DE20215459U1 - Model airplane or helicopter capable of vertical take off and landing - Google Patents

Model airplane or helicopter capable of vertical take off and landing

Info

Publication number
DE20215459U1
DE20215459U1 DE20215459U DE20215459U DE20215459U1 DE 20215459 U1 DE20215459 U1 DE 20215459U1 DE 20215459 U DE20215459 U DE 20215459U DE 20215459 U DE20215459 U DE 20215459U DE 20215459 U1 DE20215459 U1 DE 20215459U1
Authority
DE
Germany
Prior art keywords
propellers
aircraft
model
drive units
aircraft according
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 - Lifetime
Application number
DE20215459U
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.)
DAUSCHEK KLAUS
Original Assignee
DAUSCHEK KLAUS
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by DAUSCHEK KLAUS filed Critical DAUSCHEK KLAUS
Priority to DE20215459U priority Critical patent/DE20215459U1/en
Publication of DE20215459U1 publication Critical patent/DE20215459U1/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • A—HUMAN NECESSITIES
    • A63—SPORTS; GAMES; AMUSEMENTS
    • A63H—TOYS, e.g. TOPS, DOLLS, HOOPS OR BUILDING BLOCKS
    • A63H27/00—Toy aircraft; Other flying toys
    • A63H27/12—Helicopters ; Flying tops
    • A—HUMAN NECESSITIES
    • A63—SPORTS; GAMES; AMUSEMENTS
    • A63H—TOYS, e.g. TOPS, DOLLS, HOOPS OR BUILDING BLOCKS
    • A63H27/00—Toy aircraft; Other flying toys
    • A63H27/02—Model aircraft

Landscapes

  • Toys (AREA)

Abstract

The model aircraft has three propellers (1,2,3) driven by electric motors. Two equal sized drive units (4,5) are attached in carriers to the wing tips. A smaller drive unit (6) is attached to the tail of the aircraft. The two front drive units (4,5) can preferably be tipped forwards and backwards by a servo control. The aircraft can be flown in a helicopter type motion or forwards like an airplane.

Description

Der Beschreibungstext wurde nicht elektronisch erfaßt The description text was not recorded electronically  

Der Beschreibungstext wurde nicht elektronisch erfaßt The description text was not recorded electronically  

Der Beschreibungstext wurde nicht elektronisch erfaßt The description text was not recorded electronically  

Der Beschreibungstext wurde nicht elektronisch erfaßtThe description text was not recorded electronically

Claims (6)

1. Senkrecht startendes und landendes Modellflugzeug mit drei durch Elektromotoren betriebenen Luftschrauben (1, 2, 3), wobei jeweils zwei gleich große Antriebseinheiten (4, 5) in Gondeln an den Flügelspitzen und eine kleinere Antriebseinheit (6) im Heck des Flugzeuges angebracht sind.1. Vertical starting and landing model airplane with three propellers ( 1 , 2 , 3 ) operated by electric motors, whereby two equally large drive units ( 4 , 5 ) are attached in gondolas to the wing tips and a smaller drive unit ( 6 ) in the tail of the aircraft , 2. Modellflugzeug nach Anspruch 1 dadurch gekennzeichnet, dass die beiden Antriebseinheiten (4, 5) jeweils durch eine Servoansteuerung im rechten- und im linken Tragflügel, nach Vorne und nach Hinten gekippt werden können.2. Model aircraft according to claim 1, characterized in that the two drive units ( 4 , 5 ) can each be tilted to the front and to the rear by a servo control in the right and in the left wing. 3. Modellflugzeug nach Anspruch 1 und 2 dadurch gekennzeichnet, dass die Steuerung des Flugzeuges im hubschrauberähnlichen Schwebeflug und im horizontalen Vorwärtsflug nur durch Drehzahlsteuerung der drei Luftschrauben (1, 2, 3) und durch Kippen der zwei Antriebseinheiten (4, 5) an den Flügelspitzen erfolgt.3. Model aircraft according to claim 1 and 2, characterized in that the control of the aircraft in helicopter-like hover and in horizontal forward flight only by speed control of the three propellers ( 1 , 2 , 3 ) and by tilting the two drive units ( 4 , 5 ) at the wing tips he follows. 4. Modellflugzeug nach Anspruch 1 bis 3 dadurch gekennzeichnet, dass das Flugzeug um alle drei Bewegungsachsen mit Kreiseln stabilisiert wird.4. Model aircraft according to claim 1 to 3, characterized in that the aircraft at all three movement axes are stabilized with gyros. 5. Modellflugzeug nach Anspruch 1 bis 4 dadurch gekennzeichnet, dass die beiden Propeller 1 und 2 gleichläufig sind.5. Model aircraft according to claim 1 to 4, characterized in that the two propellers 1 and 2 are the same. 6. Modellflugzeug nach Anspruch 1 bis 4 dadurch gekennzeichnet, dass die Propeller 1 und 2 gegenläufig sind.6. Model aircraft according to claim 1 to 4, characterized in that the propellers 1 and 2 are in opposite directions.
DE20215459U 2002-10-08 2002-10-08 Model airplane or helicopter capable of vertical take off and landing Expired - Lifetime DE20215459U1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
DE20215459U DE20215459U1 (en) 2002-10-08 2002-10-08 Model airplane or helicopter capable of vertical take off and landing

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE20215459U DE20215459U1 (en) 2002-10-08 2002-10-08 Model airplane or helicopter capable of vertical take off and landing

Publications (1)

Publication Number Publication Date
DE20215459U1 true DE20215459U1 (en) 2003-03-06

Family

ID=7975792

Family Applications (1)

Application Number Title Priority Date Filing Date
DE20215459U Expired - Lifetime DE20215459U1 (en) 2002-10-08 2002-10-08 Model airplane or helicopter capable of vertical take off and landing

Country Status (1)

Country Link
DE (1) DE20215459U1 (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN101837195B (en) * 2010-01-21 2012-02-08 罗之洪 Model airplane with vertical takeoff and landing
CN104494812A (en) * 2015-01-08 2015-04-08 常州大学 Fixed-wing air vehicle device with screw propeller having tiltable shaft
CN106267839A (en) * 2015-05-15 2017-01-04 上海九鹰电子科技有限公司 Propeller connector, model aerial vehicle for model aerial vehicle

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN101837195B (en) * 2010-01-21 2012-02-08 罗之洪 Model airplane with vertical takeoff and landing
CN104494812A (en) * 2015-01-08 2015-04-08 常州大学 Fixed-wing air vehicle device with screw propeller having tiltable shaft
CN106267839A (en) * 2015-05-15 2017-01-04 上海九鹰电子科技有限公司 Propeller connector, model aerial vehicle for model aerial vehicle

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Legal Events

Date Code Title Description
R207 Utility model specification

Effective date: 20030410

R156 Lapse of ip right after 3 years

Effective date: 20060503