Acoustic noise suppressing ducted fan propulsor mounting arrangement and treatments

US12195167B2 · US · B2

Patent metadata
FieldValue
Publication numberUS-12195167-B2
Application numberUS-202318451619-A
CountryUS
Kind codeB2
Filing dateAug 17, 2023
Priority dateApr 17, 2018
Publication dateJan 14, 2025
Grant dateJan 14, 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 general mounting method for ducted fan propulsors is disclosed. This mounting method uses extremely slender stators that connect the duct ring to the propulsor which is mounted in the middle and drives the rotor, fan or propeller. The slender stators take the form of spokes and as such are so slender that the midspan stresses within the spokes are dominated by axial tension loads rather than the shear loads experienced by conventional stators. The spokes may have an aerodynamic shape and damping methods may be used to retard spoke vibrations and transmission of engine vibrations to the duct and force. The duct itself is also stiffened by the spoke arrangement, thereby reducing low frequency vibration modes.

First claim

Opening claim text (preview).

The invention claimd is: 1. An acoustic noise suppressing mounting arrangement for a ducted fan assembly comprising: an outer duct through which air is entrained on one end and ejected on the other; a central shaft assembly comprising: at least one rotating member, wherein the at least one rotating member comprises at least one of a fan, a propeller, an impeller, and a rotor; and a shaft power source configured to provide shaft power to the at least one rotating member, wherein the shaft power source comprises an external drive shaft, an electric engine, an internal combustion engine, or a turbine engine; and one or more bearing assemblies configured to rotatably secure the at least one rotating member within the outer duct and to transfer thrust loads between the outer duct and the central shaft assembly; and a plurality of structural spokes coupled to the central shaft assembly and configured to transfer loads between the outer duct and at least a portion of the central shaft assembly, wherein each structural spoke of the plurality of structural spokes is pretensioned and has a high aspect ratio. 2. The acoustic noise suppressing mounting arrangement of claim 1 , wherein the plurality of structural spokes comprise a first structural spoke arrangement and a second structural spoke arrangement. 3. The acoustic noise suppressing mounting arrangement of claim 2 , wherein the first structural spoke arrangement comprises aft-swept structural spokes and the second structural spoke arrangement comprises forward-swept structural spokes. 4. The acoustic noise suppressing mounting arrangement of claim 1 , wherein the plurality of structural spokes are positioned upstream of the fan, the propeller, the impeller, or the rotor. 5. The acoustic noise suppressing mounting arrangement of claim 1 , wherein the plurality of structural spokes are positioned downstream of the fan, the propeller, the impeller, or the rotor. 6. The acoustic noise suppressing mounting arrangement of claim 1 , further comprising a second rotating member, wherein the second rotating member comprises at least one of a second fan, a second propeller, a second impeller, and a second rotor, and wherein the plurality of structural spokes are positioned between the at least one rotating member and the second rotating member. 7. The acoustic noise suppressing mounting arrangement of claim 1 , wherein the plurality of structural spokes are positioned upstream of the fan. 8. The acoustic noise suppressing mounting arrangement of claim 1 , wherein each of the plurality of structural spokes is configured to damp out vibrations transfer to a cross-section of the spoke. 9. The acoustic noise suppressing mounting arrangement of claim 1 , further comprising a plurality of fixtures, each fixture of the plurality of fixtures corresponding to one structural spoke of the plurality of structural spokes and configured to couple a first end of the corresponding structural spoke to the central shaft assembly. 10. The acoustic noise suppressing mounting arrangement of claim 1 , further comprising a plurality of structural spoke mounting assemblies, each structural spoke mounting assembly of the plurality of structural spoke mounting assemblies corresponding to one structural spoke of the plurality of structural spokes and configured to couple a second end of the corresponding structural spoke to the outer duct, wherein each the plurality of structural spoke mounting assemblies is configured to tighten the corresponding structural spoke and to minimize transfer of axial spoke vibrations to a wall of the outer duct. 11. The acoustic noise suppressing mounting arrangement of claim 1 , wherein the plurality of structural spoke mounting assemblies comprise at least one of piezoelectric actuators, electroresistive actuators, and magnetostrictive actuators. 12. The acoustic noise suppressing mounting arrangement of claim 11 , wherein the plurality of structural spoke mounting assemblies are configured to actively minimize the transfer of the axial spoke vibrations to the wall of the outer duct. 13. The acoustic noise suppressing mounting arrangement of claim 11 , wherein the plurality of structural spoke mounting assemblies are configured to generate electricity by converting vibrational energy to electrical energy. 14. The acoustic noise suppressing mounting arrangement of claim 1 , further comprising at least one of a layer damping treatment applied to each structural spoke of the plurality of structural spokes, the outer duct, or both. 15. The acoustic noise suppressing mounting arrangement of claim 1 , wherein at least one structural spoke of the plurality of structural spokes comprises a secondary conduit configured to transfer at least one of electrical energy, signals, and fluids. 16. The acoustic noise suppressing mounting arrangement of claim 1 , wherein each structural spoke of the plurality of structural spokes is configured to preswirl a flow entering the outer duct or swirl a flow exiting the outer duct. 17. The acoustic noise suppressing mounting arrangement of claim 1 , further comprising acoustic vibration reduction treatments applied to at least one of an inside of the outer duct and a portion the central shaft assembly, wherein the acoustic vibration reduction treatment is configured to absorb acoustic energy. 18. The acoustic noise suppressing mounting arrangement of claim 1 , further comprising rub strips mounted to an inner wall of the outer duct. 19. The acoustic noise suppressing mounting arrangement of claim 1 , further comprising one or more spoke cross-members configured to connect two or more structural spokes together. 20. The acoustic noise suppressing mounting arrangement of claim 19 , wherein the one or more spoke cross-members are configured to prevent a foreign object or body part from being ingested into the ducted fan assembly.

Assignees

Inventors

Classifications

  • Preventing, counteracting or reducing vibration or noise · CPC title

  • Antivibration arrangements · CPC title

  • Ornithopters · CPC title

  • Rotorcraft characterised by having shrouded rotors, e.g. flying platforms · CPC title

  • B64C11/001Primary

    Shrouded propellers · CPC title

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Frequently asked questions

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What does patent US12195167B2 cover?
A general mounting method for ducted fan propulsors is disclosed. This mounting method uses extremely slender stators that connect the duct ring to the propulsor which is mounted in the middle and drives the rotor, fan or propeller. The slender stators take the form of spokes and as such are so slender that the midspan stresses within the spokes are dominated by axial tension loads rather than …
Who is the assignee on this patent?
Univ Kansas
What technology area does this patent fall under?
Primary CPC classification B64C11/001. Mapped technology areas include Operations & Transport.
When was this patent published?
Publication date Tue Jan 14 2025 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).