Rotor assembly and fluid transmission device having the same

US12221968B1 · US · B1

Patent metadata
FieldValue
Publication numberUS-12221968-B1
Application numberUS-202418656599-A
CountryUS
Kind codeB1
Filing dateMay 7, 2024
Priority dateNov 5, 2023
Publication dateFeb 11, 2025
Grant dateFeb 11, 2025

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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

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  7. Citations and related patents

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Abstract

Official abstract text for this publication.

A rotor assembly includes a rotation axis, a propeller, an active ring, a driver link, and a reciprocating spring. The propeller includes a hub portion and fan blades. The hub portion is located on one end of the rotation axis, and the inner sidewall of the hub portion has a gear structure surrounding the rotation axis. The active ring sleeves on the rotation axis. The driver link is pivotally connected to the active ring. The reciprocating spring is telescopically disposed on the active ring and abuts against the driver link. When the rotation axis drives the active ring to rotate, the driver link abuts against the gear structure of the hub portion and compresses the reciprocating spring. When the rotation axis stops rotating, the reciprocating spring returns to an initial position to push the driver link to separate from the gear structure.

First claim

Opening claim text (preview).

What is claimed is: 1. A rotor assembly, comprising: a rotation axis; a propeller comprising a hub portion and a plurality of fan blades extending outward from the hub portion, wherein the hub portion is located on one end of the rotation axis, and an inner sidewall of the hub portion has a gear structure surrounding the rotation axis; an active ring sleeving on the rotation axis; at least one driver link pivotally connected to the active ring; and at least one reciprocating spring telescopically disposed on the active ring and abutting against the driver link, wherein when the rotation axis drives the active ring to rotate, the driver link abuts against the gear structure of the hub portion and compresses the reciprocating spring due to a force generated by rotation, and when the rotation axis stops rotating, the reciprocating spring returns to an initial position to push the driver link to separate from the gear structure. 2. The rotor assembly of claim 1 , wherein the active ring, the driver link, and the reciprocating spring are located in the hub portion. 3. The rotor assembly of claim 1 , wherein the active ring, the driver link, and the reciprocating spring are surrounded by the gear structure. 4. The rotor assembly of claim 1 , wherein the driver link is hook shape, L shape, V shape, or U shape. 5. The rotor assembly of claim 1 , wherein the driver link comprises a first extending portion and a second extending portion adjoining the first extending portion, and an extending direction of the first extending portion is different from an extending direction of the second extending portion. 6. The rotor assembly of claim 5 , wherein the first extending portion is located between the active ring and the second extending portion, and the second extending portion is located between first extending portion and the gear structure of the hub portion. 7. The rotor assembly of claim 5 , wherein a length of the second extending portion is greater than a length of the first extending portion. 8. The rotor assembly of claim 1 , wherein the number of the driver links and the number of the reciprocating springs are both two, the two driver links are symmetrically disposed on the active ring, and the two reciprocating springs are symmetrically disposed on the active ring. 9. A fluid transmission device, comprising: a housing having an accommodating space, wherein one end of the housing has an opening communicated with the accommodating space; a motor located in the accommodating space of the housing; and an rotor assembly located in the accommodating space of the housing, and comprising: a rotation axis connected to the motor; a propeller located in the opening of the housing and comprising a hub portion and a plurality of fan blades extending outward from the hub portion, wherein the hub portion is located on one end of the rotation axis, and an inner sidewall of the hub portion has a gear structure surrounding the rotation axis; an active ring sleeving on the rotation axis; at least one driver link pivotally connected to the active ring; and at least one reciprocating spring telescopically disposed on the active ring and abutting against the driver link, wherein when the rotation axis drives the active ring to rotate, the driver link abuts against the gear structure of the hub portion and compresses the reciprocating spring due to a force generated by rotation, and when the rotation axis stops rotating, the reciprocating spring returns to an initial position to push the driver link to separate from the gear structure. 10. The fluid transmission device of claim 9 , wherein the active ring, the driver link, and the reciprocating spring are located in the hub portion. 11. The fluid transmission device of claim 9 , wherein the active ring, the driver link, and the reciprocating spring are surrounded by the gear structure. 12. The fluid transmission device of claim 9 , wherein the driver link is L shape, V shape, U shape, or hook shape. 13. The fluid transmission device of claim 9 , wherein the driver link comprises a first extending portion and a second extending portion adjoining the first extending portion, and an extending direction of the first extending portion is different from an extending direction of the second extending portion. 14. The fluid transmission device of claim 13 , wherein the first extending portion is located between the active ring and the second extending portion, and the second extending portion is located between first extending portion and the gear structure of the hub portion. 15. The fluid transmission device of claim 13 , wherein a length of the second extending portion is greater than a length of the first extending portion. 16. The fluid transmission device of claim 9 , wherein the number of the driver links and the number of the reciprocating springs are both two, the two driver links are symmetrically disposed on the active ring, and the two reciprocating springs are symmetrically disposed on the active ring.

Assignees

Inventors

Classifications

  • Axial flow fans · CPC title

  • Details of the hub · CPC title

  • F04D25/022Primary

    comprising a yielding coupling, e.g. hydraulic (a magnetic coupling F04D25/026) · CPC title

Patent family

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External sources

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What does patent US12221968B1 cover?
A rotor assembly includes a rotation axis, a propeller, an active ring, a driver link, and a reciprocating spring. The propeller includes a hub portion and fan blades. The hub portion is located on one end of the rotation axis, and the inner sidewall of the hub portion has a gear structure surrounding the rotation axis. The active ring sleeves on the rotation axis. The driver link is pivotally …
Who is the assignee on this patent?
Accton Tech Corp
What technology area does this patent fall under?
Primary CPC classification F04D25/022. Mapped technology areas include Mechanical Engineering.
When was this patent published?
Publication date Tue Feb 11 2025 00:00:00 GMT+0000 (Coordinated Universal Time) (B1). Legal status and post-grant events are not shown on this page.
What related patents are in patentsdb?
We list 2 related publications on this page (citations in our corpus or others sharing the same primary CPC).