Nozzle assembly for vehicle

Patent metadata

Field	Value
Publication number	US-2025079485-A1
Application number	US-202418791699-A
Country	US
Kind code	A1
Filing date	Aug 1, 2024
Priority date	Aug 29, 2023
Publication date	Mar 6, 2025
Grant date	—

Abstract

A nozzle assembly includes a first nozzle device that provides a fluid passage, in which a fluid flows, and a second nozzle device that surrounds the first nozzle device, and when an imaginary straight line passing through the fluid passage and extending in a direction, in which the fluid flows, is defined as a reference straight line, the first nozzle device includes a spacing area having a shape that is recessed in a direction that faces the reference straight line to be spaced apart from a portion of the second nozzle device. The nozzle assembly may be fixed to a body of a vehicle as part of an ejector for ejecting fluid having a pressure to a targeted location such as a hydrogen fuel cell of the vehicle.

First claim

What is claimed is:

1 . A nozzle assembly for vehicle comprising:
a first nozzle device configured to provide a fluid passage, in which a fluid flows; and a second nozzle device disposed to surround the first nozzle device, wherein when an imaginary straight line passing through the fluid passage and extending in a direction, in which the fluid flows, is defined as a reference straight line, the first nozzle device includes: a spacing area configured to be recessed in a direction that faces the reference straight line to be spaced apart from a portion of the second nozzle device.

2 . The nozzle assembly of claim 1 , wherein the spacing area is recessed in the direction that is a radial direction of the second nozzle device.

3 . The nozzle assembly of claim 1 , further comprising:
an attachment area having a shape protruding in a direction that becomes more distant from the reference straight line to be attached to another portion of the second nozzle device.

4 . The nozzle assembly of claim 3 , wherein a first distance that is a spacing distance between the spacing area and the reference straight line is smaller than a second distance that is a spacing distance between the attachment area and the reference straight line.

5 . The nozzle assembly of claim 3 , wherein the fluid passage is defined by an inner surface of the first nozzle device, and
wherein the inner surface of the first nozzle device includes: a first inner surface defining an inner surface of the spacing area and having a cape shape; and a second inner surface defining an inner surface of the attachment area and having a bay shape.

6 . The nozzle assembly of claim 5 , wherein a radius of curvature of the first inner surface in the radial direction that is a direction that is perpendicular to the reference straight line is greater than or equal to a radius of curvature of the second inner surface in the radial direction.

7 . The nozzle assembly of claim 5 , wherein the radial direction is defined as a direction that is perpendicular to the reference straight line, and
wherein a radius of curvature of at least a portion of an outer surface of the attachment area disposed on an opposite side of the second inner surface, in the radial direction, corresponds to a radius of curvature of at least a portion of an inner surface of the second nozzle device in the radial direction.

8 . The nozzle assembly of claim 3 , wherein when, among the radial directions, a direction that faces the reference straight line is defined as a contraction direction and, among the radial directions, a direction that becomes more distant from the reference straight line is defined as an expansion direction,
each of the first nozzle device and the second nozzle device is configured to be expanded in the expansion direction or contracted in the contraction direction with respect to the reference straight line in a state between a first state in which the fluid passage is not expanded, and a second state in which the fluid passage is expanded more than in the first state.

9 . The nozzle assembly of claim 8 , wherein an inner surface of the first nozzle device is configured to contact the fluid flowing in the fluid passage,
wherein the first nozzle device is configured to be expanded with respect to the reference straight line by the fluid in contact when a fluid pressure of the fluid is higher than a threshold pressure, and wherein the second nozzle device is configured to be expanded with respect to the reference straight line through expansion of the first nozzle device.

10 . The nozzle assembly of claim 9 , wherein a portion of an inner surface of the second nozzle device is configured to contact a portion of an outer surface of the first nozzle device,
wherein the second nozzle device is configured to be contacted with respect to the reference straight line by a restoring force when the fluid pressure of the fluid becomes lower from the state, in which the first nozzle device is expanded, and wherein the first nozzle device is configured to be contacted with respect to the reference straight line by the restoring force of the second nozzle device.

11 . The nozzle assembly of claim 8 , wherein when the first nozzle device is switched from the first state to the second state,
a displacement by which an end of the spacing area in the contraction direction is expanded with respect to the reference straight line is greater than a displacement by which an end of the attachment area in the contraction direction is expanded with respect to the reference straight line.

12 . The nozzle assembly of claim 8 , wherein the second nozzle device is configured to press the first nozzle device in the contraction direction when the first nozzle device is switched from the first state to the second state, and
wherein when the first nozzle device is in the second state, deformation of the attachment area of a first reference value or more is restricted by the second nozzle device, and deformation of the spacing area of a second reference value or more is restricted by the attachment area.

13 . The nozzle assembly of claim 12 , wherein the spacing area is configured to be deformed such that a radius of curvature thereof becomes greater when the first nozzle device is switched from the first state to the second state, and
wherein an expansion resisting force applied in the contraction direction is formed in the first nozzle device when the spacing area is deformed such that the radius of curvature becomes greater.

14 . The nozzle assembly of claim 8 , wherein the spacing area includes:
a first spacing area defining a side of the spacing area in the contraction direction and defining a portion of the fluid passage; and a second spacing area defining a side of the spacing area in the expansion direction and facing an inner surface of the second nozzle device, and wherein when the first nozzle device is in the second state, a compressive force is applied to the first spacing area, and a tensile force is applied to the second spacing area.

15 . The nozzle assembly of claim 14 , wherein an end of the first spacing area in the contraction direction has a shape that is convex in the contraction direction, and
wherein an end of the second spacing area in the expansion direction has a shape that is concave in the contraction direction.

16 . The nozzle assembly of claim 14 , wherein when the first nozzle device is in the first state, a first thickness that is the radial thickness of the first spacing area is greater than or equal to a second thickness that is the radial thickness of the second spacing area, and
wherein when an imaginary area formed between the first spacing area and the second spacing area with respect to the radial direction is a border area such that the first spacing area and the second spacing area are divided: the first thickness is defined as the radial spacing distance between an end of the first spacing area in the first state in the contraction direction and the border area, and the second thickness is defined as the radial spacing distance between an end of the second spacing area in the first state in the expansion direction and the border area.

17 . The nozzle assembly of claim 8 , wherein when the first nozzle device and the second nozzle device are switched from the first state to the second state,
a strain of the second nozzle device is smaller than or equal to a strain of the first nozzle device.

18 . The nozzle assembly of claim 1 , wherein a radial

Assignees

• Hyundai Motor Co Ltd
• Kia Corp

Inventors

• Jeong Pu Reum
• Shim Hyo Sub
• Park In Tae
• You Sung Jin
• Nam Sang Hyeok
• Ban Hyeon Seok
• Kim Hak Yoon

Classifications

• Y02E60/50

  Fuel cells · CPC title

• H01M2250/20

  Fuel cells in motive systems, e.g. vehicle, ship, plane · CPC title

• H01M8/04089

  of gaseous reactants · CPC title

• B05B15/14

  Arrangements for preventing or controlling structural damage to spraying apparatus or its outlets, e.g. for breaking at desired places; Arrangements for handling or replacing damaged parts · CPC title

• B05B1/06 Primary

  in annular, tubular or hollow conical form · CPC title