DE202016001637U1 - Extension mechanism for drives in aircraft models - Google Patents

Extension mechanism for drives in aircraft models Download PDF

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Publication number
DE202016001637U1
DE202016001637U1 DE202016001637.8U DE202016001637U DE202016001637U1 DE 202016001637 U1 DE202016001637 U1 DE 202016001637U1 DE 202016001637 U DE202016001637 U DE 202016001637U DE 202016001637 U1 DE202016001637 U1 DE 202016001637U1
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Germany
Prior art keywords
ausfahrmechanik
drives
aircraft models
linear rail
extension mechanism
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Expired - Lifetime
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DE202016001637.8U
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German (de)
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Individual
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Individual
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Publication of DE202016001637U1 publication Critical patent/DE202016001637U1/en
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    • AHUMAN NECESSITIES
    • A63SPORTS; GAMES; AMUSEMENTS
    • A63HTOYS, e.g. TOPS, DOLLS, HOOPS OR BUILDING BLOCKS
    • A63H27/00Toy aircraft; Other flying toys
    • A63H27/14Starting or launching devices for toy aircraft; Arrangements on toy aircraft for starting or launching
    • AHUMAN NECESSITIES
    • A63SPORTS; GAMES; AMUSEMENTS
    • A63HTOYS, e.g. TOPS, DOLLS, HOOPS OR BUILDING BLOCKS
    • A63H27/00Toy aircraft; Other flying toys
    • A63H27/02Model aircraft

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  • Transmission Devices (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Toys (AREA)

Abstract

Ausfahrmechanik für Antriebe bei Flugmodellen insbesondere Impeller u. Klappluftschrauben, dadurch gekennzeichnet, dass die vertikale Führung durch eine Linearschiene (4) mit Wagen (5) nahezu spielfrei und ohne horizontale Verschiebung des Schwerpunktes erfolgt.Ausfahrmechanik for drives in aircraft models in particular impeller u. Folding propellers, characterized in that the vertical guidance by a linear rail (4) with carriage (5) is almost free of play and without horizontal displacement of the center of gravity.

Description

Am Markt befindliche Systeme haben eine Klappfunktion und werden von einem Servo ausgefahren. Linear ausfahrbare Systeme werden mit Spindelantrieb und Steuerelektronik angeboten.On the market systems have a folding function and are extended by a servo. Linear extendable systems are offered with spindle drive and control electronics.

Hier wird nach Anspruch 1 u. 2 ein präzises Linearführungssystem mit der einfachen Ansteuerung mittels Servo (1) realisiert.Here is according to claim 1 u. 2 a precise linear guidance system with easy control via servo ( 1 ) realized.

Des weiteren können nach Anspruch 3 durch Tausch von Kniehebel und Linearschiene verschiedene Triebwerksgrößen verwendet werden.Furthermore, different engine sizes can be used according to claim 3 by exchange of toggle and linear rail.

Nach Anspruch 4 kann das System durch Tausch des Tragarm (7) mit dem Propellermast (8) für Impeller und Klappluftschrauben verwendet werden.According to claim 4, the system by exchanging the support arm ( 7 ) with the propeller mast ( 8th ) for impellers and folding propellers.

1 u. 2 zeigen die Mechanik im ein- bzw. ausgefahrenem Zustand. Auf 3 ist die Variante mit Klappluftschraube zu sehen. 1 u. 2 show the mechanics when retracted or extended. On 3 is the variant with folding air screw to see.

Claims (4)

Ausfahrmechanik für Antriebe bei Flugmodellen insbesondere Impeller u. Klappluftschrauben, dadurch gekennzeichnet, dass die vertikale Führung durch eine Linearschiene (4) mit Wagen (5) nahezu spielfrei und ohne horizontale Verschiebung des Schwerpunktes erfolgt.Ausfahrmechanik for drives in aircraft models in particular impeller u. Folding propellers, characterized in that the vertical guide by a linear rail ( 4 ) with cart ( 5 ) occurs almost without play and without horizontal displacement of the center of gravity. Ausfahrmechanik nach Anspruch 1, dadurch gekennzeichnet, dass der Ausfahrvorgang durch ein Servo mit Servohebel (1) ohne zusätzliche Elektronik (Endschalter etc.) bewerkstelligt wird.Ausfahrmechanik according to claim 1, characterized in that the extension operation by a servo with servo lever ( 1 ) without additional electronics (limit switch, etc.) is accomplished. Ausfahrmechanik nach Anspruch 1 oder 2, dadurch gekennzeichnet, dass durch Anpassung der Länge der Kniehebel u. Linearschiene verschiedene Triebwerksgrößen verwendet werden können.Ausfahrmechanik according to claim 1 or 2, characterized in that by adjusting the length of the knee lever u. Linear rail different engine sizes can be used. Ausfahrmechanik nach einem der Ansprüche 1 bis 3, dadurch gekennzeichnet, dass durch Tausch des Tragarmes (7) für den Impeller, durch die Montage eines Propellermastes (8) auch eine Verwendung für Klappluftschrauben möglich ist.Ausfahrmechanik according to one of claims 1 to 3, characterized in that by exchange of the support arm ( 7 ) for the impeller, by mounting a propeller mast ( 8th ) also a use for folding propellers is possible.
DE202016001637.8U 2015-04-08 2016-03-11 Extension mechanism for drives in aircraft models Expired - Lifetime DE202016001637U1 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
AT91/2015U 2015-04-08
ATGM91/2015U AT14811U1 (en) 2015-04-08 2015-04-08 Extension mechanism for drives in aircraft models

Publications (1)

Publication Number Publication Date
DE202016001637U1 true DE202016001637U1 (en) 2016-05-31

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ID=56097397

Family Applications (1)

Application Number Title Priority Date Filing Date
DE202016001637.8U Expired - Lifetime DE202016001637U1 (en) 2015-04-08 2016-03-11 Extension mechanism for drives in aircraft models

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AT (1) AT14811U1 (en)
DE (1) DE202016001637U1 (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE202019102543U1 (en) 2019-05-07 2019-05-21 CS Besitz- und Verwaltungs-UG (haftungsbeschränkt) Device for moving a drive unit for an aircraft
DE102019111791A1 (en) * 2019-05-07 2020-11-12 CS Besitz- und Verwaltungs-UG (haftungsbeschränkt) Device for moving a drive unit for an aircraft

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE2445013C3 (en) * 1974-09-20 1980-08-21 Rhein-Flugzeugbau Gmbh, 4050 Moenchengladbach Drive unit with jacket screw
DE4231676C1 (en) * 1992-09-22 1994-03-17 Klaus Plesser Motor-driven foldable propeller for motorised glider - has propeller located at stern, and is retracted into glider body
DE4426403C1 (en) * 1994-07-26 1996-02-08 Conzelmann Modelltechnik Auxiliary power plant for glider
DE10152381A1 (en) * 2001-10-28 2003-05-08 Hce Consulting & Engineering H Twin-jet power plant has both engines in flap-covered shaft in fuselage when not in use and extended out from fuselage sideways when in use
DE202013003812U1 (en) * 2013-04-24 2013-06-13 Lutz Focke Extending or unfolding impeller for model gliders

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE202019102543U1 (en) 2019-05-07 2019-05-21 CS Besitz- und Verwaltungs-UG (haftungsbeschränkt) Device for moving a drive unit for an aircraft
DE102019111791A1 (en) * 2019-05-07 2020-11-12 CS Besitz- und Verwaltungs-UG (haftungsbeschränkt) Device for moving a drive unit for an aircraft
DE102019111791B4 (en) * 2019-05-07 2021-05-27 CS Besitz- und Verwaltungs-UG (haftungsbeschränkt) Device for moving a drive unit for an aircraft

Also Published As

Publication number Publication date
AT14811U1 (en) 2016-06-15

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R086 Non-binding declaration of licensing interest
R207 Utility model specification
R156 Lapse of ip right after 3 years