DE3627219A1 - Power-operated hinge with an integrated excursion mechanism - Google Patents
Power-operated hinge with an integrated excursion mechanismInfo
- 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- Withdrawn
Links
Classifications
-
- E—FIXED CONSTRUCTIONS
- E05—LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
- E05F—DEVICES FOR MOVING WINGS INTO OPEN OR CLOSED POSITION; CHECKS FOR WINGS; WING FITTINGS NOT OTHERWISE PROVIDED FOR, CONCERNED WITH THE FUNCTIONING OF THE WING
- E05F11/00—Man-operated mechanisms for operating wings, including those which also operate the fastening
- E05F11/02—Man-operated mechanisms for operating wings, including those which also operate the fastening for wings in general, e.g. fanlights
- E05F11/08—Man-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
- E05F11/12—Mechanisms by which the bar shifts the wing
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C9/00—Adjustable control surfaces or members, e.g. rudders
- B64C9/02—Mounting or supporting thereof
-
- E—FIXED CONSTRUCTIONS
- E05—LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
- E05Y—INDEXING 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
- E05Y2900/00—Application of doors, windows, wings or fittings thereof
- E05Y2900/50—Application of doors, windows, wings or fittings thereof for vehicles
- E05Y2900/502—Application of doors, windows, wings or fittings thereof for vehicles for aircraft
Abstract
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)
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)
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 |
-
1986
- 1986-08-11 DE DE19863627219 patent/DE3627219A1/en not_active Withdrawn
Cited By (3)
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 |