Systems, methods, and mechanical designs for inverters for evtol aircraft
US-2024253796-A1 · Aug 1, 2024 · US
US9476735B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-9476735-B2 |
| Application number | US-201414499874-A |
| Country | US |
| Kind code | B2 |
| Filing date | Sep 29, 2014 |
| Priority date | Oct 24, 2013 |
| Publication date | Oct 25, 2016 |
| Grant date | Oct 25, 2016 |
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Official abstract text for this publication.
A magnetic encoder 1 including a support member 2 attached to a rotating body 12 and a magnet member 3 fixed to the support member 2 , the support member 2 and the magnet 4 are not attached to each other using an adhesive but the support member 2 and the plastic magnet 4 are joined together by molding shrinkage or wrap-around form of the magnet 4 , and the material for the magnet 4 is selected such that the value of the ratio ((αp−αm)/εc) of a difference (αp−αm) between flowing-direction linear expansion coefficient (αp) of the magnet 4 and linear expansion coefficient (αm) of the support member 2 , to tensile breaking strain (εc) of the material for the magnet 4 is equal to or less than a value beginning at a threshold (Nth) based on a prescribed value of cycle member at thermal shock destructive test.
Opening claim text (preview).
The invention claimed is: 1. A magnetic encoder comprising: an annular support member that is formed from a steel plate and attached to a rotating body; and an annular magnet member that is fixed to the support member and has N and S poles magnetized circumferentially at regular intervals in a multipolar manner, wherein the magnet member is a plastic magnet, there is no adhesive layer between the support member and the plastic magnet, and the support member and the plastic magnet are joined together by molding shrinkage of the plastic magnet or wrap-around form of the plastic magnet, and the material for the plastic magnet is selected such that the value of the ratio ((αp−αm)/εc) of a difference (αp−αm) between flowing-direction linear expansion coefficient (αp) of the plastic magnet and linear expansion coefficient (αm) of the support member, to tensile breaking strain (εc) of the material for the plastic magnet is equal to or less than a value beginning at a threshold (Nth) based on a prescribed value of cycle number at thermal shock destructive test, and tensile strength (σc) of the plastic magnet is equal to or more than a value beginning at a threshold (Fth) based on a prescribed value of axial binding force between the plastic magnet and the support member, and wherein the magnetic encoder is an axial type, and includes a joint portion resulting from molding shrinkage at a radially outer peripheral part of the plastic magnet and includes a joint portion resulting from wrap-around from a radially inner peripheral part of the plastic magnet. 2. A bearing device comprising the magnetic encoder according to claim 1 , wherein the rotating body is an inner ring of a bearing, and the bearing device further includes a cup-shaped protective cover that is press-fitted into an outer ring of the bearing as a non-rotating body to cover the magnetic encoder.
Shaft end sealing means, e.g. cup-shaped caps or covers · CPC title
delivered by rotating magnets · CPC title
Wheel hubs or castors · CPC title
influenced by the relative movement between the Hall device and magnetic fields (see G01R33/06) · CPC title
mounted in bearings (bearings F16C) · CPC title
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