DE1813311C - Wing arrangement for a vehicle for movement on land or in water and in the air - Google Patents

Description

, _ refer to efefc suf eise "_

arrangement of the door of a vehicle to move around on the Lanilc * biw. the water IMA ία the air, comprising a hull, - "öhenniiier and rudder as well as an engine and comprises on wheels or floats ausgerüitiitjstufld wherein substantially dreieckförraige in plan wing Verwendüng'finden, ate at the top convex and concave at the bottom are arched and their trailing edges run in one plane and unite in one point, this plane delimiting the vehicle to the floating surface and in the plane only the trailing edges of the wing and the underside of "floats" so that the wing against the Floor-

bifdet, according to patent 1234 535.

A TragSiigclauseiig each dsm Henptpateni allow to generate the full standing pressure on the water surface when the vehicle moves forward. A loss of upward lift is effectively avoided. The straight rear edges, which run in one plane and unite at a square, also look like an effective sliding surface for water. The hydrofoil design makes it possible to fly with the vehicle through the use of a ground-breaking effect "with immeasurable ground thrust. At the same time, without reducing or increasing the stability of the traffic jam, it can go over to flight.

If you want to graduate such vehicles, ie dynamic se ground effect devices, in waters that are also used with other boats, you have to arrange the propeller drive mi that any danger to other vehicles from exposed propellers, such as. B. Airscrews at Rnmpfbng as or before the flight phase, to damage and injure Irwassen, but this means that the airscrew or several airscrews must be attached over the wing center slot. Since the thrust generated by the propellers in this case is far above the center of gravity and has an ectferat effect from the water surface, "a top-heavy moment arises, dm of the size of the thrust, ie vas dsm degsa flight or Fahrüaistasd" aWt ^ ngjig is. Do you also have this? 45 eenadnten FWigeiausoSaiiBg snd saier retention of the dynamic floor effect! » za sihsSfea, in which the above-mentioned difficulties are significantly improved, and the ability to be abused without the ground effect. The invention is characterized in that two of these wings are used in the vehicle mentioned, each associated with a side of the fuselage and the trailing edges of the wings extending from the end of the fuselage and extending backwards and outwards, and one of the Schwniuner ih known per se Way is formed by the fuselage.

Through such training of the ground-effect vehicle? significant stability advantages are achieved. With this design, the propeller drive can be attached to the end of the hull as deep as possible above the surface of the water. The outflow of the propeller will then have no influence on the blades which would change the state of the sound. The creation of a top-heavy moss duck during thrust is avoided. In connection with an improved position of the propeller at the risk of nuisance to other neighboring boats, a significantly improved stability is achieved when the vehicle is only carried through the accumulation of the ground. Also, you can at the end of the trunk one - gegebeaenialls single fold-out wad - Wasserpropeiter anord-Den, which for driving a boat at low speeds, for. B. within harbor waters, can be used advantageously.

Va the rear ends of the substantially triangular Wings expediently output in the well-known white Lehwerkträger, the Seitenleitwetke Carrying cad tail units. At the trapezförmireo The shape of each wing is the long and parting the FiOgcl provided that this log! a shorter distance rarely to the hull-longitudinal mines than to the Seitlkfogn ends of the wings aofwdst In 4er Veriänäksss Scheheb can be used by the tail boom

The invention is sa Hssä der ia der Zekhmmg. “. » ~~ « _-._ .. · _ Qj

tttST.

Fig. 1 shows a schaubiMIictie AntJchl of a floor

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LoitschranbenstraJü asä der Qhmeite des Fföj§sls a fairly strong EissäaS saf die Fißgslsörämtasg eeiber tmd calls ems dt mM &

Äi der l ^ feJfa ^

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Fig. 2 mü 3 eteSsa dis Vonferansicht and the

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Fig. 4 imu 5 is a ^ diers AiisfBhnmgsfbrm dss Falassages ^ mIS dsr ErfeHiong in the Schkubild

in the immediate vicinity of Bodesnizhs

Gsriis dm ismsiiäalb tmd «Ssr eus S! Chsrdislg

The BosteK ^ ö & t-Wasscr-Lufi-Faiiiz ^ dsr Fig. 1 taam as Sch ^ nssskSiper srags formed

te s! s & i ^ s wing 14, dls — seen in the GmndriB— felri d ^^ i fsd tsid teea ftogzeug-

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own, vnnhaode- or open or open

Äüfgafcs dsr ErfiSälaRg fet estern Fah ^ ecg s = «ii ist

p j eSoea «borrowed from In general, you can see it from the doorstep Above the ground

ti * Laß * tsii Dödef, the ία

Scgmitiiog of won "ige" drive generated,

Device before Ibex the water surface scnwe-Wk Fsg.2 can be recognized, form both RW is dkr Yanfenackfaft of the vehicle one ON"". §Scrku does the frostiest prone cut dnrcfa «* FKJpIM dtta-Sdk ad or gratis, to whose iifua tdl] s ria Lcitwcrksträgtr 16 attached fet, dar ■ advises Schchnkitwerkl? expires, stuf Horizontal tail unit 18 is at rest

: Qacndnttt arched upwards, the thrust propeller 2 ι the end of the fuselage attached drive wok. Furthermore, a retractable water drive 13 can be arranged on the underside of the hull. If Stützschwimmsr provided at dm lateral wing tips. Short courtyard wings 20, which extend upwards and outwards, serve to stabilize the transverse position. μ

The construction of the embodiment of FIGS. 4 and 5 corresponds essentially to the embodiment 1 to 3. The wings 21 arranged on both sides of the fuselage 1 run - in Cross-section seen - but strongly arched, where- * s the lift of these wings close to the ground is particularly strengthened. Each wing 21 ShneK im Ground plan more of the triangular shape. Since this Flugefform corresponds to an inclined Zylmdenbschnitt, such wings can thread in a Cylinder jacket can be produced bent. I have a flight station with a low dry spot and a high utilization of the ground effect are combined in this vehicle

In the plan in the wesen'Jchea dVeirckför- ss In some, kovex upward flights 21 the Lanjtudoeitel in Mtgtele & e & e one every wing run, so every BS guest in essential symmetrical structure tJarsteSt, where the fuselage between the flights «eJBg & fögg Bt, Die- 4 · ser can prescribe to a wesanüchea part cadi of.

Claims (4)

Claims; 1. Tiag & ügaian arrangement for a vehicle to move on the land or, the water and in de; I-uit, which has a fuselage, elevator and side rod as well as an engine and is equipped with wheels or floats and in which, in plan, essentially triangular wings are used that are convex on the upper side and concave on the underside and their trailing edges run in one plane and unite at one point ?, this plane bounding the vehicle to the surface being floated over and only the trailing edges of the wing and the underside of floats running in the plane, so that the wing moves against the surface of the ground or the water Stsuramn open at the front forms, according to patent 1234535, characterized in that two of these wings (14,21) are used, one each being assigned to a side of the fuselage and the rear edges {14a, 2Ia) of the wings output from the fuselage and to the rear and outside verbnfea and one of the swimmers is formed in a manner known per se by the hull (10). 2. Vehicle according to claim 1, characterized in that that the hull designed as a float (1 ·) at the rear end has at least one propeller (12) close to the bottom or SafweisL water area 3. Vehicle according to claim 1 or 2, characterized gekeraissiclmet that in a known manner from the rear ends along the apex (15) of the essentially triangular wings (14) Tail trigcr (IQ go out, the rudder units (17) end tailplane (18) carry. 4. Vehicle according to one of claims 1 to 3, characterized in that the longitudinal apex (IS) the FlSget (14) a shorter distance to Rsmpf length stitching than to the side ends the wing (14) has (Fig. 2). Here »1 sheet of Zekfewsyef ·.