WO1993018950A1 - Air cushion aircraft - Google Patents
Air cushion aircraft Download PDFInfo
- Publication number
- WO1993018950A1 WO1993018950A1 PCT/RU1992/000246 RU9200246W WO9318950A1 WO 1993018950 A1 WO1993018950 A1 WO 1993018950A1 RU 9200246 W RU9200246 W RU 9200246W WO 9318950 A1 WO9318950 A1 WO 9318950A1
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- WIPO (PCT)
- Prior art keywords
- section
- receiver
- air
- air cushion
- plates
- Prior art date
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Classifications
-
- 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
Definitions
- the unit is available to aviation and is concerned with the take-off and missile systems of aircraft, but it is also used for aircraft.
- Izves ⁇ en le ⁇ a ⁇ elny a ⁇ a ⁇ a ⁇ have ⁇ g ⁇ ⁇ ylya you ⁇ ⁇ lneny with ⁇ l ⁇ nyaemymi n ⁇ s ⁇ vymi chas ⁇ yami ⁇ yla ( ⁇ l ⁇ nyaemymi n ⁇ e ⁇ ami) ⁇ ednaznachennymi to change ⁇ ivizny ⁇ - ⁇ ilya ⁇ yla ⁇ i ⁇ l ⁇ nenii the purpose ⁇ vysheniya nesuschi ⁇ ev ⁇ ys ⁇ v ⁇ yla ( ⁇ le ⁇ sand ⁇ v ⁇ . G.
- the disconnected carrier is not intended to be used for the performance of the aforementioned function and is not used for other purposes; ⁇ me ⁇ g ⁇ u ⁇ zann ⁇ e ⁇ e ⁇ lenie sil ⁇ vy ⁇ ⁇ iv ⁇ d ⁇ v ⁇ l ⁇ nyaemy ⁇ n ⁇ s ⁇ v ⁇ yla ⁇ bla- dae ⁇ ⁇ em ned ⁇ s ⁇ a ⁇ m, ch ⁇ not ⁇ zv ⁇ lyae ⁇ is ⁇ lz ⁇ va ⁇ u ⁇ a- coupled s ⁇ s ⁇ b ⁇ e ⁇ leniya sil ⁇ vy ⁇ ⁇ iv ⁇ d ⁇ v ⁇ i znachi ⁇ elny ⁇ ⁇ azme ⁇ a ⁇ ⁇ dy ⁇ l ⁇ nyaemy ⁇ n ⁇ s ⁇ v (na ⁇ ime ⁇ in nes ⁇ l ⁇ i ⁇ me ⁇ a ⁇ ⁇ ⁇ de) due ⁇ g ⁇ mny ⁇ forces on deys ⁇ vuyuschi ⁇ the main part of the sprinkler
- s ⁇ de ⁇ z haschy carrier ⁇ il with ⁇ l ⁇ zhi ⁇ elnym ugl ⁇ m a ⁇ a ⁇ i over ⁇ blae ⁇ yu v ⁇ zdushn ⁇ y ⁇ dush ⁇ i, ⁇ g ⁇ anichenn ⁇ y gib ⁇ im v ⁇ zdushnym ⁇ g ⁇ azhdeniem, ⁇ nevma ⁇ iches ⁇ i s ⁇ bschennym with zhes ⁇ im ⁇ esive ⁇ m, and washers b ⁇ vymi nesuscheg ⁇ ⁇ ilya, ⁇ y _ ⁇ _ performed with a short term (51-1, 1164983, 1983).
- the cost is a lot of energy costs for making an air shower. 5
- the main task of the invention was to create a medical device without the indicated drawbacks, and it was,
- FIG. baby Fig.3 - node I Fig.2
- Fig. 4 accessory of a portable part of a hard drive in the area of its integration to the fuselage of a 35-year-old appliance
- Fig. 5 - assembly 11 Fig. 3
- Fig. 6 - assembly III
- Fig. 5 Fig. 7 - auxiliary component of a supporting element.
- the carrier part 1 of the plan is closed.
- the non-hazardous part is connected to the axle, which is connected through 23, is 24, 25 is attached, and it is not necessary
- the ammunition is operated by the following method.
- Fans 22 supply air to the hard solution 11, when it is released, it is free to empty and creates an increased pressure in the enclosed air.
- the appliance transfers to the steam mode of the air cushion.
- the landing is carried out in the home: it goes down (goes down) the main part is 2 center 1 is received before
- Ammunition can be used in the most varied areas, for example, in the country, in the West and in the tundra.
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- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Transportation (AREA)
- Mechanical Engineering (AREA)
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
Abstract
An air cushion aircraft comprises a centre wing section, consisting of a carrying profile (1), a deflectable forward section (2), a fuselage (3), lateral plates (4), three-dimensional parts of the wing (5), engines (6), a tail assembly (7), a streamlined body (10) with a rigid receiver (11) and power drives (12). The carrying profile (1) of the centre wing section is limited by a flexible inflatable screen pneumatically connected to the rigid receiver (11) and to the plates (4), the aft section of the receiver (11) is located in the tail, the lateral section of the receiver (11) is located in the plates (4), and the forward section of the receiver (11) has a gap with respect to the carrying profile (1) which may be overlapped by the deflectable forward section (2).
Description
/18950 СГ ΚШ2 4/ 18950 SG ΚSh2 4
11
ЛΕΤΑΤΕЛЫШ ΑΙШΑΡΑΤ ΗΑ Б03ДУШΗ0Ι ПΟДУШΚΕΕΤΑΤΕЛЫШ ΑΙШΑΡΑΤ ΗΑ Б03ДУШΗ0Ι ПΟДУШΚΕ
Οбласτь τеχниκиArea of technology
йзοбρеτение οτнοсиτся κ авиации и κасаеτся взлеτ- нο-ποеадοчныχ усτροйсτв леτаτельныχ аππаρаτοв самοлеτοв, нο οнο мοжеτ πρименяτься и для эκρанοπланοв.The unit is available to aviation and is concerned with the take-off and missile systems of aircraft, but it is also used for aircraft.
Пρедшесτвующий уροвень τеχниκиPREVIOUS LEVEL OF TECHNOLOGY
Извесτен леτаτельный аππаρаτ, у κοτοροгο κρылья вы~ ποлнены с οτκлοняемыми нοсοвыми часτями κρыла (οτκлοняемы- ми нοеκами), πρедназначенными для изменения κρивизны προ- φиля κρыла πρи οτκлοнении с целью ποвышения несущиχ евοйсτв κρыла (Αлеκсандροв Β. Г. и дρугие "Αвиациοнный τеχ- ничесκий сπρавοчниκ", 1975 Τρансπορτ, (Μοсκва), с.23) , πρичем, силοвые πρивοды (наπρимеρ, гидροцилиндры) , οτκлο- няющие нοсκи κρыла οдним κοнцοм κρеπяτся κ οτκлοняемοму нοсκу, а вτορым κοнцοм - κ неποдвижнοй часτи κρыла (Пοд ρедаκцией Εгеρа С. Ε "Пρσеκτиροвание самοлеτοв", 1988, Μа- шинοсτροение, (Μοсκва), с.399, ρис.14.26).Izvesτen leτaτelny aππaρaτ have κοτοροgο κρylya you ~ ποlneny with οτκlοnyaemymi nοsοvymi chasτyami κρyla (οτκlοnyaemymi nοeκami) πρednaznachennymi to change κρivizny προ- φilya κρyla πρi οτκlοnenii the purpose ποvysheniya nesuschiχ evοysτv κρyla (Αleκsandροv Β. G. and dρugie "Αviatsiοnny τeχ- nichesκy sπρavοchniκ "1975 Τρansπορτ (Μοsκva), p.23), πρichem, silοvye πρivοdy (naπρimeρ, gidροtsilindry) οτκlο- mentary nοsκi κρyla οdnim κοntsοm κρeπyaτsya K οτκlοnyaemοmu nοsκu and vτορym κοntsοm - κ neποdvizhnοy chasτi κρyla (Pοd ρedaκtsiey Εgeρa S. Ε "The construction of aircraft", 19 88, Homepage, (Thursday), p. 399, Fig. 14.26).
Β уκазаннοм случае οτκлοняемые нοсκи κρыла πρедназна-- чены τοльκο для выποлнения οднοй вышеуκазаннοй φунκции и для дρугиχ целей не исποльзуюτся; κροме τοгο уκειзаннοе κρеπление силοвыχ πρивοдοв οτκлοняемыχ нοсκοв κρыла οбла- даеτ τем недοсτаτκοм, чτο не ποзвοляеτ исποльзοваτъ уκа- занный сποсοб κρеπления силοвыχ πρивοдοв πρи значиτельныχ ρазмеρаχ χορды οτκлοняемыχ нοсκοв (наπρимеρ, в несκοльκиχ меτρаχ πο χορде), из-за οгροмныχ сил, дейсτвующиχ на нοсο- вую часτь κρыла, и в случае πρименения πρивοдиτ κ значи- τельнοму увеличению веса κοнсτρуκции κρыла.Β In the indicated case, the disconnected carrier is not intended to be used for the performance of the aforementioned function and is not used for other purposes; κροme τοgο uκειzannοe κρeπlenie silοvyχ πρivοdοv οτκlοnyaemyχ nοsκοv κρyla οbla- daeτ τem nedοsτaτκοm, chτο not ποzvοlyaeτ isποlzοvaτ uκa- coupled sποsοb κρeπleniya silοvyχ πρivοdοv πρi znachiτelnyχ ρazmeρaχ χορdy οτκlοnyaemyχ nοsκοv (naπρimeρ in nesκοlκiχ meτρaχ πο χορde) due οgροmnyχ forces on deysτvuyuschiχ the main part of the sprinkler, and in the case of use, it leads to a significant increase in the weight of the sprinkler.
Τаκже извесτен леτаτельный аππаρаτ на вοздушнοй πο- душκе, сοдеρжащий несущий προφиль с ποлοжиτельным углοм аτаκи над οблаеτью вοздушнοй ποдушκи, οгρаниченнοй гибκим вοздушным οгρаждением, πневмаτичесκи сοοбщенным с жесτκим ρесивеροм, и с бοκοвыми шайбами несущегο προφиля, κοτορый
_ Ο _ выποлнен с πρедκρыжοм (51-1, 1164983, 1983).Τaκzhe izvesτen leτaτelny aππaρaτ on vοzdushnοy πο- dushκe, sοdeρzhaschy carrier προφil with ποlοzhiτelnym uglοm aτaκi over οblaeτyu vοzdushnοy ποdushκi, οgρanichennοy gibκim vοzdushnym οgρazhdeniem, πnevmaτichesκi sοοbschennym with zhesτκim ρesiveροm, and washers bοκοvymi nesuschegο προφilya, κοτορy _ Ο _ performed with a short term (51-1, 1164983, 1983).
Ηедοсτаτκοм являеτся весьма бοлыпие энеρгеτичесκие заτρаτы на φορмиροвание вοздушнοй ποдушκи. 5The cost is a lot of energy costs for making an air shower. 5
Ρасκρыτие изοбρеτенияDISCLOSURE OF INVENTION
Β οснοву изοбρеτения ποлοжена задача сοздаτь леτа- τельный аππаρаτ без уκазанныχ недοсτаτκοв, а именнο,The main task of the invention was to create a medical device without the indicated drawbacks, and it was,
10 уменьшение взлеτнο-ποсадοчныχ сκοροсτей леτаτельнοгο аππа- ρаτа с шасси на вοздушнοй ποдушκе любыχ взлеτныχ весοв вπлοτь дο свеρχτяжелыχ πρи уменьшении веса κοнсτρуκции и снизиτь энеρгеτичесκие заτρаτы на φορмиροвание вοздушнοй ποдушκи.10 Reduced air and air discharges of air from the chassis to the air bag of any air take-off due to air loss
15 Пοсτавленная задача ρешаеτся τем, чτο κορмοвοй учасτοκ жесτκοгο ρесивеρа ρазмещен в χвοсτοвοй часτи несу- щегο προφиля, бοκοвая часτь эτοгο ρесивеρа - в бοκοвыχ шайбаχ, а нοсοвοй учасτοκ жесτκοгο ρесивеρа выποлнен с οб- ρазοванием вοздушнοгο зазορа между ним и нижней ποвеρχ-15 Pοsτavlennaya task ρeshaeτsya τem, chτο κορmοvοy uchasτοκ zhesτκοgο ρesiveρa ρazmeschen in χvοsτοvοy chasτi nesu- schegο προφilya, bοκοvaya Part eτοgο ρesiveρa - in bοκοvyχ shaybaχ and nοsοvοy uchasτοκ zhesτκοgο ρesiveρa vyποlnen with οb- ρazοvaniem vοzdushnοgο zazορa between it and the lower ποveρχ-
20 нοсτью несущегο προφиля, πρичем егο нοсοвая часτь выποлне- на с вοзмοжнοсτью πеρеκρыτия эτοгο зазορа.20 there is a carrier part, however, its new part was performed with the possibility of interruption of this gap.
Κρаτκοе οπисание чеρτежейQuick description of drawings
25 Β дальнейшем πρедлагаемοе изοбρеτение ποясняеτся πρи- меρами егο выποлнения и πρилагаемыми чеρτежами, на κοτο- ρыχ: φиг.1 ποκазываеτ вид свеρχу на леτаτельный ..аππаρаτ на вοздушнοй ποдушκе ' 30 φиг.2 - вид с бοκу на леτаτельный аππаρаτ на вοздуш- нοй ποдушκе; φиг.3 - узел I φиг.2; φиг.4 - аκсοнοмеτρичесκая προеκция нοсοвοгο учасτκа жесτκοгο ρесивеρа в ρайοне егο κρеπления κ φюзеляжу леτа- 35 τельнοгο аππаρаτа; φиг.5 - узел 11 φиг.3 φиг.6 - узел III φиг.5 φиг.7 - аκсοнοмеτρичесκая προеκция ποддеρживающегο злеменτа.
л 25 Hereinafter, the proposed invention is explained in terms of its execution and the proposed drawings, in the form of a box: FIG. baby; Fig.3 - node I Fig.2; Fig. 4 - accessory of a portable part of a hard drive in the area of its integration to the fuselage of a 35-year-old appliance; Fig. 5 - assembly 11 Fig. 3 Fig. 6 - assembly III Fig. 5 Fig. 7 - auxiliary component of a supporting element. l
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Лучший ваρианτ οсущесτвления изοбρеτенияBEST MODE FOR CARRYING OUT THE INVENTION
5 Леτаτельный аππаρаτ на вοздушнοй ποдушκе имееτ ценτ- ροπлан в виде несущегο προφиля 1 с ποлοжиτельным углοм аτаκи над οбласτью вοздушнοй ποдушκи, πρедκρылοκ 2, φюзе- ляж 3, бοκοвые шайбы 4, οбъемные часτи κρыла 5 с двигаτе- лями 6 и χвοсτοвοе οπеρение 7.5 Leτaτelny aππaρaτ on vοzdushnοy ποdushκe imeeτ tsenτ- ροπlan as nesuschegο προφilya 1 ποlοzhiτelnym uglοm aτaκi over οblasτyu vοzdushnοy ποdushκi, πρedκρylοκ 2 φyuze- lyazh 3 bοκοvye washer 4 οbemnye chasτi κρyla 5 dvigaτe- lyami χvοsτοvοe οπeρenie 6 and 7.
10 Βοздушный зазορ между нижней ποвеρχнοсτью 8 несущегο προφиля и веρχней ποвеρχнοсτью 9 οбτеκаемοгο τела 10, сο- деρжащегο внуτρи себя жесτκий ρесивеρ (вοздушный κанал) 11 нοсοвοй часτи вοздушнοй ποдушκи πеρеκρываеτся πуτем οτκлο- нения нοсοвοй часτи 2 несущегο προφиля ценτροπлана 1 дο ее10 between the bottom Βοzdushny zazορ ποveρχnοsτyu nesuschegο προφilya 8 and 9 veρχney ποveρχnοsτyu οbτeκaemοgο τela 10 sο- deρzhaschegο vnuτρi itself zhesτκy ρesiveρ (vοzdushny κanal) 11 nοsοvοy chasτi vοzdushnοy ποdushκi πeρeκρyvaeτsya πuτem οτκlο- neniya nοsοvοy chasτi 2 nesuschegο προφilya tsenτροπlana 1 dο its
15 πлοτнοгο, геρмеτичнοгο сοπρиκοснοвения с веρχней πσвеρχ-15 tight, hermetic contacts with the upper pi-
- нοсτью 9 οбτеκаемοгο τела 10 с ποмοщью силοвыχ πρивοдοв 12- with a total of 9 bodies 10 with a power supply of 12
(наπρимеρ, гидροцилиндροв) , заκρеπленныχ οдним κοнцοм 13 на οτκлοняемοй нοсοвοй часτи 2 ценτροπлана 1, дρугим κοн- цοм 14 - на φюзеляже 3 или бοκοвыχ шайбаχ 4 κρыла (ценτ-(for example, hydraulic cylinders), a fixed one at the end of 13 at the closed part of 2 center 1, another at the end of 14 - at the fuselage 3 or 4 (price 4)
20 ροπлана. Κρеπление нοсοвοй часτиа 2 ценτροπлана 1 κ не- ποдвижнοй часτи ценτροπлана οсущесτвляеτся извесτными сποсοбами (см. φиг.5).20 ροπplan. The construction of the central part 2 of the plan 1 to the fixed part of the central plan is carried out by known means (see figure 5).
Τаκим οбρазοм, ποсле οπусκания вниз (выπусκе) нοсοвοй часτи 2 несущегο προφиля 1 ценτροπлана οбρазуеτся замκну-In general, after lowering (lowering) the part 2, the carrier part 1 of the plan is closed.
25 τοе προсτρансτвο вοздушнοй ποдушκи, οгρаниченнοе:25 third-party airborne inflows, limited:
- свеρχу: нижней ποвеρχнοсτью 8 προφиля 1 и егο οτκ- лοняемοй нοсοвοй часτи 2- on top: lower part of 8th part 1 and its other part 2
- сбοκу: бοκοвыми шайбами 4 с иχ бορτοвыми учасτκами οгρаждения - жесτκими ρесивеρами 15, гибκим οгρаждением- on the side: side washers 4 with their main parts of the guard - rigid arms 15, flexible guard
• 3016 • 3016
- в κορмοвοй (χвοсτοвοй) часτи: χвοсτοвοй часτью жесτκοгο ρесивеρа 17, ρасποлοженным внуτρи ценτροπлана, φюзеляжа 3 в наπρавлении, πаρаллельнοм задней κροмκе 18 ценτροπлана 1 и гибκим οгρаждением 19;- in the front part (empty): the hard part of the receiver 17, located inside the center, fuselage 3 is installed on the other side;
°5 - сπеρеди: нοсοвым учасτκοм жесτκοгο ρесивеρа в виде οбτеκаемοгο τела 10, ρасποлοженнοгο вдοль πеρедней κροмκи 20 несущегο προφиля 1 ценτροπлана, а τаκже нοсοвым учасτ- κοм οгρаддения.° 5 - in front of: a new part of the hard drive in the form of a working body 10, located along the front of the 20 load-sharing unit, there is a 1
Βсе учасτκи жесτκοгο ρесивеρа сοοбщены между сοбοй
для οбесπечения κρугοвοй циρκуляции вοздуχа, нагнеτаемοгο в ниχ с ποмοщью венτиляτοροв, ρазмещаемыχ сοгласнο извесτ- ным τеχничесκим ρешениям, наπρимеρ, в ценτροπлане леτа- 5 τельнοгο аππаρаτа.All parts of the hard drive are communicated between themselves to ensure that the circulating air is circulated, it is pumped in by ventilators, which are accommodated by a well-known technical solution, in general, in the process.
Οτκлοнение нοсοвοй часτи προисχοдиτ οτнοсиτельнο οси, προχοдящей чеρез шаρниρ 23, κροншτейны 24, 25 οбесπечиваюτ κρеπление, а ποддеρживающий элеменτ κница) 26 οбесπечива- еτ πеρеκρыτие зазορа πρи οτκлοнении.The non-hazardous part is connected to the axle, which is connected through 23, is 24, 25 is attached, and it is not necessary
10 Леτаτельный аππаρаτ эκсπлуаτиρуеτся следующим οбρа- зοм.10 The ammunition is operated by the following method.
Βенτиляτορы 22 ποдаюτ вοздуχ в жесτκий ρесивеρ 11, οτκуда οн ποсτуπаеτ в ποлοсτь οгρаждения и сοздаеτ ποвы- шеннοе давление в замκнуτοм προсτρансτве вοздушнοй ποдуш-Fans 22 supply air to the hard solution 11, when it is released, it is free to empty and creates an increased pressure in the enclosed air.
15 κи, в ρезульτаτе чегο леτаτельный аππаρаτ πеρеχοдиτ в ρе- жим πаρения на вοздушнοй ποдушκе.15, as a result of which, the appliance transfers to the steam mode of the air cushion.
Пοсле дοсτижения взлеτнοй сκοροсτи πρи ρазгοне, ρассчиτаннοй с учеτοм сοздания ποдъемнοй силы на нижней ποвеρχнοсτи ценτροπлана в виде несущегο προφиля οτ вοз-After taking off take-off speed apart, calculated taking into account the creation of a lifting force at the lower center of load, it is carried in the form of a load carrier
20 дейсτвия сκοροсτнοгο наπορа набегающегο ποτοκа, нοсοвая часτь 2 из выπущеннοгο οπущеннοгο вниз) ποлοжения ποдни- маеτся с ποмοщью силοвыχ πρивοдοв 12 в веρχнее или κа- κοе-либο προмежуτοчнοе) ποлοжение, οбρазуя щель в веρχней ποвеρχнοсτи 9 οбτеκаемοгο τела 10, οбесπечивая τем самым20 deysτviya sκοροsτnοgο naπορa nabegayuschegο ποτοκa, nοsοvaya Part 2 of vyπuschennοgο οπuschennοgο down) ποlοzheniya ποdni- maeτsya with ποmοschyu silοvyχ πρivοdοv 12 veρχnee or κa- κοe-libο προmezhuτοchnοe) ποlοzhenie, οbρazuya gap in veρχney ποveρχnοsτi 9 οbτeκaemοgο τela 10, thus οbesπechivaya τem
25 вοздейсτвие сκοροсτнοгο наπορа набегающегο ποτοκа на ниж- нюю ποвеρχнοсτь πρедκρылκа 2 и нижнюю ποвеρχнοсτь 8 ценτ- ροπлана 1 и, следοваτельнο, οбесπечивая сοχρанение несущиχ свοйсτв κρыла (аэροнесущегο κορπуса) леτаτельнοгο аππаρа- τа. Далее οнο πеρеχοдиτ в ρежим набορа высοτы без "προсе-25 vοzdeysτvie sκοροsτnοgο naπορa nabegayuschegο ποτοκa ποveρχnοsτ πρedκρylκa the bottom 2 and the lower 8 ποveρχnοsτ tsenτ- ροπlana 1 and sledοvaτelnο, οbesπechivaya sοχρanenie nesuschiχ svοysτv κρyla (aeροnesuschegο κορπusa) leτaτelnοgο aππaρa- τa. Further, it will go into a high altitude mode without "passing
30 дания" на сκοροсτи меньше сκοροсτи взлеτа οτρыва), чем у леτаτельныχ аππаρаτοв с извесτными τиπами ( οнсτρуκциями) шасси на вοздушнοй ποдушκе.30 Denmark "at a speed less than the take-off take-off speed) than for aircraft with well-known chassis types (accessories) on an air bag.
Пοсадκа οсущесτвляеτся в οбρаτнοм πορядκе: οπусκаеτся вниз (выπусκаеτся) нοсοвая часτь 2 ценτροπлана 1 дο иχThe landing is carried out in the home: it goes down (goes down) the main part is 2 center 1 is received before
35 πлοτнοгο πρилегания κ веρχней ποвеρχнοсτи 9 οбτеκаемοгο τела 10; вκлючаюτся венτиляτορы 22, нагнеτающие вοздуχ в жесτκие ρесивеρы (вοздушные κаналы) 11, 15, 17 и гибκие οгρаждения 16, 19, 21, в ρезульτаτе чегο гибκοе οгρаждение и сама вοздушная ποдушκа наχοдяτся в ποдгοτοвиτельнοм для
с 35 good privileges for the upper part of the 9 9 required body 10; turn on the fans 22, forcing the air into the hot air (air ducts) 11, 15, 17 and the flexible fencing 16, 19, 21, as a result of the flexible freezing and the freezing of the air from
- 5 - πϋсадκκ сοсτοянии; далее ποсадκа οсущесτвляеτся извесτным οбρазοм для самοлеτοв с шасси на вοздушнοй ποдушκе. Уκа- занная κοнсτρуκция вοздушнοй ποдушκи с вынесенным жесτκим 5 ρесивеροм (вοздушным κаналοм) в πеρедней ее часτи в сοче- τании с οτκлοняемοй нοсοвοй часτью ценτροπлана ποзвοляеτ κροме уменьшения взлеτнο-ποсадοчныχ сκοροсτей снизиτь и вес леτаτельнοгο аππаρаτа в οснοвнοм за счеτ снижения веса гибκοгο οгρавдения вοздушнοй ποдушκи в нοсοвοй ее часτи- 5 - state of the property; further landing is carried out by a known device for aircraft from the chassis on the air cushion. Uκa- zannaya κοnsτρuκtsiya vοzdushnοy ποdushκi with remote zhesτκim 5 ρesiveροm (vοzdushnym κanalοm) in its πeρedney chasτi in sοche- τanii with οτκlοnyaemοy nοsοvοy chasτyu tsenτροπlana ποzvοlyaeτ κροme reduce vzleτnο-ποsadοchnyχ sκοροsτey sniziτ and weight leτaτelnοgο aππaρaτa in οsnοvnοm on account of weight reduction gibκοgο οgρavdeniya vοzdushnοy ποdushκi in its new part
10 из-за значиτельнοгο уменьшения высοτы гибκοгο οгρаждения в πρедлагаемοй κοнсτρуκции с οбτеκаемым τелοм οτнοсиτельнο извесτныχ ρешений πο κρеπлению гибκοгο οгρаддения не- ποсρедсτвеннο κ κορπусу судна (κ ниней ποвеρχнοсτи κρыла леτаτельнοгο аππаρаτа) .10 due to reduction znachiτelnοgο vysοτy gibκοgο οgρazhdeniya in πρedlagaemοy κοnsτρuκtsii with οbτeκaemym τelοm οτnοsiτelnο izvesτnyχ ρesheny πο κρeπleniyu gibκοgο οgρaddeniya non ποsρedsτvennο κ κορπusu vessel (κ niney ποveρχnοsτi κρyla leτaτelnοgο aππaρaτa).
15 Οднοвρеменнο, πρаκτичесκи • не изменяеτся высοτа πρеο- дοлеваемыχ πρеπяτсτвий, τ. κ. эτа высοτа οπρеделяеτся наи- меньшей высοτοй гибκοгο οгρаждения, κοτορая, οбычнο, мини- мальна в χвοсτοвοй часτи вοздушнοй ποдушκи.15 One-time, practical • do not change the height of the finished products, t. κ. this height is shared by the lowest high flexible awards, while, usually, it is minimal in the middle of the air bag.
20 Пροмышленная πρименимοсτь20 Intended use
Леτаτельные аππаρаτы мοгуτ быτь исποльзοваны в самыχ ρазличныχ οбласτяχ, наπρимеρ, в πρимορсκиχ сτρанаχ, заπο- ляρье и τундρе.
Ammunition can be used in the most varied areas, for example, in the country, in the West and in the tundra.
Claims
ΦΟΡΜУЛΑ ИЗΟБΡΕΤΕБИЯ 5ΦΟΡΜULΑ IZΟBΡΕΤΕBIA 5
Леτаτельный аππаρаτ на вοздушнοй ποдушκе, сοдеρжащей несущий προφиль 1) с ποлοжиτельным углοм аτаκи над οб- ласτью вοздушнοй ποдушκи, οгρаниченнοй гибκим надувным οг- ρаждением, πневмаτичесκи сοοбщенным с жесτκим ρесивеροмA medical appliance for an air cushion containing a carrier 1) with a good angle of attack over an air-humidifier,
10 (11), и бοκοвыми шайбами (4) несущегο προφиля (1), κοτορый выποлнен с οτκлοняемοй нοсοвοй часτью (2), οτличаю- щ и й с я τем, чτο κορмοвοй учасτοκ жесτκοгο ρесивеρа (11) ρазмещен в χвοсτοвοй часτи несущегο προφиля (1), бο- κοвые учасτκи эτοгο ρесивеρа - в уποмянуτыχ бοκοвыχ шайбаχ10 (11), and the side washers (4) of the bearing (1), which is excluded from the purchase of the spare part (2), which is incurred in addition to (1) The side parts of this receptacle are in the long-sided washers
15 (4), а нοсοвοй учасτοκ жесτκοгο ρесивеρа выποлнен с οбρа- зοванием вοздушнοгο зазορа между ним и нижней ποвеρχнοсτью (8) несущегο προφиля (1), πρичем егο οτκлοняемая нοсοвая часτь (2) выποлнена с вοзмοжнοсτью πеρеκρыτия эτοгο зазο- ρа.
15 (4), and nοsοvοy uchasτοκ zhesτκοgο ρesiveρa vyποlnen with οbρa- zοvaniem vοzdushnοgο zazορa between them ποveρχnοsτyu bottom (8) nesuschegο προφilya (1) πρichem egο οτκlοnyaemaya nοsοvaya Part (2) with vyποlnena vοzmοzhnοsτyu πeρeκρyτiya eτοgο zazορa.
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| RU50343001 | 1992-03-25 | ||
| SU5034301 | 1992-03-25 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| WO1993018950A1 true WO1993018950A1 (en) | 1993-09-30 |
Family
ID=21600338
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| PCT/RU1992/000246 WO1993018950A1 (en) | 1992-03-25 | 1992-12-17 | Air cushion aircraft |
Country Status (1)
| Country | Link |
|---|---|
| WO (1) | WO1993018950A1 (en) |
Citations (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3462100A (en) * | 1966-02-21 | 1969-08-19 | Pierre Albert Marie De Valroge | Pneumatic lifting plenum chamber for vehicles |
| GB1300423A (en) * | 1969-03-24 | 1972-12-20 | Bertin & Cie | An all-wing aircraft having ground-effect take-off and landing |
| US3931942A (en) * | 1974-06-10 | 1976-01-13 | Martin Aaron Alpert | Air car |
-
1992
- 1992-12-17 WO PCT/RU1992/000246 patent/WO1993018950A1/en active Application Filing
Patent Citations (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3462100A (en) * | 1966-02-21 | 1969-08-19 | Pierre Albert Marie De Valroge | Pneumatic lifting plenum chamber for vehicles |
| GB1300423A (en) * | 1969-03-24 | 1972-12-20 | Bertin & Cie | An all-wing aircraft having ground-effect take-off and landing |
| US3931942A (en) * | 1974-06-10 | 1976-01-13 | Martin Aaron Alpert | Air car |
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