IP Library Granted Patent US 9,302,623
Granted Patent B2
US 9,302,623 · App. 13/964,251 · Granted Apr 5, 2016

Apparatus for mounting an object to a structure in a vibration-free manner

Inventors: Joerg Melcher (Lehre, DE); Bjoern Timo Kletz (Braunschweig, DE); Julian Redlich (Braunschweig, DE)
Assignee: DEUTSCHES ZENTRUM FUR LUFT-UND RAUMFAHRT E.V.
B60R1/076F16F7/104F16F15/022F16M13/02
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Quick Facts
Patent No.
US 9,302,623
App. No.
13/964,251
Granted
Apr 5, 2016
Kind
B2
Abstract

The invention relates to a device for mounting an object to a structure in a vibration-free manner. The device has an elastic arrangement that supports the object at the structure in a stiff manner in the directions of at least two of the total of six translational and rotational degrees of freedom and in a soft manner in the directions of at least one of the total of six translational and rotational degrees of freedom. Main modes of motion of the object in the directions of the rigid support have natural frequencies that are higher than any main mode of motion of the object in any direction of the soft support at least by a factor of ten. The soft support is undamped, and a damping device is provided for any main mode of motion of the object in any direction of the soft support.

Claims (20)

1. An apparatus for mounting an object to a structure in a vibration-free manner, the apparatus comprising:

an elastic arrangement comprising at last two leaf springs which are spirally wound into each other about a spiral axis within a common leaf plane and which are connected to both the structure and the object in connection areas which are facing each other across a center of mass of the object, the at last two leaf springs

stiffly support the object at the structure in directions of two translational degrees of freedom parallel to the leaf plane and one rotational degree of freedom about the spiral axis and

soft elastically support the object at the structure in directions of one translational degree of freedom in direction of the spiral axis and two rotational degrees of freedom about two axes orthogonal to the spiral axis and orthogonal to each other,

wherein the object, in each of the directions of the two translational degrees of freedom parallel to the leaf plane and the one rotational degree of freedom about the spiral axis, comprises an eigenfrequency which is by a factor of at least ten higher than any eigenfrequency of the object in each of the directions of the one translational degree of freedom in direction of the spiral axis and

the two rotational degrees of freedom about two axes orthogonal to the spiral axis and orthogonal to each other, and

wherein the elastic arrangement is undamped in each of the directions of the one translational degree of freedom in direction of the spiral axis and the two rotational degrees of freedom about two axes orthogonal to the spiral axis and orthogonal to each other; and

an attenuation device for any motion of the object in the directions of the one translational degree of freedom in direction of the spiral axis and the two rotational degrees of freedom about two axes orthogonal to the spiral axis and orthogonal to each other.

2. The apparatus of claim 1 , wherein the attenuation device comprises a passive vibration absorber having absorber eigenfrequencies adjusted to the eigenfrequencies of the object in the directions of the one translational degree of freedom in direction of the spiral axis and the two rotational degrees of freedom about two axes orthogonal to the spiral axis and orthogonal to each other.

3. The apparatus of claim 2 , wherein the vibration absorber is damped.

4. The apparatus of claim 3 , wherein an attenuation factor of the damped vibration absorber according to Lehr is less than 0.5.

5. The apparatus of claim 2 , wherein the absorber eigenfrequencies of the vibration absorber are by 5% to 25% smaller than the corresponding eigenfrequencies of the object in the directions of the one translational degree of freedom in direction of the spiral axis and the two rotational degrees of freedom about two axes orthogonal to the spiral axis and orthogonal to each other.

6. The apparatus of claim 2 , wherein the vibration absorber comprises an absorber mass which is coupled to the object via a further elastic arrangement, the further elastic arrangement being equivalent to the elastic arrangement.

7. The apparatus of claim 2 , wherein the vibration absorber comprises an absorber mass which at least partially counter-balances the object with regard to its connection to the elastic arrangement.

8. The apparatus of claim 1 , wherein the attenuation device comprises actuators made of activatable functional material which is applied to the attenuation device.

9. The apparatus of claim 8 , wherein the actuators made of activatable functional material are arranged and configured such that their activation generates at least one of movements and forces between the object and the structure in at least one of the directions of the one translational degree of freedom in direction of the spiral axis and the two rotational degrees of freedom about two axes orthogonal to the spiral axis and orthogonal to each other.

10. The apparatus of claim 9 , wherein the attenuation device activates the actuators made of activatable functional material in the sense of an active attenuation of the object in the at least one of the directions of the one translational degree of freedom in direction of the spiral axis and the two rotational degrees of freedom about two axes orthogonal to the spiral axis and orthogonal to each other.

11. The apparatus of claim 1 , wherein motions of the objects in the directions of the one translational degree of freedom in direction of the spiral axis and of the two rotational degrees of freedom about two axes orthogonal to the spiral axis and orthogonal to each other are decoupled from each other.

12. The apparatus of claim 1 , wherein the object in each of the directions of the one translational degree of freedom in direction of the spiral axis and the two rotational degrees of freedom about two axes orthogonal to the spiral axis and orthogonal to each other has an eigenfrequency of not more than about 10 Hz, and wherein the object in each of the directions of the two translational degrees of freedom parallel to the leaf plane and the one rotational degree of freedom about the spiral axis has an eigenfrequency of not less than about 100 Hz.

13. The apparatus of claim 1 , wherein the object is a mirror glass of an exterior rear view mirror of a motor vehicle, wherein the structure is a mirror holder, and wherein the directions of the one translational degree of freedom in direction of the spiral axis and the two rotational degrees of freedom about two axes orthogonal to the spiral axis and orthogonal to each other are those of a translational degree of freedom parallel to a longitudinal axis of the motor vehicle and of two rotations degrees of freedom about a vehicle cross axis and a vehicle vertical axis.

Assignments (1)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Sep 11, 2013
From: MELCHER, JOERG, DR.; KLETZ, BJOERN TIMO; REDLICH, JULIAN
To: DEUTSCHES ZENTRUM FUR LUFT- UND RAUMFAHRT E.V.
Reel/Frame 031182/0688 →
Priority Claims (2)
DE 10 2011 000 656 · Feb 11, 2011 · national
DE 20 2011 000 635 · Mar 21, 2011 · national
Continuity (2)
Continuation In Part PCTEP2012052283 · Feb 10, 2012
Related Publication 20130328337A1 · Dec 12, 2013