Power switches for aircraft

US9246482B2 · US · B2

Patent metadata
FieldValue
Publication numberUS-9246482-B2
Application numberUS-201113082137-A
CountryUS
Kind codeB2
Filing dateApr 7, 2011
Priority dateApr 7, 2010
Publication dateJan 26, 2016
Grant dateJan 26, 2016

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  1. Title

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  2. Abstract

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  3. Assignees and inventors

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  4. Key dates

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  5. First independent claim

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  6. CPC / IPC classifications

    Technology tags used to group this patent with similar filings.

  7. Citations and related patents

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Abstract

Official abstract text for this publication.

The present invention relates generally to power switches for aircraft. According to a first aspect, the present invention provides an integrated solid state power switch for fault protection in an aircraft power distribution system. The integrated solid state power switch is formed of semiconductor material that provides a field effect transistor (FET) channel that is operable during normal device operation to provide an operating current flow path and a bipolar transistor channel that is operable during device overload conditions to provide an overload current flow path. A method for manufacturing such an integrated solid state power switch is also described. Various embodiments of the invention provide automatic overload current protection for aircraft systems without the need to use bulky switches or heavy cooling equipment.

First claim

Opening claim text (preview).

What is claimed is: 1. An integrated solid state power switch for fault protection in an aircraft power distribution system, the integrated solid state power switch being formed of semiconductor material comprising: a gate structure; a single channel layer electrically coupled to the gate structure, wherein the single channel layer comprises: a field effect transistor (FET) channel that is operable during normal device operation to provide an operating current flow path; and a bipolar transistor channel that is operable during device overload conditions to provide an overload current flow path; a substrate layer comprising P-type IGBT doped collector regions surrounding at least one N-type MOSFET drain region wherein the single channel layer is between the gate structure and the at least one-type MOSFET drain region; and a source/emitter physically connected to a side of the single channel layer; wherein at least one MOSFET structure and at least one IGBT structure occupy substantially the same volume vertically between the substrate layer and the gate structure to form at least one vertically integrated hybrid device. 2. The integrated solid state power switch of claim 1 , wherein the operating current flow path has maximal conductivity when the solid state power switch operates with a normal current load having a magnitude I normal , and overload current flow path has maximal conductivity when the solid state power switch operates with a fault current load having a magnitude I fault . 3. The integrated solid state power switch of claim 2 , wherein I fault >n.I normal , n being an integer having a value greater than one. 4. The integrated solid state power switch of claim 1 , wherein the field effect transistor (FET) channel is provided by at least one metal-oxide-silicon field effect transistor (MOSFET) structure. 5. The integrated solid state power switch of claim 1 , wherein the bipolar transistor channel is provided by at least one insulated gate bipolar transistor (IGBT) structure. 6. The integrated solid state power switch of claim 1 , wherein the single channel layer is between the gate structure and the P-type IGBT doped collector regions. 7. The integrated solid state power switch of claim 1 , wherein a ratio (Δ) of a number MOSFET structures (m) to a number of IGBT structures (i) is greater than 1:1. 8. The integrated solid state power switch of claim 7 , wherein the ratio (Δ) is 3:1. 9. The integrated solid state power switch of claim 1 , wherein the semiconductor material is silicon. 10. The integrated solid state power switch of claim 1 , formed on a single semiconductor wafer. 11. The integrated solid state power switch of claim 1 , wherein the integrated solid state power switch is a high power device. 12. The integrated solid state power switch of claim 1 , wherein the gate structure comprises a single gate device. 13. The integrated solid state power switch of claim 1 , comprising a ring shaped electrical contact formed on a face of the semiconductor material opposite the substrate layer and concentrically aligned with a center of the MOSFET drain region, wherein the contact comprises a radially outermost N+-type ring of material having an exposed surface, a radially innermost concentric P-type ring of material in contact with the channel layer, the outermost ring of material and the face of the semiconductor material opposite the substrate layer, and a third concentric ring of N−-type material in contact with the face of the semiconductor material opposite the substrate layer, the outermost ring of material and the innermost ring of material. 14. The integrated solid state power switch of claim 13 , wherein the gate structure comprises a layer of oxide material overlapping the innermost ring of material and the third ring of material of the contact where they are exposed at the face of the semiconductor material opposite the substrate layer. 15. The integrated solid state power switch of claim 14 , comprising a metallic layer of material over the oxide material to form a gate contact of the gate structure.

Assignees

Inventors

Classifications

  • H03K17/082Primary

    by feedback from the output to the control circuit · CPC title

  • Vertical IGBTs · CPC title

  • Vertical DMOS [VDMOS] FETs · CPC title

  • Drain regions of DMOS transistors · CPC title

  • H10D62/124Primary

    Shapes, relative sizes or dispositions of the regions of semiconductor bodies or of junctions between the regions · CPC title

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Frequently asked questions

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What does patent US9246482B2 cover?
The present invention relates generally to power switches for aircraft. According to a first aspect, the present invention provides an integrated solid state power switch for fault protection in an aircraft power distribution system. The integrated solid state power switch is formed of semiconductor material that provides a field effect transistor (FET) channel that is operable during normal de…
Who is the assignee on this patent?
Shipley Adrian, Stevens Martin James, Mawby Phil, and 2 more
What technology area does this patent fall under?
Primary CPC classification H03K17/082. Mapped technology areas include Electricity.
When was this patent published?
Publication date Tue Jan 26 2016 00:00:00 GMT+0000 (Coordinated Universal Time) (B2). Legal status and post-grant events are not shown on this page.
What related patents are in patentsdb?
We list 8 related publications on this page (citations in our corpus or others sharing the same primary CPC).