SECURING POWER SEMICONDUCTOR COMPONENTS TO CURVED SURFACES

Abstract

The disclosure relates to an arrangement with a power module including power semiconductor components. The arrangement further includes a component having a curved surface. The power module is arranged on the curved surface of the component and is non-positively detachably connected to the component. The disclosure also relates to a power converter with the arrangement and to a vehicle with a power converter.

Claims

1. An arrangement comprising: a power module having power semiconductor components; and a component having a curved surface, wherein the power module is arranged on the curved surface of the component, and wherein the power module is releasably connected to the component in a non-positive manner.

2. The arrangement of claim 1, wherein the component is a heat sink.

3. The arrangement of claim 1, wherein the power module has a casing with internal dies, and wherein the internal dies are configured to press onto the power semiconductor components or a circuit carrier of the power module in direction of the curved surface of the component.

4. The arrangement of claim 3, wherein the power semiconductor components are arranged on the circuit carrier.

5. The arrangement of claim 3, wherein the casing is fixed on the component in a non-positive manner by screws.

6. The arrangement of claim 3, wherein the casing is fixed on the component in a non-positive manner using a shroud loop fixed by screws.

7. The arrangement of claim 3, wherein the casing is fixed on the component in a non-positive manner using clamps.

8. The arrangement of claim 2, wherein a plurality of power modules with casings are fixed on the component in a non-positive manner with aid of a single shroud loop or a shrink-fit tube.

9. The arrangement of claim 8, wherein the component is cylindrical and the shroud loop wraps around the component, and wherein two ends of the shroud loop are fixed in an anchor point on the component.

10. The arrangement of claim 3, wherein an elastic first thermally conductive material is arranged between the component and the power module.

11. The arrangement of claim 10, wherein the casing is filled with an elastic second thermally conductive material.

12. A power converter comprising: an arrangement having: a power module comprising power semiconductor components; and a component having a curved surface, wherein the power module is arranged on the curved surface of the component, and wherein the power module is releasably connected to the component in a non-positive manner.

13. A vehicle comprising: a power converter for an electric or hybrid-electric drive, wherein the power converter has an arrangement comprising: a power module comprising power semiconductor components; and a component having a curved surface, wherein the power module is arranged on the curved surface of the component, and wherein the power module is releasably connected to the component in a non-positive manner.

14. The vehicle of claim 13, wherein the vehicle is an aircraft.

15. The vehicle of claim 14, further comprising: an electric motor configured to be supplied with electrical energy by the power converter; and a propeller configured to be set in rotation by the electric motor.

16. The arrangement of claim 1, wherein an elastic first thermally conductive material is arranged between the component and the power module.

17. The arrangement of claim 1, wherein the power module has a casing filled with an elastic thermally conductive material.

18. The arrangement of claim 2, wherein the power module has a casing with internal dies, and wherein the internal dies are configured to press onto the power semiconductor components or a circuit carrier of the power module in direction of the curved surface of the component.

19. The arrangement of claim 18, wherein the casing is fixed on the component in a non-positive manner by screws, a shroud loop fixed by screws, or clamps.

Description

BRIEF DESCRIPTION OF THE DRAWINGS

[0027] In the drawings:

[0028] FIG. 1 shows a sectional view of an arrangement of a first exemplary embodiment.

[0029] FIG. 2 shows a sectional view of an arrangement of a second exemplary embodiment.

[0030] FIG. 3 shows a sectional view of an arrangement of a third exemplary embodiment.

[0031] FIG. 4 shows a sectional view of an arrangement of a fourth exemplary embodiment.

[0032] FIG. 5 shows a block diagram of a power converter including a power module according to an embodiment.

[0033] FIG. 6 shows an example of an aircraft including an electrical thrust-generating unit.

DETAILED DESCRIPTION

[0034] FIG. 1 to FIG. 4 show sectional views of exemplary embodiments of how the power-electronics circuit (e.g., power module 1) is brought into contact with a one-dimensionally curved component 2, e.g., a heat sink. A circuit carrier 4 on which the power semiconductor components 3 are arranged is located on the bottom side of the power module 1. In this case, the power module 1 is pressed permanently onto the curved surface of the component 2 by a suitable device or a suitable compression die.

[0035] The topology or the curvature of the surface of the component 2 is also transferred to the circuit or the circuit carrier 4 of the power module 1 due to the contact pressure. The circuit carrier 4 may be of a ceramic or organic nature. The die 5.1 for exerting contact pressure on the power semiconductor components 3 may be configured in different variants and press directly or indirectly (e.g., with the aid of a pressure compensation material) onto the power semiconductor components 3 or onto parts of the circuit carrier.

[0036] The die 5.1 may be integrated into a casing 5 or configured as an independent component. In addition, the die 5.1 may also be used for making electrical contact with the circuit or as an additional way of heat dissipation from the top side. In one case, application of the necessary contact pressure force may be provided by screws 6 (see FIG. 1), which exert contact pressure on the dies 5.1.

[0037] Other solutions are also possible, e.g. pressing down on the power module 1 by a tensioning ring or a tensioning shroud (e.g., shroud loop 7, see FIG. 2) as well as by levers or clamps 8 (see FIG. 3). The use of a shroud loop 7 offers the possibility of arranging a large number of power modules 1 around a cylindrical component 2 (e.g., turbine/propeller casing, motor, cooling pipe, etc.) in a simple manner (see FIG. 4). The ends of the shroud loop 7 are fixed in an anchor point 9 on the component 2. Instead of the shroud loop 7, a shrink-fit tube may be used.

[0038] An additional contact force may be generated by a suitable construction of the casing 5 and by utilizing the thermal expansion of the materials used. As a result of the expansion, the power modules 1 are increasingly pressed against the component 2 during the heating operation. The intermediate space between the circuit carrier 4 and the component 2 may be filled with a first thermally conductive material 10 (e.g., thermally conductive paste, thermally conductive pad, thermal oil, graphite pad, etc.) with good thermal conductivity. The intermediate spaces in the casing 5 may be filled with a second thermally conductive material.

[0039] FIG. 5 shows a block diagram of a power converter 12, in particular a converter, with a power module 1 attached to a cooler 10 in line with the illustrations of FIG. 1 to FIG. 4.

[0040] FIG. 6 shows an electric or hybrid-electric aircraft 14, in particular an airplane, including a power converter 12 according to FIG. 5 which supplies an electric motor 15 with electrical energy. The electric motor 15 drives a propeller 16. Both are part of an electrical thrust-generating unit.

[0041] Although the disclosure has been described and illustrated more specifically in detail by the exemplary embodiments, the disclosure is not restricted by the disclosed examples and other variations may be derived therefrom by a person skilled in the art without departing from the scope of protection of the disclosure.

[0042] It is to be understood that the elements and features recited in the appended claims may be combined in different ways to produce new claims that likewise fall within the scope of the present disclosure. Thus, whereas the dependent claims appended below depend from only a single independent or dependent claim, it is to be understood that these dependent claims may, alternatively, be made to depend in the alternative from any preceding or following claim, whether independent or dependent, and that such new combinations are to be understood as forming a part of the present specification,

LIST OF REFERENCE SIGNS

[0043] 1 Power module [0044] 2 Component (in particular heat sink) [0045] 3 Power semiconductor component [0046] 4 Circuit carrier [0047] 5 Casing [0048] 5.1 Die [0049] 6 Screw [0050] 7 Shroud loop [0051] 8 Clamp [0052] 9 Anchor point [0053] 10 First thermally conductive material [0054] 11 Second thermally conductive material [0055] 12 Power converter [0056] 13 Aircraft [0057] 14 Electric motor [0058] 15 Propeller