DE3627219A1 - Power-operated hinge with an integrated excursion mechanism - Google Patents

Power-operated hinge with an integrated excursion mechanism

Info

Publication number
DE3627219A1
DE3627219A1 DE19863627219 DE3627219A DE3627219A1 DE 3627219 A1 DE3627219 A1 DE 3627219A1 DE 19863627219 DE19863627219 DE 19863627219 DE 3627219 A DE3627219 A DE 3627219A DE 3627219 A1 DE3627219 A1 DE 3627219A1
Authority
DE
Germany
Prior art keywords
hinge
shaft
power
excursion
integrated
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.)
Withdrawn
Application number
DE19863627219
Other languages
German (de)
Inventor
Eckehart Zehrfeldt
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
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 Individual filed Critical Individual
Priority to DE19863627219 priority Critical patent/DE3627219A1/en
Publication of DE3627219A1 publication Critical patent/DE3627219A1/en
Withdrawn legal-status Critical Current

Links

Classifications

    • EFIXED CONSTRUCTIONS
    • E05LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
    • E05FDEVICES FOR MOVING WINGS INTO OPEN OR CLOSED POSITION; CHECKS FOR WINGS; WING FITTINGS NOT OTHERWISE PROVIDED FOR, CONCERNED WITH THE FUNCTIONING OF THE WING
    • E05F11/00Man-operated mechanisms for operating wings, including those which also operate the fastening
    • E05F11/02Man-operated mechanisms for operating wings, including those which also operate the fastening for wings in general, e.g. fanlights
    • E05F11/08Man-operated mechanisms for operating wings, including those which also operate the fastening for wings in general, e.g. fanlights with longitudinally-moving bars guided, e.g. by pivoted links, in or on the frame
    • E05F11/12Mechanisms by which the bar shifts the wing
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C9/00Adjustable control surfaces or members, e.g. rudders
    • B64C9/02Mounting or supporting thereof
    • EFIXED CONSTRUCTIONS
    • E05LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
    • E05YINDEXING SCHEME RELATING TO HINGES OR OTHER SUSPENSION DEVICES FOR DOORS, WINDOWS OR WINGS AND DEVICES FOR MOVING WINGS INTO OPEN OR CLOSED POSITION, CHECKS FOR WINGS AND WING FITTINGS NOT OTHERWISE PROVIDED FOR, CONCERNED WITH THE FUNCTIONING OF THE WING
    • E05Y2900/00Application of doors, windows, wings or fittings thereof
    • E05Y2900/50Application of doors, windows, wings or fittings thereof for vehicles
    • E05Y2900/502Application of doors, windows, wings or fittings thereof for vehicles for aircraft

Abstract

To avoid the need for a separate excursion deflection mechanism and to reduce weight, in the power-operated hinge with an integrated excursion mechanism, which allows the possibility of a pivotable mounting and pivoting of a pivotable arrangement connected to aircraft wings, doors and flaps, the shaft (3) is angled level with the pivot axis (4) only to the extent necessary for maximum excursion and can run freely in a recess within the hinge half (2), with the result that an excursion of the hinge takes place according to the rotational movement of the shaft (3). <IMAGE>

Description

Die Erfindung betrifft ein kraftbetätigtes Scharnier mit integrierter Auslenkmechanik, welches die Möglichkeit einer schwenkbaren Lagerung und Verschwenkung einer schwenkbaren Anordnung in Verbindung an Flugzeugflügeln, Toren und Klappen ermöglicht.The invention relates to a power-operated hinge with integrated deflection mechanism, which is the possibility a pivotable mounting and pivoting one swiveling arrangement in connection with aircraft wings, Gates and flaps enabled.

Es sind zwar Verfahren bekannt, insbesondere für die Betätigung und Lagerung von Klappen an Flugzeugflügeln, diese haben jedoch den Nachteil, daß außer einer schwenk­ baren Lagerung noch eine separate Aus- und Umlenkmechanik erforderlich ist.Methods are known, in particular for the Actuation and storage of flaps on aircraft wings, however, these have the disadvantage that besides panning a separate deflection and deflection mechanism is required.

Die Erfindung hat sich zur Aufgabe gesetzt, diese Nach­ teile zu vermeiden und eine Gewichtsverminderung zu er­ zielen.The invention has set itself the task of this avoid parts and reduce weight aim.

Diese Aufgabe wird erfindungsgemäß dadurch gelöst, daß eine quer zur Schwenkachse in das Scharnier eingebaute Welle auf Höhe der Schwenkachse in einem Winkel ent­ sprechend der erforderlichen Auslenkung abgewinkelt ist, und sich in einer Aussparung innerhalb der zweiten Schar­ nierhälfte frei bewegen kann, und bei Drehung eine bestimmte, vom Grad der Abwinklung der Welle abhängige, Auslenkung des Scharniers bewirkt.This object is achieved in that one built into the hinge at right angles to the swivel axis Ent shaft at the height of the swivel axis at an angle is angled according to the required deflection, and in a recess within the second coulter half can move freely, and when rotating one certain, depending on the degree of the angling of the shaft, Deflection of the hinge causes.

Die Zeichnung zeigt inThe drawing shows in

Fig. 1 eine perspektivische Ansicht und Fig. 1 is a perspective view

Fig. 2 eine perspektivische Teilansicht eines Flugzeugflügels mit Ausbrechungen, um die Funktion nach der Erfindung aufzuzeigen. Fig. 2 is a partial perspective view of an aircraft wing with knockouts to show the function according to the invention.

Fig. 1 zeigt das kraftbetätigte Scharnier mit inte­ grierter Auslenkmechanik, bestehend aus den beiden Schar­ nierhälften 1 und 2, der Welle 3 und dem Anlenkklotz 5, welcher zur Aufnahme einer Anlenkeinheit dient. Die Welle 3, welche die Scharnierhälfte 1 durchläuft, ist auf der der Schwenkachse 4 abgewendeten Seite rechtwinklig abgewinkelt und mit Gewinde versehen, zur Aufnahme eines in der Höhe zum Drehpunkt der Welle 3 verstellbaren An­ lenkklotzes 5, mit dem eine Anpassung an vorhandene Ansteuergeräte vorgenommen werden kann. Die andere Seite der Welle 3 ist auf Höhe der Schwenkachse 4 nur soweit abgewinkelt, daß ihr horizontaler Bewegungsanteil in einer Aussparung innerhalb der Scharnierhälfte 2 frei verlaufen kann. Erfolgt nun eine Anlenkung der Welle 3 über den Anlenkklotz 5 so bewirkt der vertikale Bewegungsanteil, welcher nicht innerhalb der Aussparung der Scharnierhälfte 2 frei verlaufen kann, eine Verschwenkung des Scharniers. Hierbei entspricht der maximale Grad der Verschwenkung dem Grad der Abwinklung der Welle 3 auf Höhe der Schwenk­ achse 4. Fig. 1 shows the power-operated hinge with inte grated deflection mechanism, consisting of the two coulter nierhälften 1 and 2 , the shaft 3 and the articulation block 5 , which serves to accommodate a articulation unit. The shaft 3 , which passes through the hinge half 1 , is angled at right angles on the side facing away from the pivot axis 4 and is provided with a thread for receiving a height-adjustable pivot block 5 at the pivot point of the shaft 3 , with which an adaptation to existing control devices can be carried out can. The other side of the shaft 3 is angled at the level of the pivot axis 4 only to such an extent that its horizontal movement component can run freely in a recess within the hinge half 2 . If the shaft 3 is now articulated via the articulation block 5 , the vertical movement component, which cannot run freely within the recess in the hinge half 2 , causes the hinge to pivot. Here, the maximum degree of pivoting corresponds to the degree of bending of the shaft 3 at the level of the pivot axis 4th

Claims (3)

1. Kraftbetätigtes Scharnier mit integrierter Auslenk­ mechanik, welches die Möglichkeit einer schwenkbaren Lagerung und Verschwenkung einer schwenkbaren Anordnung in Verbindung an Flugzeugflügeln, Toren und Klappen ermöglicht, dadurch gekennzeichnet, daß eine in der Scharnierhälfte (1) eingebaute Welle (3), auf Höhe der Schwenkachse (4) nur soweit, wie für die maximale Auslenk­ ung erforderlich, abgewinkelt ist, und in einer Aus­ sparung innerhalb der Scharnierhälfte (2) frei verlaufen kann, wodurch eine Auslenkung des Scharniers je nach Drehbewegung der Welle (3) erfolgt.1. Power-operated hinge with integrated deflection mechanism, which enables the possibility of a pivotable mounting and pivoting of a pivotable arrangement in connection with aircraft wings, gates and flaps, characterized in that a shaft ( 3 ) installed in the hinge half ( 1 ), at the level of Swivel axis ( 4 ) is only angled as far as required for the maximum deflection, and can run freely in a recess from within the hinge half ( 2 ), whereby the hinge is deflected depending on the rotary movement of the shaft ( 3 ). 2. Kraftbetätigtes Scharnier mit integrierter Auslenk­ mechanik nach Anspruch 1, dadurch gekennzeichnet, daß zur Auslenkung des Scharniers die Welle (3) auf der der Schwenk­ achse (4) abgewendeten Seite rechtwinklig abgewinkelt und mit Gewinde versehen ist, zur Aufnahme eines in der Höhe zum Drehpunkt der Welle (3) verstellbaren Anlenkklotzes (5), mit dem eine Anpassung an vorhandene Ansteuergeräte vor­ genommen werden kann.2. Power-operated hinge with integrated deflection mechanism according to claim 1, characterized in that for deflecting the hinge, the shaft ( 3 ) on the pivot axis ( 4 ) facing away from the side is angled at right angles and is provided with a thread for receiving a height Pivot point of the shaft ( 3 ) adjustable pivot block ( 5 ), with which an adaptation to existing control devices can be made. 3. Kraftbetätigtes Scharnier mit integrierter Auslenk­ mechanik nach Anspruch 1, dadurch gekennzeichnet, daß zur Auslenkung des Scharniers auch eine direkte Drehbewegung an der Welle (3) erfolgen kann. 3. Power-operated hinge with integrated deflection mechanism according to claim 1, characterized in that a direct rotary movement on the shaft ( 3 ) can also take place to deflect the hinge.
DE19863627219 1986-08-11 1986-08-11 Power-operated hinge with an integrated excursion mechanism Withdrawn DE3627219A1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
DE19863627219 DE3627219A1 (en) 1986-08-11 1986-08-11 Power-operated hinge with an integrated excursion mechanism

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE19863627219 DE3627219A1 (en) 1986-08-11 1986-08-11 Power-operated hinge with an integrated excursion mechanism

Publications (1)

Publication Number Publication Date
DE3627219A1 true DE3627219A1 (en) 1988-02-18

Family

ID=6307166

Family Applications (1)

Application Number Title Priority Date Filing Date
DE19863627219 Withdrawn DE3627219A1 (en) 1986-08-11 1986-08-11 Power-operated hinge with an integrated excursion mechanism

Country Status (1)

Country Link
DE (1) DE3627219A1 (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP1316501A3 (en) * 2001-11-28 2004-04-28 Northrop Grumman Corporation Aerodynamic control surface system
DE102010034755A1 (en) 2010-08-19 2012-02-23 Michael Frey Rotary drive system linkage for use in aircraft wing, has attached unit drive displaceably mounted on multiple guides and movable during operation on pivotal axis such that shaft executes movement on drive hinge half

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP1316501A3 (en) * 2001-11-28 2004-04-28 Northrop Grumman Corporation Aerodynamic control surface system
DE102010034755A1 (en) 2010-08-19 2012-02-23 Michael Frey Rotary drive system linkage for use in aircraft wing, has attached unit drive displaceably mounted on multiple guides and movable during operation on pivotal axis such that shaft executes movement on drive hinge half
DE102010034755B4 (en) * 2010-08-19 2013-11-07 Michael Frey Linkage of one aerodynamic component to another component according to the RDS principle

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Legal Events

Date Code Title Description
8139 Disposal/non-payment of the annual fee