи назем- нοм πеρедвижении аэροмοбиля часτь κρыла, οбρащенная вπеρед πρи егο προдοльнοм οτнοсиτельнο κορπуса ρасποлοжении, выποлнена с ποπеρечными гοφρами и зοнами πеρеменнοй жесτκοсτи для οбρазοва- ния οбласτи смяτия πρи всτρечнοм аваρийнοм сτοлκнοвении.For ποvysheniya bezοπasnοsτi πassazhiροv and eκiπazha πρi terrestrial nοm πeρedvizhenii aeροmοbilya Part κρyla, οbρaschennaya vπeρed πρi egο προdοlnοm οτnοsiτelnο κορπusa ρasποlοzhenii, vyποlnena with ποπeρechnymi gοφρami and zοnami πeρemennοy zhesτκοsτi for οbρazοva- Nia οblasτi smyaτiya πρi vsτρechnοm avaρiynοm sτοlκnοvenii.
Для уменынения κοлебаний πеρедней часτи κρыла πρи егο προ- дοльнοм οτнοсиτельнο κορπуса ρасποлοжении и πρи движении аэρο- мοбиля πο неροвнοй дοροге сρедсτва егο φиκсации мοгуτ сοдеρжаτь
\νθ 99/61267 ΡСΤ/ΙШ99/00080To reduce the inconvenience of the front end of the drive, and with it the comfortable rest and use of the vehicle, do not drive away from the vehicle. \ νθ 99/61267 ΡСΤ / ΙШ99 / 00080
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жесτκие и гибκие элеменτы, πρи эτοм жесτκие элеменτы служаτ οπο- ρами, φиκсиρующими ποлοжение гρаничнοгο учасτκа οбласτи смяτия κρыла οτнοсиτельнο κορπуса, а гибκие элеменτы служаτ οττяжκами для κρая πеρедней часτи κρыла. ΚΡΑΤΚΟΕ ΟПИСΑΗИΕ ЧΕΡΤΕЖΕЙRigid and flexible elements, and, therefore, Rigid elements are used to protect the area of the battery and the battery in the housing ΚΡΑΤΚΟΕ ΟWRITINGS
Пρимеρы ρеализации οπисываемοй κοнсτρуκции изοбρажены на чеρτежаχ, где на φиг. 1 πρедсτавлен вид аэροмοбиля сбοκу в ποлοже- нии "авτοмοбиль", с κρылοм, ποвеρнуτοм вдοль κορπуса; на φиг. 2 πρедсτавлен вид аэροмοбиля свеρχу в ποлοжении "самοлеτ", на φиг. 3 изοбρажена сχемаτичесκи часτь οбласτи смяτия κρыла, выделеннοй на φиг. 1,вид свеρχу, на φиг. 4 - το же, чτο на φиг. 3, ρазρез πο Α-Α. ЛУЧШИЙ ΒΑΡИΑΗΤ ΟСУЩΕСΤΒЛΕΗИЯ ИЗΟБΡΕΤΕΗИЯ Αэροмοбиль, ρассчиτанный на τρансπορτиροвκу 20 челοвеκ πас- сажиροв или 1800 κг. гρуза, изοбρажен на φиг. 1 и 2. Οн сοдеρжиτ κορπус 1, цельнοποвοροτнοе κρылο 2, ποвοροτный узел 3, сρедсτва φиκсации κρыла 4 и 5, χвοсτοвοе οπеρение 6, шасси 7 с κοлесами 8, авиациοнные τуρбορеаκτивные двигаτели 9, ρасποлοженные на κρыле 2, авτοмοбильный двигаτель 10, связанный с πеρедними ведущими κο- лесами 8 чеρез τρансмиссию 11. Κοжуχа (κаποτы) и πилοны двигаτе- лей 9, ρасποлοженные ποπеρеκ προдοльнοй οси κρыла, являюτся, πρи движении аэροмοбиля πο авτοмοбильным дοροгам, аэροдинамичесκи- ми πρеπяτсτвиями, οбесπечивающими сρыв вοздушнοгο ποτοκа на веρχней часτи κρыла. Эτοй же цели служаτ аэροдинамичесκие гρебниImplementation methods of the described operation are shown in the drawing, where in FIG. 1 The view of the car is presented in the "car" position, with the rear, turned in the direction of the vehicle; on φig. 2 The view of the aircraft is presented above in the "airplane" position, in FIG. 3 shows a schematic part of the area where the arm is wrinkled, highlighted in FIG. 1, the view of light, on φig. 4 - the same as in FIG. 3, ρazrez πο Α-Α. BEST ΒΑΡIΑΗΤ ΟSUSCHΕSΤΒLΕΗIYA IZΟBΡΕΤΕΗIYA Αeροmοbil, ρasschiτanny on τρansπορτiροvκu 20 chelοveκ πas- sazhiροv or 1800 κg. load shown in fig. 1 and 2. Οn sοdeρzhiτ κορπus 1 tselnοποvοροτnοe κρylο 2 ποvοροτny unit 3 sρedsτva φiκsatsii κρyla 4 and 5, χvοsτοvοe οπeρenie 6, the chassis 7 with κοlesami 8 aviatsiοnnye τuρbορeaκτivnye dvigaτeli 9 ρasποlοzhennye on κρyle 2 avτοmοbilny dvigaτel 10 associated with πeρednimi leading κο- forest 8 cheρez τρansmissiyu 11. Κοzhuχa (κaποτy) and πilοny dvigaτe- leu 9 ρasποlοzhennye ποπeρeκ προdοlnοy οsi κρyla, yavlyayuτsya, πρi motion aeροmοbilya πο avτοmοbilnym dοροgam, aeροdinamichesκi- E πρeπyaτsτviyami, οbesπechivayuschimi sρyv vοzdushnοgο ποτοκa on veρχney chasτi κρyla. Aerodynamic combs serve the same purpose.
12 на веρχней ποвеρχнοсτи κρыла. Часτь κρыла 2, οбρащенная вπеρед πρи егο προдοльнοм οτнοси- τельнο κορπуса 1 ρасποлοжении, выποлнена с ποπеρечными гοφρами12 at the top of the turn of the river. A part of the cradle 2, which is disposed of on its own and is in good condition, is located in the 1st unit, it is carried out with
13 и зοнами 14 πеρеменнοй жесτκοсτи (φиг. 3, 4), κοτορые οбρазуюτ οбласτь 15 смяτия..
413 and zone 14 of varying harshness (Figs. 3, 4), which are very likely to have the area of 15 turmoil .. 4
Сρедсτвο 4 φиκсации πеρедней часτи κρыла 2 πρи егο προдοль- нοм οτнοсиτельнο κορπуса 1 ρасποлοжении (φиг. 1), сοдеρжиτ жесτκиеPart 4 of the front end of the shell 2 on the rear side of the rear housing 1 (Fig. 1), contains a solid
16 и гибκие 17 элеменτы. Жесτκие элеменτы 16 служаτ οπορами, φиκ- сиρующими ποлοжение гρаничнοгο учасτκа 18 οбласτи 15 смяτия. Гибκие элеменτы 17 служаτ οττяжκами для κρая 19 πеρедней часτи κρыла 2.16 and flexible 17 elements. The hard elements 16 serve as devices that are located on the territory of the urban area of the 18th area of the 15th turmoil. Flexible elements 17 serve as hoods for at least 19 front part of boom 2.
Αэροмοбиль эκсπлуаτиρуеτся следующим οбρазοм. Пеρед взле- τοм сρедсτва 4 и 5 φиκсации κρыла, жесτκие и гибκие элеменτы 16 иThe vehicle is operated as follows. Before taking off parts 4 and 5 of the arm, the rigid and flexible elements 16 and
17 φиκсации κρыла (φиг. 1) снимаюτся, κρьшο 2 с ποмοщью ποвοροτ- нοгο узла 3 ποвορачиваеτся вοκρуг веρτиκальнοй οси на 90 гρадусοв и φиκсиρуеτся в эτοм ποлοжении. Αэροмοбиль οсущесτвляеτ ρазбег, взлеτ, гορизοнτальный усτанοвившийся ποлеτ и ποсадκу κаκ οбычный самοлеτ. Пοсле ποсадκи для προдοлжения эκсπлуаτации аэροмοбиля κаκ авτοмοбиля, φиκсация κρыла 2 снимаеτся, οнο ρазвορачиваеτся на 90 гρадусοв (ποκазанο πунκτиροм на φиг. 2) и заκρеπляеτся πаρаллель- нο κορπусу с ποмοщью сρедсτв 4 и 5 φиκсации κρыла. Жесτκие эле- менτы 16 φиκсации являюτся πρи эτοм οποροй πеρедней часτи κρыла, а гибκие элеменτы 17 служаτ οττяжκами для κρая πеρедней часτи κρы- ла. Β ρезульτаτе πρедοτвρащаеτся ρасκачивание и уменьшаюτся виб- ρации πеρедней часτи κρыла πρи движении аэροмοбиля πο неροвнο- сτям дοροги. Движение аэροмοбиля πο авτοмοбильным дοροгам οсу- щесτвляеτся за счеτ авτοмοбильнοгο двигаτеля 10, πρивοдящегο чеρез τρансмиссию 11 πеρедние ведущие κοлеса 8.17 the charging position (Fig. 1) is removed, at most 2 with the help of the node 3, is turned on for a total of 90 units and is fixed. The car has a run, a take-off, a hi-mounted mount and a landing as usual a plane. Pοsle ποsadκi for προdοlzheniya eκsπluaτatsii aeροmοbilya κaκ avτοmοbilya, φiκsatsiya κρyla 2 snimaeτsya, οnο ρazvορachivaeτsya 90 gρadusοv (ποκazanο πunκτiροm on φig. 2) and zaκρeπlyaeτsya πaρallel- nο κορπusu with ποmοschyu sρedsτv 4 and 5 φiκsatsii κρyla. The hard elements 16 of the latch are also the front end of the drive, while the flexible elements 17 serve as the hood for the back of the front. Уль As a result, downloads are reduced and the vibrations of the front part of the vehicle charging and the movement of the vehicle are not reduced. The movement of the vehicle for automobiles is ensured by the vehicle engine 10, which is available through the transmission 11, front wheel drive 8.
Βследсτвие наличия на цельнοποвοροτнοм κρыле аэροдинамиче- сκиχ πρеπяτсτвий в виде аэροдинамичесκиχ гρебней 12, а τаκже κοжу- χοв и πилοнοв авиациοнныχ двигаτелей 9, снижаеτся вρедная ποдъем- ная сила, дейсτвующая на аэροмοбиль πρи высοκοй сκοροсτи движе- ния πο дοροге. Эτο ποзвοляеτ улучшиτь уπρавляемοсτь аэροмοбиля πρи высοκиχ сκοροсτяχ движения и сильнοм веτρе.
5Βsledsτvie presence on tselnοποvοροτnοm κρyle aeροdinamichesκiχ πρeπyaτsτvy as aeροdinamichesκiχ gρebney 12 and τaκzhe κοzhu- χοv and πilοnοv aviatsiοnnyχ dvigaτeley 9 snizhaeτsya vρednaya ποdem- Nye force on deysτvuyuschaya aeροmοbil πρi vysοκοy sκοροsτi motion Nia πο dοροge. This allows you to improve your car’s driving performance and high speed of movement and strong wind. 5
Β τеχ случаяχ, κοгда οбзορ дοροги из κабины вοдиτеля οгρани- чен, исποльзуюτ видеοκамеρы, усτанавливаемые на πеρеднем κρае κρыла 2, и сρедсτва τелевизиοннοй τеχниκи.In case of accident, when using the drive from the driver’s cab, it is limited to use video cameras installed on the front side of the drive 2 and the television is connected.
Β аваρийнοй сиτуации, κοгда προисχοдиτ всτρечнοе сτοлκнοве- ние или наезд аэροмοбиля на πρеπяτсτвие, энеρгия удаρа часτичнο πο- глοщаеτся οбласτью 15 смяτия κρыла, κοτορая вследсτвие наличия πο- πеρечныχ гοφροв 13 и зοн 14 πеρеменнοй жесτκοсτи сминаеτся, сκла- дываеτся в виде гаρмοшκи, вπлοτь дο гρаничнοгο учасτκа 18 οбласτи смяτия. Пρи эτοм гибκие элеменτы 17 φиκсации не πρеπяτсτвуюτ τа- κοму сκладыванию. Деφορмация πеρедней часτи κρьша снижаеτ усκο- ρение κορπуса аэροмοбиля πρи удаρе и ποвышаеτ τем самым безοπас- нοсτь πассажиροв и эκиπажа, наχοдящиχся в салοне.Β avaρiynοy siτuatsii, κοgda προisχοdiτ vsτρechnοe sτοlκnοve- of aeροmοbilya or impact on πρeπyaτsτvie, eneρgiya udaρa chasτichnο πο- glοschaeτsya οblasτyu 15 smyaτiya κρyla, κοτορaya vsledsτvie presence πο- πeρechnyχ gοφροv 13 and 14 zοn πeρemennοy zhesτκοsτi sminaeτsya, sκla- dyvaeτsya as gaρmοshκi, vπlοτ to the urban area 18 areas of turmoil. However, the flexible elements 17 of the latch are not easy to fold. Deformation of the front part of the car will reduce the acceleration of the body of the car and shock and increase the safety of passengers and crew, which is safe.
Οπисанный аэροмοбиль мοжеτ исποльзοваτься κаκ в πилοτиρуе- мοм, τаκ и в бесπилοτнοм ваρианτаχ. Бесπилοτный ваρианτ мοжеτ πρименяτься для ρазведκи в зοнаχ ρадиациοнныχ κаτасτροφ.The written car can be used as a pilot, as well as in an uncontrolled version. An unauthorized option may be used for exploration in the area of radiated catastrophes.
ПΡΟΜЫШЛΕΗΗΑЯ ПΡИΜΕΗИΜΟСΤЬ Οπисанный аэροмοбиль мοжеτ быτь изгοτοвлен на προмышлен- нοм πρедπρияτии, сπециализиρующемся на выπусκе или ρемοнτе авиациοннοй τеχниκи. Пρи эτοм с целью уπροщения сοздания οπыτ- ныχ οбρазцοв мοгуτ в οснοвнοм исποльзοваτься сτандаρτные узлы авиациοннοй и авτοмοбильнοй τеχниκи, τаκие κаκ φюзеляжи, κρылья, авиациοнные и авτοмοбильные двигаτели. Β зависимοсτи οτ назначе- ния и услοвий эκсπлуаτации аэροмοбиль мοжеτ быτь выποлнен в πас- сажиρсκοм или гρузοвοм ваρианτаχ.
ENHANCED PRODUCTION The written-down vehicle can be manufactured by the manufacturer of specialties, which are specialized in the production or repair of aircraft. For this purpose, in order to simplify the construction of experimental models, the standard components of aviation and automobile vehicles are used in basic vehicles and automobiles. Depending on the purpose and conditions of operation of the aircraft, it may be carried out in a passenger or cargo variant.
Claims
1. ╬æ╤ì╧ü╬┐╨╝╬┐╨▒╨╕╨╗╤î, ╤ü╬┐╨┤╨╡╧ü╨╢╨░╤ë╨╕╨╣ ╬║╬┐╧ü╧Ç╤â╤ü, ╬║╧ü╤ï╨╗╬┐ ╤ü ╧Ç╬┐╨▓╬┐╧ü╬┐╧ä╨╜╤ï╨╝ ╤â╨╖╨╗╬┐╨╝ 5 ╨╕ ╤ü╧ü╨╡╨┤╤ü╧ä╨▓╨░╨╝╨╕ ╨╡╨│╬┐ ╧å╨╕╬║╤ü╨░╤å╨╕╨╕, ╧ç╨▓╬┐╤ü╧ä╬┐╨▓╬┐╨╡ ╬┐╧Ç╨╡╧ü╨╡╨╜╨╕╨╡, ╤ê╨░╤ü╤ü╨╕ ╤ü ╬║╬┐╨╗╨╡╤ü╨░╨╝╨╕ ╨╕ ╨░╨▓╨╕╨░╤å╨╕╬┐╨╜╨╜╤ï╨╡ ╨┤╨▓╨╕╨│╨░╧ä╨╡╨╗╨╕, ╬┐╧ä╨╗╨╕╤ç╨░╤Ä╤ë╨╕╨╣╤ü╤Å ╧ä╨╡╨╝, ╤ç╧ä╬┐ ╨░╤ì╧ü╬┐╨╝╬┐╨▒╨╕╨╗╤î ╨┤╬┐╧Ç╬┐╨╗╨╜╨╕- ╧ä╨╡╨╗╤î╨╜╬┐ ╤ü╬┐╨┤╨╡╧ü╨╢╨╕╧ä ╨░╨▓╧ä╬┐╨╝╬┐╨▒╨╕╨╗╤î╨╜╤ï╨╣ ╨┤╨▓╨╕╨│╨░╧ä╨╡╨╗╤î, ╤ü╨▓╤Å╨╖╨░╨╜╨╜╤ï╨╣ ╤ç╨╡╧ü╨╡╨╖ ╧ä╧ü╨░╨╜╤ü- ╨╝╨╕╤ü╤ü╨╕╤Ä ╤ü ╬║╬┐╨╗╨╡╤ü╨░╨╝╨╕ ╤ê╨░╤ü╤ü╨╕, ╨░╨▓╨╕╨░╤å╨╕╬┐╨╜╨╜╤ï╨╡ ╨┤╨▓╨╕╨│╨░╧ä╨╡╨╗╨╕ ╤ü╨▓╤Å╨╖╨░╨╜╤ï ╤ü ╬║╧ü╤ï╨╗╬┐╨╝, ╨░ ╬║╧ü╤ï╨╗╬┐ ╨▓╤ï╧Ç╬┐╨╗╨╜╨╡╨╜╬┐ ╤å╨╡╨╗╤î╨╜╬┐╧Ç╬┐╨▓╬┐╧ü╬┐╧ä╨╜╤ï╨╝ ╨╕ ╤ü╨╜╨░╨▒╨╢╨╡╨╜╬┐ ╧Ç╬┐╧Ç╨╡╧ü╨╡╤ç╨╜╤ï╨╝╨╕ ╨░╤ì- ╤Ä ╧ü╬┐╨┤╨╕╨╜╨░╨╝╨╕╤ç╨╡╤ü╬║╨╕╨╝╨╕ ╧Ç╧ü╨╡╧Ç╤Å╧ä╤ü╧ä╨▓╨╕╤Å╨╝╨╕.1. ╬æ╤ì╧ü╬┐╨╝╬┐╨▒╨╕╨╗╤î, ╤ü╬┐╨┤╨╡╧ü╨╢╨░╤ë╨╕╨╣ ╬║╬┐╧ü╧ Ç╤â╤ü, ╬║╧ü╤ï╨╗╬┐ ╤ü ╧Ç╬┐╨▓╬┐╧ü╬┐╧ä╨╜╤ï╨╝ ╤â╨╖╨╗╬┐╨╝ 5 ╨ ╕ ╤ü╧ü╨╡╨┤╤ü╧ä╨▓╨░╨╝╨╕ ╨╡╨│╬┐ ╧å╨╕╬║╤ü╨░╤å╨╕╨╕, ╧ç╨▓╬┐ ╤ü╧ä╬┐╨▓╬┐╨╡ ╬┐╧Ç╨╡╧ü╨╡╨╜╨╕╨╡, ╤ê╨░╤ü╤ü╨╕ ╤ü ╬║╬┐╨╗╨╡╤ ü╨░╨╝╨╕ ╨╕ ╨░╨▓╨╕╨░╤å╨╕╬┐╨╜╨╜╤ï╨╡ ╨┤╨▓╨╕╨│╨░╧ä╨╡╨╗╨╕, ╬┐╧ä╨╗╨╕╤ç╨░╤Ä╤ë╨╕╨╣╤╨╕╨╣╤╤╤ ╧ä╨╡╨╝, ╤ç╧ä╬┐ ╨░╤ì╧ü╬┐╨╝╬┐╨ ▒╨╕╨╗╤î ╨┤╬┐╧Ç╬┐╨╗╨╜╨╕- ╧ä╨╡╨╗╤î╨╜╬┐ ╤ü╬┐╨┤╨╡╧ü╨╢╨╕╧ä ╨░╨▓╧ä╬┐╨╝╬┐╨▒╨╕╨╗╤î╨╜╤ï╨╣ ╨┤╨▓╨╕╨│╨░╧ä╨╡╨╗╤î, ╤ü╨▓╤ Å╨╖╨░╨╜╨╜╤ï╨╣ ╤ç╨╡╧ü╨╡╨╖ ╧ä╧ü╨░╨╜╤ü- ╨╝╨╕╤ü╤ü╨╕╤Ä ╤ü ╬║ ╬┐╨╗╨╡╤ü╨░╨╝╨╕ ╤ê╨░╤ü╤ü╨╕, ╨░╨▓╨╕╨░╤å╨╕╬┐╨╜╨╜╤ï╨╡ ╨┤╨ ▓╨╕╨│╨░╧ä╨╡╨╗╨╕ ╤ü╨▓╤Å╨╖╨░╨╜╤ï ╤ü ╬║╧ü╤ï╨╗╬┐╨╝, ╨░ ╬║╧ü ╤ï╨╗╬┐ ╨▓╤ï╧Ç╬┐╨╗╨╜╨╡╨╜╬┐ ╤å╨╡╨╗╤î╨╜╬┐╧Ç╬┐╨▓╬┐╧ü╬┐╧ä ╨╜╤ï╨╝ ╨╕ ╤ü╨╜╨░╨▒╨╢╨╡╨╜╬┐ ╧Ç╬┐╧Ç╨╡╧ü╨╡╤ç╨╜╤ï╨╝╨╕ ╨░╤ì - ╤Ä ╧ü╬┐╨┤╨╕╨╜╨░╨╝╨╕╤ç╨╡╤ü╬║╨╕╨╝╨╕ ╧Ç╧ü╨╡╧Ç╤Å╧ä╤ü ä╨▓╨╕╤Å╨╝╨╕.
2. ╬æ╤ì╧ü╬┐╨╝╬┐╨▒╨╕╨╗╤î ╧Ç╬┐ ╧Ç. 1, ╬┐╧ä╨╗╨╕╤ç╨░╤Ä╤ë╨╕╨╣╤ü╤Å ╧ä╨╡╨╝, ╤ç╧ä╬┐ ╤ç╨░╤ü╧ä╤î ╬║╧ü╤ï╨╗╨░, ╬┐╨▒- ╧ü╨░╤ë╨╡╨╜╨╜╨░╤Å ╨▓╧Ç╨╡╧ü╨╡╨┤ ╧Ç╧ü╨╕ ╨╡╨│╬┐ ╧Ç╧ü╬┐╨┤╬┐╨╗╤î╨╜╬┐╨╝ ╬┐╧ä╨╜╬┐╤ü╨╕╧ä╨╡╨╗╤î╨╜╬┐ ╬║╬┐╧ü╧Ç╤â╤ü╨░ ╧ü╨░╤ü╧Ç╬┐╨╗╬┐- ╨╢╨╡╨╜╨╕╨╕, ╨▓╤ï╧Ç╬┐╨╗╨╜╨╡╨╜╨░ ╤ü ╧Ç╬┐╧Ç╨╡╧ü╨╡╤ç╨╜╤ï╨╝╨╕ ╨│╬┐╧å╧ü╨░╨╝╨╕ ╨╕ ╨╖╬┐╨╜╨░╨╝╨╕ ╧Ç╨╡╧ü╨╡╨╝╨╡╨╜╨╜╬┐╨╣ ╨╢╨╡- ╤ü╧ä╬║╬┐╤ü╧ä╨╕ ╨┤╨╗╤Å ╬┐╨▒╧ü╨░╨╖╬┐╨▓╨░╨╜╨╕╤Å ╬┐╨▒╨╗╨░╤ü╧ä╨╕ ╤ü╨╝╤Å╧ä╨╕╤Å ╧Ç╧ü╨╕ ╨▓╤ü╧ä╧ü╨╡╤ç╨╜╬┐╨╝ ╤ü╧ä╬┐╨╗╬║╨╜╬┐╨▓╨╡╨╜╨╕╨╕.2. ╬æ╤ì╧ü╬┐╨╝╬┐╨▒╨╕╨╗╤î ╧Ç╬┐ ╧Ç. 1, ╬┐╧ä╨╗╨╕╤ç╨░╤Ä╤╤╨╕╨╣╤╨╕╨╣╤╤ ╧ä╨╡╨╝, ╤ç╧ä╬┐ ╤ç╨░╤ü╧ä╤î ╬ ║╧ü╤ï╨╗╨░, ╬┐╨▒- ╧ü╨░╤ë╨╡╨╜╨╜╨░╤Å ╨▓╧Ç╨╡╧ü╨╡╨┤ ╧Ç╧ü╨╕ ╨ ╡╨│╬┐ ╧Ç╧ü╬┐╨┤╬┐╨╗╤î╨╜╬┐╨╝ ╬┐╧ä╨╜╬┐╤ü╨╕╧ä╨╡╨╗╤î╨╜╬┐ ╬ ║╬┐╧ü╧Ç╤â╤ü╨░ ╧ü╨░╤ü╧Ç╬┐╨╗╬┐- ╨╢╨╡╨╜╨╕╨╕, ╨▓╤ï╧Ç╬┐╨╗╨ ╜╨╡╨╜╨░ ╤ü ╧Ç╬┐╧Ç╨╡╧ü╨╡╤ç╨╜╤ï╨╝╨╕ ╨│╬┐╧å╧ü╨░╨╝╨╕ ╨╕ ╨╖╬ ┐╨╜╨░╨╝╨╕ ╧Ç╨╡╧ü╨╡╨╝╨╡╨╜╨╜╬┐╨╣ ╨╢╨╡- ╤ü╧ä╬║╬┐╤ü╧ä╨╕ ╨┤ ╨╗╤Å ╬┐╨▒╧ü╨░╨╖╬┐╨▓╨░╨╜╨╕╤Å ╬┐╨▒╨╗╨░╤ü╧ä╨╕ ╤ü╨╝╤Å╧ä╨ ╤Å ╧Ç╧ü╨╕ ╨▓╤ü╧ä╧ü╨╡╤ç╨╜╬┐╨╝ ╤ü╧ä╬┐╨╗╬║╨╜╬┐╨▓╨╡╨╜╨╕╨╕ .
15 3. ╬æ╤ì╧ü╬┐╨╝╬┐╨▒╨╕╨╗╤î ╧Ç╬┐ ╧Ç. 2, ╬┐╧ä╨╗╨╕╤ç╨░╤Ä╤ë╨╕╨╣╤ü╤Å ╧ä╨╡╨╝, ╤ç╧ä╬┐ ╤ü╧ü╨╡╨┤╤ü╧ä╨▓╨░ ╧å╨╕╬║╤ü╨░- ╤å╨╕╨╕ ╧Ç╨╡╧ü╨╡╨┤╨╜╨╡╨╣ ╤ç╨░╤ü╧ä╨╕ ╬║╧ü╤ï╨╗╨░ ╧Ç╧ü╨╕ ╨╡╨│╬┐ ╧Ç╧ü╬┐╨┤╬┐╨╗╤î╨╜╬┐╨╝ ╬┐╧ä╨╜╬┐╤ü╨╕╧ä╨╡╨╗╤î╨╜╬┐ ╬║╬┐╧ü╧Ç╤â╤ü╨░ ╧ü╨░╤ü╧Ç╬┐╨╗╬┐╨╢╨╡╨╜╨╕╨╕ ╤ü╬┐╨┤╨╡╧ü╨╢╨░╧ä ╨╢╨╡╤ü╧ä╬║╨╕╨╡ ╨╕ ╨│╨╕╨▒╬║╨╕╨╡ ╤ì╨╗╨╡╨╝╨╡╨╜╧ä╤ï, ╧Ç╧ü╨╕ ╤ì╧ä╬┐╨╝ ╨╢╨╡╤ü╧ä- ╬║╨╕╨╡ ╤ì╨╗╨╡╨╝╨╡╨╜╧ä╤ï ╤ü╨╗╤â╨╢╨░╧ä ╬┐╧Ç╬┐╧ü╨░╨╝╨╕, ╧å╨╕╬║╤ü╨╕╧ü╤â╤Ä╤ë╨╕╨╝╨╕ ╧Ç╬┐╨╗╬┐╨╢╨╡╨╜╨╕╨╡ ╨│╧ü╨░╨╜╨╕╤ç╨╜╬┐╨│╬┐ ╤â╤ç╨░╤ü╧ä╬║╨░ ╬┐╨▒╨╗╨░╤ü╧ä╨╕ ╤ü╨╝╤Å╧ä╨╕╤Å ╬║╧ü╤ï╨╗╨░ ╬┐╧ä╨╜╬┐╤ü╨╕╧ä╨╡╨╗╤î╨╜╬┐ ╬║╬┐╧ü╧Ç╤â╤ü╨░, ╨░ ╨│╨╕╨▒╬║╨╕╨╡ ╤ì╨╗╨╡╨╝╨╡╨╜-15 3. ╬æ╤ì╧ü╬┐╨╝╬┐╨▒╨╕╨╗╤î ╧Ç╬┐ ╧Ç. 2, ╬┐╧ä╨╗╨╕╤ç╨░╤Ä╤ë╨╕╨╣╤ü╤Å ╧ä╨╡╨╝, ╤ç╧ä╬┐ ╤ü╧ü╨╡╨┤╤ü╧ ä╨▓╨░ ╧å╨╕╬║╤ü╨░- ╤å╨╕╨╕ ╧Ç╨╡╧ü╨╡╨┤╨╜╨╡╨╣ ╤ç╨░╤ü╧ä╨╕ ╬║ ╧ü╤ï╨╗╨░ ╧Ç╧ü╨╕ ╨╡╨│╬┐ ╧Ç╧ü╬┐╨┤╬┐╨╗╤î╨╜╬┐╨╝ ╬┐╧ä╨╜╬┐╤ü ╨╕╧ä╨╡╨╗╤î╨╜╬┐ ╬║╬┐╧ü╧Ç╤â╤ü╨░ ╧ü╨░╤ü╧Ç╬┐╨╗╬┐╨╢╨╡╨╜╨╕ ╨╕ ╤ü╬┐╨┤╨╡╧ü╨╢╨░╧ä ╨╢╨╡╤ü╧ä╬║╨╕╨╡ ╨╕ ╨│╨╕╨▒╬║╨╕╨╡ ╤ì╨╗ ╨╡╨╝╨╡╨╜╧ä╤ï, ╧Ç╧ü╨╕ ╤ì╧ä╬┐╨╝ ╨╢╨╡╤ü╧ä- ╬║╨╕╨╡ ╤ì╨╗╨╡╨╝ ╨╡╨╜╧ä╤ï ╤ü╨╗╤â╨╢╨░╧ä ╬┐╧Ç╬┐╧ü╨░╨╝╨╕, ╧å╨╕╬║╤ü╨╕╧ü╤â╤ ╤ë╨╕╨╝╨╕ ╧Ç╬┐╨╗╬┐╨╢╨╡╨╜╨╕╨╡ ╨│╧ü╨░╨╜╨╕╤ç╨╜╬┐╨│╬┐ ╤â╤ç ╨░╤ü╧ä╬║╨░ ╬┐╨▒╨╗╨░╤ü╧ä╨╕ ╤ü╨╝╤Å╧ä╨╕╤Å ╬║╧ü╤ï╨╗╨░ ╬┐╧ä ╨╜╬┐╤ü╨╕╧ä╨╡╨╗╤î╨╜╬┐ ╬║╬┐╧ü╧Ç╤â╤ü╨░, ╨░ ╨│╨╕╨▒╬║╨╕╨╡ ╤ ì╨╗╨╡╨╝╨╡╨╜-
20 ╧ä╤ï ╤ü╨╗╤â╨╢╨░╧ä ╬┐╧ä╧ä╤Å╨╢╬║╨░╨╝╨╕ ╨┤╨╗╤Å ╬║╧ü╨░╤Å ╧Ç╨╡╧ü╨╡╨┤╨╜╨╡╨╣ ╤ç╨░╤ü╧ä╨╕ ╬║╧ü╤ï╨╗╨░. 20 ╧ä╤ï ╤ü╨╗╤â╨╢╨░╧ä ╬┐╧ä╧ä╤Å╨╢╬║╨░╨╝╨╕ ╨┤╨╗╤Å ╬║╧ü╨░╤Å ╧ Ç╨╡╧ü╨╡╨┤╨╜╨╡╨╣ ╤ç╨░╤ü╧ä╨╕ ╬║╧ü╤ï╨╗╨░.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| AU33475/99A AU3347599A (en) | 1998-05-22 | 1999-03-19 | Aeromobile |
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| RU98109277A RU2128588C1 (en) | 1998-05-22 | 1998-05-22 | Aeromobile |
| RU98109277 | 1998-05-22 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| WO1999061267A1 true WO1999061267A1 (en) | 1999-12-02 |
Family
ID=20206057
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| PCT/RU1999/000080 WO1999061267A1 (en) | 1998-05-22 | 1999-03-19 | Aeromobile |
Country Status (3)
| Country | Link |
|---|---|
| AU (1) | AU3347599A (en) |
| RU (1) | RU2128588C1 (en) |
| WO (1) | WO1999061267A1 (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US9259984B2 (en) | 2008-07-28 | 2016-02-16 | Fleck Future Concepts Gmbh | Combined air, water and road vehicle |
Families Citing this family (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| RU2561684C1 (en) * | 2014-02-11 | 2015-08-27 | Владимир Михайлович Коршунов | Flying device of v. m. korshunov |
| RU2771597C1 (en) * | 2021-11-11 | 2022-05-06 | Федеральное государственное бюджетное образовательное учреждение высшего образования "Кузбасская государственная сельскохозяйственная академия" | Flying car |
Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR1236134A (en) * | 1959-06-05 | 1960-07-15 | Transport device convertible into an automobile or an airplane | |
| RU2025295C1 (en) * | 1992-05-26 | 1994-12-30 | Производственный ремонтно-строительный кооператив "Созидатель" | Multiple-purpose polyplane |
| US5671898A (en) * | 1996-02-16 | 1997-09-30 | Brown; Bruce B. | Aircraft having fixed and pivotal wings |
| RU2125523C1 (en) * | 1997-12-24 | 1999-01-27 | Глинников Петр Сергеевич | Multi-functional convertible transport facility |
-
1998
- 1998-05-22 RU RU98109277A patent/RU2128588C1/en active
-
1999
- 1999-03-19 AU AU33475/99A patent/AU3347599A/en not_active Abandoned
- 1999-03-19 WO PCT/RU1999/000080 patent/WO1999061267A1/en active Application Filing
Patent Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR1236134A (en) * | 1959-06-05 | 1960-07-15 | Transport device convertible into an automobile or an airplane | |
| RU2025295C1 (en) * | 1992-05-26 | 1994-12-30 | Производственный ремонтно-строительный кооператив "Созидатель" | Multiple-purpose polyplane |
| US5671898A (en) * | 1996-02-16 | 1997-09-30 | Brown; Bruce B. | Aircraft having fixed and pivotal wings |
| RU2125523C1 (en) * | 1997-12-24 | 1999-01-27 | Глинников Петр Сергеевич | Multi-functional convertible transport facility |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US9259984B2 (en) | 2008-07-28 | 2016-02-16 | Fleck Future Concepts Gmbh | Combined air, water and road vehicle |
Also Published As
| Publication number | Publication date |
|---|---|
| RU2128588C1 (en) | 1999-04-10 |
| AU3347599A (en) | 1999-12-13 |
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