DE732706C - Storage of oars, flaps or the like on aircraft - Google Patents
Storage of oars, flaps or the like on aircraftInfo
- Publication number
- DE732706C DE732706C DEK155801D DEK0155801D DE732706C DE 732706 C DE732706 C DE 732706C DE K155801 D DEK155801 D DE K155801D DE K0155801 D DEK0155801 D DE K0155801D DE 732706 C DE732706 C DE 732706C
- Authority
- DE
- Germany
- Prior art keywords
- flaps
- aircraft
- oars
- storage
- bearings
- 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
Links
Classifications
-
- 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
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Support Of The Bearing (AREA)
Description
Lagerung von Rudern, Kappen o. dgl. an Flugzeugen Die bisher bekannten Ruder- oder Klappenlagerungen für Flugzeuge haben den Nachteil, daß sie im allgemeinen viel Zeit zum An- und Abbauen der Ruder oder Klappen erfordern. Die Bolzen oder Muttern zum Befestigen der Lager für die Ruder oder Klappen werden an der Flugzeugzelle aus strömungstechnischen Gründen meist innerhalb des Umrisses von Flossen, Rudern oder Klappen angeordnet und sind daher schwer zugänglich.Storage of oars, caps or the like on aircraft The previously known Rudder or flap mountings for aircraft have the disadvantage that they in general require a lot of time to attach and remove the oars or flaps. The bolts or Nuts for attaching the bearings for the rudder or flaps are attached to the airframe for fluidic reasons mostly within the outline of fins, oars or flaps and are therefore difficult to access.
Es ist bereits bekannt, geteilte Lagerringe für die Achslager von Rudern bei Flugzeugen zu verwenden. Jedoch erfordern diese noch immer einen unverhältnismäßig großen Konstruktionsaufivand.It is already known to use split bearing rings for the axle bearings of To use rowing on airplanes. However, these still require a disproportionate amount large construction effort.
Durch die Erfindung werden die bisherigen Mängel dadurch behoben, da.ß in den geteilten Lagerringen .eine beliebige Anzahl Wälzlager drehbar befestigt sind.The present deficiencies are eliminated by the invention, da.ß in the split bearing rings .any number of roller bearings rotatably attached are.
Dabei ist es besonders vorteilhaft, die Wälzlager in bekannter Weise elastisch zu lagern oder mit einem nachgiebigen Belag zu versehen.It is particularly advantageous to use the rolling bearings in a known manner to be stored elastically or to be provided with a flexible covering.
Hierdurch wird das Übertragen von Schwingungen auf die Bauglieder des Flugzeuges, an welche die Ruder oder Klappen angeschlossen sind, unterbunden.This prevents vibrations from being transmitted to the structural members of the aircraft to which the rudders or flaps are connected.
Abb. i zeigt eine Lagerung gemäß der Erfindung, Abb.2 einen Schnitt durch den Lagerring.Fig. I shows a storage according to the invention, Fig.2 shows a section through the bearing ring.
In einem zweiteiligen Ring i, 2 sind an sich bekannte Abi; älzlager 3 in beliebiger An zahl und Verteilung angea-rdnet, und zwar so., daß die Achsen der Abwälzlager parallel zu der Drehachse des Ruders oder der Klappe liegen. Die Hälfte i des Lagerringes i, 2 ist fest oder bewegbar an dem Lagerträgerteil q. des Flugzeuges in beliebiger Weise angebaut. Die Hälfte 2 des Lagerringes i, 2 ist abklappbar an die Hälfte i befestigt, und deren Schwenkachse. ist ebenfalls parallel zu der Drehachse des Ruders oder der Klappe angeordnet. Zur Dämpfung von Ruder- oder Klappenschwirngungen sowie zum Ausgleich von Bauungenauigkeiten können die Abwälzlager 3 elastisch gelagert «-erden oder mit einem beliebigen elastischen Bezug versehen werden.In a two-part ring i, 2 are known Abi; roller bearings 3 assigned in any number and distribution, in such a way that the axes the roller bearings are parallel to the axis of rotation of the rudder or the flap. the Half i of the bearing ring i, 2 is fixed or movable on the bearing support part q. of Aircraft grown in any way. Half 2 of the bearing ring i, 2 can be folded down attached to half i, and its pivot axis. is also parallel to the The axis of rotation of the rudder or the flap is arranged. For damping oar or flap swings and to compensate for structural inaccuracies, the rolling bearings 3 can be elastically mounted «-Ground or provided with any elastic cover.
Claims (3)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DEK155801D DE732706C (en) | 1939-10-19 | 1939-10-19 | Storage of oars, flaps or the like on aircraft |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DEK155801D DE732706C (en) | 1939-10-19 | 1939-10-19 | Storage of oars, flaps or the like on aircraft |
Publications (1)
Publication Number | Publication Date |
---|---|
DE732706C true DE732706C (en) | 1943-03-10 |
Family
ID=7253348
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DEK155801D Expired DE732706C (en) | 1939-10-19 | 1939-10-19 | Storage of oars, flaps or the like on aircraft |
Country Status (1)
Country | Link |
---|---|
DE (1) | DE732706C (en) |
-
1939
- 1939-10-19 DE DEK155801D patent/DE732706C/en not_active Expired
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