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Air discharge device

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  • Publication Date:
    October 01, 2024
  • معلومة اضافية
    • Patent Number:
      12103,364
    • Appl. No:
      17/064831
    • Application Filed:
      October 07, 2020
    • نبذة مختصرة :
      An air discharge device includes a duct that defines a flow passage through which a working air flow to be discharged passes, and a hole forming member defining an air discharge hole as an outlet of the working air flow. The hole forming member has a vortex generation structure configured to generate an auxiliary vortex having a vortex characteristic including a vortex rotation direction and a vortex axis direction. The vortex characteristic of the auxiliary vortex is different from that of a lateral vortex generated by the working air flow at a downstream side of the air discharge hole. The vortex generation structure is configured in the hole forming member so that the auxiliary vortex collides with the lateral vortex in a state where at least one of the vortex rotation direction and the vortex axial direction of the vortex characteristic is different from that of the lateral vortex.
    • Inventors:
      DENSO CORPORATION (Kariya, JP)
    • Assignees:
      DENSO CORPORATION (Kariya, JP)
    • Claim:
      1. An air discharge device comprising: a duct defining a flow passage through which a working air flow passes to be blown toward a discharge target; and a hole forming member defining an air discharge hole located at a downstream air side of the duct, as an air outlet from which the working air flow is blown out, wherein the hole forming member has a vortex generation structure configured to generate an auxiliary vortex having a vortex characteristic including a vortex rotation direction and a vortex axis direction, different from that of a lateral vortex generated by the working air flow at a downstream air side of the air discharge hole, the vortex generation structure is configured in the hole forming member such that the auxiliary vortex collides with the lateral vortex in a state where at least one of the vortex rotation direction and the vortex axial direction of the vortex characteristic of the auxiliary vortex is different from that of the lateral vortex, the vortex generation structure includes a plurality of auxiliary holes arranged along a peripheral edge portion of the hole forming member surrounding the air discharge hole, and the plurality of auxiliary holes are configured to generate a plurality of the auxiliary vortices different from the lateral vortices in at least one of the vortex rotation direction and the vortex axial direction, the peripheral edge portion of the hole forming member surrounding the air discharge hole includes a first edge and a second edge that are opposed to each other and extend with a predetermined distance therebetween, a third edge connecting one ends of the first edge and the second edge, and a fourth edge connecting the other ends of the first edge and the second edge, the first edge and the second edge configure a pair of long edges facing each other with a distance therebetween, smaller than a distance between the third edge and the fourth edge, the third edge and the fourth edge configure a pair of short edges facing each other with a distance therebetween, larger than the distance between the first edge and the second edge, the plurality of auxiliary holes are provided in the peripheral edge portion of the hole forming member surrounding the air discharge hole mainly on the edge sides of the pair of long edges such that the plurality of auxiliary vortices are less likely to be generated on the edge sides of the pair of short edges than on the edge sides of the pair of long edges, and an inner wall surface of each of the plurality of auxiliary holes from an upstream end to a downstream end is parallel with an inner wall surface of the duct separating an auxiliary air flow from the working air flow.
    • Claim:
      2. The air discharge device according to claim 1 , wherein the air discharge hole has a flat open shape, the peripheral edge portion of the hole forming member surrounding the air discharge hole includes the pair of long edges facing each other in a short axial direction, and the pair of short edges facing each other in a long axial direction and continuously connected with the pair of long edges, the short edge having a length smaller than a length of the long edge.
    • Claim:
      3. The air discharge device according to claim 1 , wherein the plurality of auxiliary holes are provided in the pair of long edges and are not provided in the pair of short edges.
    • Claim:
      4. The air discharge device according to claim 1 , wherein the third edge and the fourth edge configure a pair of curved short edges facing each other with the distance therebetween larger than the distance between the first edge and the second edge.
    • Claim:
      5. The air discharge device according to claim 1 , wherein the air discharge hole has an elliptical shape.
    • Claim:
      6. An air discharge device comprising: a duct defining a flow passage through which a working air flow passes to be blown toward a discharge target; and a hole forming member defining an air discharge hole located at a downstream air side of the duct, as an air outlet from which the working air flow is blown out, wherein the hole forming member has a vortex generation structure configured to generate an auxiliary vortex having a vortex characteristic including a vortex rotation direction and a vortex axis direction, different from that of a lateral vortex generated by the working air flow at a downstream air side of the air discharge hole, the vortex generation structure is configured in the hole forming member such that the auxiliary vortex collides with the lateral vortex in a state where at least one of the vortex rotation direction and the vortex axial direction of the vortex characteristic of the auxiliary vortex is different from that of the lateral vortex, the vortex generation structure includes a plurality of auxiliary holes arranged along a peripheral edge portion of the hole forming member surrounding the air discharge hole, and the plurality of auxiliary holes are configured to generate a plurality of the auxiliary vortices different from the lateral vortices in at least one of the vortex rotation direction and the vortex axial direction, the air discharge hole has a flat open shape, the peripheral edge portion of the hole forming member surrounding the air discharge hole includes a pair of long edges facing each other in a short axial direction, and a pair of short edges facing each other in a long axial direction and continuously connected with the pair of long edges, the short edge having a length smaller than a length of the long edge, the plurality of auxiliary holes are provided in the peripheral edge portion of the hole forming member surrounding the air discharge hole mainly in the pair of long edges such that the plurality of auxiliary vortices are less likely to be generated on the edge sides of the pair of short edges than on the edge sides of the pair of long edges, and an inner wall surface of each of the plurality of auxiliary holes from an upstream end to a downstream end is parallel with an inner wall surface of the duct separating an auxiliary air flow from the working air flow.
    • Claim:
      7. The air discharge device according to claim 6 , wherein the peripheral edge portion of the hole forming member surrounding the air discharge hole includes the pair of long edges facing each other in the short axial direction, and a pair of curved short edges facing each other in the long axial direction and continuously connected with the pair of long edges.
    • Patent References Cited:
      20110039491 February 2011 Khalifa
      20150300385 October 2015 Akagi et al.
      104769367 July 2015
      H08210943 August 1996
      H08318176 December 1996
      2007255879 October 2007
      2017116228 June 2017


    • Other References:
      U.S. Appl. No. 17/065,045, filed Oct. 7, 2020, Jun Yamaoka, et al. cited by applicant
      U.S. Appl. No. 17/065,267, filed Oct. 7, 2020, Jun Yamaoka, et al. cited by applicant
      Makito Sakai et al. Study on Flow Characteristics of a Plane Jet Perturbed by Tabs at the Slit Nozzle Exit. In: The Japan Society of Mechanical Fluid Engineering Division (Nov. 12-13, 2016, Ube) Copyright © 2016 Japan Society of Mechanical Engineers. cited by applicant
    • Primary Examiner:
      Schult, Allen R. B.
    • Attorney, Agent or Firm:
      Harness, Dickey & Pierce, P.L.C.
    • الرقم المعرف:
      edspgr.12103364