DE469690C - Elongated aileron made up of several areas - Google Patents

Elongated aileron made up of several areas

Info

Publication number
DE469690C
DE469690C DED47663D DED0047663D DE469690C DE 469690 C DE469690 C DE 469690C DE D47663 D DED47663 D DE D47663D DE D0047663 D DED0047663 D DE D0047663D DE 469690 C DE469690 C DE 469690C
Authority
DE
Germany
Prior art keywords
aileron
elongated
several areas
joints
sub
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
DED47663D
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.)
Daimler Benz AG
Original Assignee
Daimler Benz AG
Publication date
Priority to DED47663D priority Critical patent/DE469690C/en
Application granted granted Critical
Publication of DE469690C publication Critical patent/DE469690C/en
Expired legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C9/00Adjustable control surfaces or members, e.g. rudders

Description

Langgestrecktes Querruder aus mehreren Teilflächen Die Erfindung betrifft ein Flugzeug mit langgestrecktem Querruder aus mehreren Teilflächen, deren Drehachsen in einer Linie liegen, und besteht darin, daß benachbarte Teilflächen durch Gelenke miteinander verbunden sind.Elongated ailerons made up of several partial surfaces The invention relates to an airplane with an elongated aileron made up of several surfaces and their axes of rotation lie in a line, and consists in that adjacent partial surfaces by joints are connected to each other.

Bei einem solchen Querruder kann die Stellvorrichtung an eine der Teilflächen oder an je eine Teilfläche der miteinander durch Gelenke verbundenen Teilflächengruppen angeschlossen sein.With such an aileron, the adjusting device can be connected to one of the Sub-areas or on one sub-area each of which are connected to one another by joints Be connected to partial area groups.

Man erreicht gegenüber den bekannten, langgestreckten, aus mehreren nicht durch Gelenke verbundenen Teilflächen bestehenden Querrudern den Vorteil, daß die Stellvorrichtung vereinfacht wird und die Gefahr des Hängenbleibens einer oder mehrerer der Teilflächen durch Versagen der Stellvorrichtung bedeutend geringer ist.One achieves over the known, elongated, from several Ailerons that are not connected by joints have the advantage of that the adjusting device is simplified and the risk of getting caught or several of the partial areas are significantly lower due to failure of the actuating device is.

Auf der Zeichnung ist durch zwei Abbildungen ein Ausführungsbeispiel der Erfindung schematisch dargestellt.An exemplary embodiment is shown in the drawing by means of two images of the invention shown schematically.

Abb. I zeigt einen Grundriß eines Flugzeuges.Fig. I shows a plan of an airplane.

Abb. 2 zeigt einen Querschnitt durch eine Tragfläche mit anschließendem Querruder. Die Tragfläche a des Flugzeuges ist mit einem Querruder versehen, das sich über die ganze Länge der Tragfläche erstreckt. Damit die infolge der Belastung eintretende Durchbiegung der Tragfläche sich nicht auf das Querruder ausdehnen kann, besteht die Ruderfläche aus Teilflächen b. Jede Teilfläche b ist durch Gelenke c mit der Tragfläche a verbunden. Unter sich dagegen sind die Teilflächen b zweckmäßig durch Kugelgelenke d verbunden. Zum Einstellen der Ruderfläche kann das Stellwerk an eine der Teilflächen oder an eine Gruppe angeschlossen sein. Zweckmäßig ist zum Betätigen der Ruderfläche ein für beideSeiten gemeinsamer, durch den Führer zu bedienender oder auf mechanische Weise zu beeinflussender Hebel vorgesehen.Fig. 2 shows a cross section through a wing with a subsequent Ailerons. The wing a of the aircraft is provided with an aileron, the extends over the entire length of the wing. So that as a result of the load any deflection of the wing that occurs cannot extend to the aileron, the rudder surface consists of sub-surfaces b. Each sub-area b is formed by joints c connected to the wing a. On the other hand, the partial areas b are useful among themselves connected by ball joints d. The signal box can be used to adjust the rudder surface be connected to one of the partial areas or to a group. Is useful for Operation of the rudder surface is common to both sides and can be operated by the driver or provided in a mechanical way to be influenced lever.

Zum Anschluß der Ruderflächen an ein gemeinsames Stellwerk werden zweckmäßig die einzelnen Flächen beispielsweise mit einem endlosen Kettenzug e versehen, in welchen auf gemeinsamer Welle sitzende Kettenräder eingreifen. Durch Verdrehen der Welle mittels eines Hebels werden die Teilflächen gleichsinnig verstellt. Es können natürlich auch Einrichtungen anderer Art vorgesehen werden.To connect the control surfaces to a common signal box it is appropriate to provide the individual surfaces with an endless chain hoist e, for example, in which seated chain wheels on a common shaft engage. By twisting the shaft by means of a lever, the partial surfaces are adjusted in the same direction. It Of course, other types of facilities can also be provided.

Claims (2)

PATENTANSPRÜCHE: I. Langgestrecktes Querruder aus mehreren Teilflächen, deren Drehachsen in einer Linie liegen, dadurch gekennzeichnet, daß benachbarte Teilflächen durch Gelenke miteinander verbunden sind. PATENT CLAIMS: I. Elongated aileron made of several partial surfaces, whose axes of rotation lie in a line, characterized in that adjacent Partial surfaces are connected to one another by joints. 2. Langgestrecktes Querruder nach Anspruch i, dadurch gekennzeichnet, daß die Stellvorrichtung an eine der Teilflächen oder an j e eine Teilfläche der miteinander durch Gelenke verbundenen Teilflächengruppen angeschlossen ist.2. Elongated aileron according to claim i, characterized in that the adjusting device is attached to one of the partial surfaces or at j e a sub-area of the sub-area groups connected to one another by joints connected.
DED47663D Elongated aileron made up of several areas Expired DE469690C (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
DED47663D DE469690C (en) Elongated aileron made up of several areas

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DED47663D DE469690C (en) Elongated aileron made up of several areas

Publications (1)

Publication Number Publication Date
DE469690C true DE469690C (en) 1928-12-19

Family

ID=7050579

Family Applications (1)

Application Number Title Priority Date Filing Date
DED47663D Expired DE469690C (en) Elongated aileron made up of several areas

Country Status (1)

Country Link
DE (1) DE469690C (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE740502C (en) * 1942-04-09 1943-10-22 Ernst Heinkel Flugzeugwerke G Drive for landing flaps
DE2944114A1 (en) * 1978-12-04 1980-06-26 Boeing Co HINGE ARRANGEMENT FOR CONTROL VALVES

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE740502C (en) * 1942-04-09 1943-10-22 Ernst Heinkel Flugzeugwerke G Drive for landing flaps
DE2944114A1 (en) * 1978-12-04 1980-06-26 Boeing Co HINGE ARRANGEMENT FOR CONTROL VALVES

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