US4619845A
Expired / Lapsed
US
⏱️ 0.0 years remaining
Method for generating fine sprays of molten metal for spray coating and powder making
Assignee: United States Department of the Navy
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Filing: 1985-02-22
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Granted: 1986-10-28
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Expires: 2005-02-22
Abstract
Abstract A method for generating fine sprays of molten metal for spray coating and wder making is disclosed. Liquid metal is fed via a melt tube to a nozzle that is shaped like the frustrum of a cone. The nozzle is surrounded with gas jets in a coaxial pattern around the melt tube orifice. High pressure gas causes the formation of a low pressure region immediately next to the melt tube orifice that draws metal out of the orifice at a higher rate than would otherwise be the case. The coaxial gas stream atomizes the metal into droplets and thereafter forms a narrow, supersonic spray containing very fine metal droplets suitable for powder making or application of a coating.
Inventors
- 👤 Jack D. Ayers
- 👤 Iver E. Anderson
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-10-31 20:54
CPC Classifications
B; B22; B22F; B22F9/00; B22F9/02; B22F9/06; B22F9/08; B22F9/082; C; C23; C23C; C23C4/00; C23C4/12; C23C4/123
Claims Analysis
Total Claims: 12
Claim 1
Independent Claim
213 words
A method for generating a supersonic spray of atomized metal droplets, employing a melt nozzle having an exterior surface portion in the shape of the frustrum of a cone with a melt tube orifice at the center of the nozzle and with a plurality of gas jets coaxial to the nozzle flowing over said exterior surface portion, comprising the steps of: (a) liquifying metal and allowing it to flow into the melt tube orifice; (b) positioning the respective gas jets over circularly-spaced portions of the exterior surface portion so that a vector describing the direction of each gas jet has a positive first component in the same direction as the direction of metal flow from the melt tube orifice and a positive second component perpendicular to the direction of metal flow from the melt tube orifice; (c) establishing the input pressure to the gas jets at a pressure in excess of 1000 psig sufficient such that a pressure comes to exist at the melt tube orifice that is of smaller magnitude than that which exists when the gas jets are at zero input pressure; and, (d) adjusting the relative magnitudes of said first component and said second component of the gas jet direction vectors such that a spray having supersonic speed is produced.
Claim 2
Independent Claim
213 words
A method for generating a supersonic spray of atomized metal droplets, employing a melt nozzle having an exterior surface portion in the shape of the frustrum of a cone with a melt tube orifice at the center of the nozzle and with a plurality of gas jets coaxial to the nozzle flowing over said exterior surface portion, comprising the steps of: (a) liquifying metal and allowing it to flow into the melt tube orifice; (b) positioning the respective gas jets over circularly-spaced portions of the exterior surface portion so that a vector describing the direction of each gas jet has a positive first component in the same direction as the direction of metal flow from the melt tube orifice and a positive second component perpendicular to the direction of metal flow from the melt tube orifice; (c) establishing the input pressure to the gas jets at a pressure in excess of 1000 psig sufficient such that a pressure comes to exist at the melt tube orifice that is of smaller magnitude than that which exists when the gas jets are at zero input pressure; and, (d) adjusting the relative magnitudes of said first component and said second component of the gas jet direction vectors such that a spray having supersonic speed is produced.
Claim 3
Dependent Claim
38 words
The method of claim 1 comprising the further step of positioning the gas jets such that each of the gas jet direction vectors is parallel with the exterior surface portion of the cone congruent with the nozzle frustrum.
Claim 4
Dependent Claim
36 words
The method of claim 2 wherein the respective axis line of each gas jet is further positioned at a distance from the exterior nozzle cone surface substantially equal to the radius of the gas jet orifice.
Claim 5
Dependent Claim
42 words
The method of claim 1 wherein the respective axis line of each gas jet is positioned with respect to the inclined exterior surface of the nozzle frustrum such that substantially laminar as opposed to turbulent gas flow exits at said exterior surface.
Claim 6
Dependent Claim
37 words
The method of claim 4 wherein the respective axis line of each gas jet is further positioned at a distance from the said exterior nozzle cone surface substantially equal to the radius of the gas jet orifice.
Claim 7
Dependent Claim
51 words
The method of claim 5 wherein the said first and second components of the gas jet direction vectors are chosen such that the respective axis line of each gas jet intersects the axis line of the melt tube orifice at an intersection angle in the range of 0 to 25 degrees.
Claim 8
Dependent Claim
51 words
The method of claim 5 wherein the said first and second components of the gas jet direction vectors are chosen such that the respective axis line of each gas jet intersects the axis line of the melt tube orifice at an intersection angle in the range of 0 to 25 degrees.
Claim 9
Dependent Claim
14 words
The method of claim 5 wherein the said intersection angle is substantially 22.5 degrees.
Claim 10
Dependent Claim
18 words
The method of claim 8 wherein the gas inlet pressure is set at substantially 12.5 MPa (1800 psig.).
Claim 11
Independent Claim
277 words
A method for generating a supersonic spray of atomized metal droplets, employing a nozzle having an exterior surface portion in the shape of the frustrum of a cone, with a melt tube orifice at the center of the nozzle, and with a plurality of gas jets coaxial to the nozzle, comprising the steps of: (a) liquifying metal and allowing it to flow into the melt tube orifice; (b) positioning the gas jet over circularly-spaced portions of the exterior surface portion so that a vector describing the direction of each gas jet has a positive first component in the same direction as the direction of metal flow from the melt tube orifice and a positive second component perpendicular to the direction of metal flow from the melt tube orifice; (c) further positioning the respective gas jets such that each gas jet vector is parallel with the exterior surface of the cone congruent with the nozzle frustrum (d) further positioning the respective axis line of each gas jet at a distance from said exterior cone surface substantially equal to the radius of the gas jet orifice (e) further positioning the gas jets such that the intersection angle between the respective axis line of each gas jet and the axis line projecting from the melt tube orifice is substantially 22.5 degrees (f) establishing a gas inlet pressure to the coaxial gas jets in the range of 10MPa to 17.5 MPa; and (e) further adjusting the gas inlet pressure to the said gas jets such that a pressure is established at the melt tube orifice which is lower than that pressure which exists when the said gas inlet pressure is zero.
Claim 12
Independent Claim
277 words
A method for generating a supersonic spray of atomized metal droplets, employing a nozzle having an exterior surface portion in the shape of the frustrum of a cone, with a melt tube orifice at the center of the nozzle, and with a plurality of gas jets coaxial to the nozzle, comprising the steps of: (a) liquifying metal and allowing it to flow into the melt tube orifice; (b) positioning the gas jet over circularly-spaced portions of the exterior surface portion so that a vector describing the direction of each gas jet has a positive first component in the same direction as the direction of metal flow from the melt tube orifice and a positive second component perpendicular to the direction of metal flow from the melt tube orifice; (c) further positioning the respective gas jets such that each gas jet vector is parallel with the exterior surface of the cone congruent with the nozzle frustrum (d) further positioning the respective axis line of each gas jet at a distance from said exterior cone surface substantially equal to the radius of the gas jet orifice (e) further positioning the gas jets such that the intersection angle between the respective axis line of each gas jet and the axis line projecting from the melt tube orifice is substantially 22.5 degrees (f) establishing a gas inlet pressure to the coaxial gas jets in the range of 10MPa to 17.5 MPa; and (e) further adjusting the gas inlet pressure to the said gas jets such that a pressure is established at the melt tube orifice which is lower than that pressure which exists when the said gas inlet pressure is zero.
References Cited (Backward Citations)
USPTO Annuity & Maintenance Windows
| Annuity Stage | Window Opens | Payment Deadline | Surcharge Period Until | Estimated Fee | Status |
|---|---|---|---|---|---|
| 3.5 Years (Year 4) | 1989-10-27 | 1990-04-28 | 1990-10-28 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1993-10-27 | 1994-04-28 | 1994-10-28 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1997-10-27 | 1998-04-28 | 1998-10-28 | $7700.00 | Window Closed / Lapsed |