DE457705C - Brushless plane - Google Patents

Brushless plane

Info

Publication number
DE457705C
DE457705C DEK92197D DEK0092197D DE457705C DE 457705 C DE457705 C DE 457705C DE K92197 D DEK92197 D DE K92197D DE K0092197 D DEK0092197 D DE K0092197D DE 457705 C DE457705 C DE 457705C
Authority
DE
Germany
Prior art keywords
brushless
plane
fuselage
wings
upwards
Prior art date
Legal status (The legal status 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 status listed.)
Expired
Application number
DEK92197D
Other languages
German (de)
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Individual
Original Assignee
Individual
Publication date
Priority to DEK92197D priority Critical patent/DE457705C/en
Application granted granted Critical
Publication of DE457705C publication Critical patent/DE457705C/en
Expired legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C39/00—Aircraft not otherwise provided for
    • B64C39/10—All-wing aircraft

Description

Schwanzloses Flugzeug. Der Gegenstand der Erfindung betrifft ein neues schwanzloses Flugzeug, dessen gondelaitiger Rumpf i mit zwei hintereinanderliegenden, nach oben gewölbten und durch eine ebenfalls nach oben gewölbte feste Zwischenfläche 2 verbyndenen Tragflächen 3, 4 ausgebildet ist, so daß in der Flugrichtung eine wellenförmig zusammenhängende Tragfläche entsteht. Durch das Verbinden der hintereinanderliegenden Tragflächen 3, 4 und durch die Zwischenfläche z kann die Luftmenge der ersteren Tragflächen nicht entweichen und somit den zweiten Tragflächen zugeführt werden, wodurch eine Vergrößerung der Trab fähigkeit erzielt wird. Auch soll die wellenförmige Ausgestaltung der Tragflächen den Vorteil herbeiführen, daß die Luftmenge etwas gehemmt und so das Kentern des Flugzeugs erschwert wird.Brushless plane. The subject of the invention relates to a new one tailless aircraft, the gondola-like fuselage i with two one behind the other, curved upwards and by a solid intermediate surface that is also curved upwards 2 connected wings 3, 4 is formed so that one in the direction of flight The result is a wave-like, contiguous wing. By connecting the Airfoils 3, 4 and through the intermediate surface z, the air volume of the former Wings do not escape and are thus fed to the second wings, thereby increasing the ability to trot. Also said to be wavy Design of the wings bring about the advantage that the amount of air slightly inhibited and thus the capsizing of the aircraft is made more difficult.

Durch die beiderseits des Rumpfes angeordneten je zwei schaluppenartigen Höhensteuer 6, 7 wird eine wirksame Einstellung ermöglicht, weil die gewölbten Steuerflächen noch Seitenwände haben. Dadurch, .daß derartige Steuerschirme vorn und hinten mehrfach angeordnet sind, wird das Zurückbringen des Flugzeugs in die Horizontallage bei einer Absturzgefahr wesentlich beschleunigt. Außerdem wird in Gemeinschaft mit der wellenförmig zusammenhängenden Tragfläche eine Fallschirmwirkung erzielt.Due to the two sloop-like ones arranged on both sides of the fuselage Height control 6, 7 is an effective adjustment possible because the curved control surfaces still have side walls. As a result, .that such control screens at the front and rear several times are arranged, the return of the aircraft in the horizontal position at a risk of falling is significantly accelerated. In addition, in association with the A parachute effect achieved with the undulating connected wing.

Claims (1)

PATRNTANSPRUCII: Schwanzloses Flugzeug, dadurch gekennzeichnet, daß über dem gondelartig ausgebildeten Rumpf zwei hintereinanderliegende, nach oben gewölbte, durch eine ebenfalls nach oben gewölbte feste Zwischenfläche (2) verbundene Tragflächen (3, 4) angeordnet sind, so daß in der Flugrichtung eine wellenförmig zusammenhängende Tragfläche entsteht, durch die in Gemeinschaft mit je zwei beiderseits des Rumpfes angeordneten, nach oben gewölbten, mit Seitenwänden versehenen Höhensteuerflächen (6, 7) eine Fallschirmwirkung erzielt wird.PATRNTANSPRUCII: Brushless aircraft, characterized in that above the gondola-like fuselage, two one behind the other, upwards arched, connected by a fixed intermediate surface (2) also arched upwards Wings (3, 4) are arranged so that in the direction of flight a wave-shaped coherent wing is created through the community with two on both sides of the fuselage arranged, upwardly curved, provided with side walls height control surfaces (6, 7) a parachute effect is achieved.
DEK92197D Brushless plane Expired DE457705C (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
DEK92197D DE457705C (en) Brushless plane

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DEK92197D DE457705C (en) Brushless plane

Publications (1)

Publication Number Publication Date
DE457705C true DE457705C (en) 1928-03-22

Family

ID=7237327

Family Applications (1)

Application Number Title Priority Date Filing Date
DEK92197D Expired DE457705C (en) Brushless plane

Country Status (1)

Country Link
DE (1) DE457705C (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO1991011363A1 (en) * 1990-01-31 1991-08-08 Moller International, Inc. Vtol aircraft

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO1991011363A1 (en) * 1990-01-31 1991-08-08 Moller International, Inc. Vtol aircraft
US5115996A (en) * 1990-01-31 1992-05-26 Moller International, Inc. Vtol aircraft

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