Device for holding and aligning a useful component, in particular a space travel component

Patent metadata

Field	Value
Publication number	US-10000300-B2
Application number	US-201514634970-A
Country	US
Kind code	B2
Filing date	Mar 2, 2015
Priority date	Mar 3, 2014
Publication date	Jun 19, 2018
Grant date	Jun 19, 2018

Abstract

A device for holding and aligning a component includes a first and a second housing part and a tilting device. The first housing part is arranged on a first end for stationary arrangement on a carrier and the second housing part is arranged on a second end for connection to the useful component. The first end and the second end are on opposite sides of the device in relation to a longitudinal axis. The tilting device mechanically connects the first and the second housing parts to one another and enables a defined alignment and holding of the relative position of the second housing part in relation to the first housing part. The actuator of the tilting device is a number of wires made of a shape-memory alloy. A length of each of the number of wires is individually adjustable by a respective determination of the resistance, which can be processed as a control variable in a control loop.

First claim

What is claimed is:

1. A device for holding and aligning a component, the device comprising:
a first housing part arranged on a first end of the device and configured for stationary arrangement on a space vehicle;
a second housing part arranged on a second end of the device and configured for connection to the component, wherein the first end and the second end of the device rest on opposite sides of the device with respect to a longitudinal axis; and
a tilting device, which mechanically connects the first and the second housing parts to one another and provides a defined alignment and holding of a relative position of the second housing part in relation to the first housing part,
wherein an actuator of the tilting device comprises a number of wires made of a shape-memory alloy, wherein a length of each of the number of wires is individually adjustable by a respective determination of a resistance of the respective wire, which is processed as a control variable in a control loop, and
wherein the first and the second housing parts are connected to one another via a release mechanism, which, in a starting configuration, rigidly connects the first and the second housing parts to one another to block relative movement of the first and the second housing parts and, in an operating configuration, allows relative movement of the first and the second housing parts.

2. The device of claim 1 , wherein each of the number of wires are mechanically fixedly connected to the first and the second housing parts.

3. The device of claim 1 , wherein the number of wires consist of a nickel-titanium alloy (NiTi).

4. The device of claim 1 , wherein the number of wires is arranged in parallel to the longitudinal axis of the device.

5. The device of claim 1 , wherein the number of wires are of equal thickness.

6. The device of claim 1 , wherein the tilting device comprises
at least one spring configured to press the first and the second housing parts away from one another.

7. The device of claim 1 , wherein the first and the second housing parts are spaced apart from one another, at least in the operating configuration, via the tilting device.

8. The device of claim 1 , wherein the number of wires is not tensioned in the starting configuration.

9. The device of claim 1 , wherein, after triggering of the release mechanism, the at least one spring tensions the number of wires.

10. The device of claim 1 , wherein the tilting device comprises a compression spring, which is pre-tensioned between the first and the second housing parts, and which is arranged centrally in the region of the longitudinal axis of the device.

11. The device of claim 10 , wherein the tilting device comprises three wires arranged equidistantly on a circle about the longitudinal axis.

12. The device of claim 6 , wherein the tilting device comprises two wires, wherein the two wires are arranged offset to one another by 90° on a circle about the longitudinal axis, and wherein each of the wires is associated with a spring, which is arranged opposite to the associated wire on a circle in relation to the longitudinal axis.

13. The device of claim 12 , wherein the spring associated with a wire counteracts the wire located on the opposite side in a same lever ratio.

14. The device of claim 6 , wherein the tilting device comprises four wires, which are distributed equidistantly on a circle about the longitudinal axis of the device.

Assignees

• Airbus Ds Gmbh

Inventors

• Haeberlein Matti

Classifications

• F16M13/022

  repositionable · CPC title

• B64G1/66 Primary

  Arrangements or adaptations of apparatus or instruments, not otherwise provided for · CPC title

• B64G1/26

  using jets · CPC title

• B64G1/24 Primary

  Guiding or controlling apparatus, e.g. for attitude control · CPC title

• B64G1/262

  having adjustable angles, e.g. gimbaled thrusters · CPC title