IP Library › Granted Patent US 12,546,381
Granted Patent B2
US 12,546,381 · App. 18/255,274 · Granted Feb 10, 2026

Coupling arrangement

Inventors: Eugen Blank (Bösingen, DE); Roland Moser (Obernheim, DE)
Assignee: SACS Aerospace GmbH
F16G11/12
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Quick Facts
Patent No.
US 12,546,381
App. No.
18/255,274
Granted
Feb 10, 2026
Kind
B2
Abstract

A coupling arrangement for connecting components, including a first and a second coupling part, where an end portion of the first coupling part is provided with an internal thread and an end portion of the second coupling part is provided with an external thread which is screwed into the internal thread of the first coupling part. A clamping sleeve is rotatably received on an outer surface of the end portion of the first coupling part, in which an inner surface of the clamping sleeve and the outer surface of the end portion of the first coupling part each have latch geometries which deviate from a circular geometry to provide, during a rotational movement of the clamping sleeve relative to the end portion of the first coupling part, an at least regionally elastic or elastic and plastic change in diameter for clamping the end portion of the second coupling part.

Claims (9)

1 . A coupling arrangement for connecting components, comprising a first coupling part to be fixed to a first component, and a second coupling part to be fixed to a second component, wherein an end portion of the first coupling part is provided with an internal thread extending along a thread axis, and wherein an end portion of the second coupling part is provided with an external thread extending along the thread axis, which external thread of the second coupling part is screwed into the internal thread of the first coupling part, wherein a clamping sleeve is rotatably received on an outer surface of the end portion of the first coupling part, wherein an inner surface of the clamping sleeve and the outer surface of the end portion of the first coupling part each have latch geometries which deviate from a circular geometry and correspond to one another in a cross-sectional plane aligned transversely to the thread axis, to provide, during a rotational movement of the clamping sleeve relative to the end portion of the first coupling part, an at least regionally elastic or elastic and plastic change in diameter of the end portion of the first coupling part for clamping the end portion of the second coupling part, wherein at least two latch geometries are formed on the inner surface of the clamping sleeve and wherein at least two latch geometries are formed on the outer surface of the end portion of the first coupling part, the latch geometries being arranged in such a way that in a first functional position of the clamping sleeve relative to the end portion of the first coupling part only one of the latch geometries of the clamping sleeve engages with one of the latch geometries of the end portion of the end portion of the first coupling part, and wherein, in a second functional position of the clamping sleeve with respect to the end portion of the first coupling part, the two latch geometries of the clamping sleeve are in engagement with the two latch geometries of the end portion of the first coupling part.

2 . The coupling arrangement according to claim 1 , wherein the first coupling part comprises a rod portion and a connecting portion, wherein the end portion of the first coupling part is formed on the connecting portion and wherein the connecting portion is screwed with an external thread into an internal thread of the rod portion.

3 . The coupling arrangement according to claim 1 , wherein the latch geometries on the inner surface of the clamping sleeve are formed as latch projections projecting radially inwards.

4 . The coupling arrangement according to claim 3 , wherein the latch geometries of the end portion of the first coupling part are determined by circular ring sections or by tapered ring sections tapered in each case on the outside in the direction of the rod portion and are formed with an internal thread for receiving the end portion of the second coupling part.

5 . The coupling arrangement according to claim 4 , wherein the latch geometries of the end portion of the first coupling part each have different angular extensions.

6 . The coupling arrangement according to claim 1 , wherein the latch geometries on the outer surface of the end portion of the first coupling part are designed as latch projections projecting radially outwards.

7 . The coupling arrangement according to claim 6 , wherein the latch geometries on the inner surface of the clamping sleeve are formed as circular jacket sections, between which grooves aligned along the thread axis are formed.

8 . The coupling arrangement according to claim 1 , wherein an end face of a latch geometry of the clamping sleeve and a corresponding end face of a latch geometry of the end portion of the first coupling part form an end stop for a rotational movement of the clamping sleeve relative to the end portion of the first coupling part from the first functional position into a release position.

9 . The coupling arrangement according to claim 1 , wherein a fork-shaped fastening portion is formed on the second coupling part and wherein a second coupling part is arranged on oppositely arranged end portions of the first coupling part in each case.

Assignments (1)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded May 31, 2023
From: BLANK, EUGEN; MOSER, ROLAND
To: SACS AEROSPACE GMBH
Reel/Frame 063813/0357 →
Priority Claims (1)
DE 10 2020 215 229.2 · Dec 2, 2020 · national
Continuity (1)
Related Publication 20240003407A1 · Jan 4, 2024
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