US2624615A - Spray apparatus - Google Patents
Spray apparatus Download PDFInfo
- Publication number
- US2624615A US2624615A US171385A US17138550A US2624615A US 2624615 A US2624615 A US 2624615A US 171385 A US171385 A US 171385A US 17138550 A US17138550 A US 17138550A US 2624615 A US2624615 A US 2624615A
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- US
- United States
- Prior art keywords
- spray
- passage
- valve
- liquid
- air
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Lifetime
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- 239000007921 spray Substances 0.000 title description 39
- 239000007788 liquid Substances 0.000 description 23
- 238000005507 spraying Methods 0.000 description 3
- 230000000694 effects Effects 0.000 description 2
- 241000238631 Hexapoda Species 0.000 description 1
- 206010061217 Infestation Diseases 0.000 description 1
- 241000607479 Yersinia pestis Species 0.000 description 1
- 238000000889 atomisation Methods 0.000 description 1
- 244000037666 field crops Species 0.000 description 1
- 239000002917 insecticide Substances 0.000 description 1
- 239000000463 material Substances 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 239000002420 orchard Substances 0.000 description 1
- 231100000614 poison Toxicity 0.000 description 1
- 230000007096 poisonous effect Effects 0.000 description 1
- 230000002000 scavenging effect Effects 0.000 description 1
- 238000009718 spray deposition Methods 0.000 description 1
Images
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D1/00—Dropping, ejecting, releasing, or receiving articles, liquids, or the like, in flight
- B64D1/16—Dropping or releasing powdered, liquid, or gaseous matter, e.g. for fire-fighting
Definitions
- My invention relates to apparatus for spraying liquid from airplanes and the principal object of my invention is to provide means by which air may be introduced into the body of spray liquid shortly before its passage into the spray forming head.
- Figure 1 is a side elevation of my spray apparatus, partly in section and with parts broken away to reduce the size of the figure.
- Fig. 2 is a vertical sectional view taken in the plane 2-2 of Fig. 1.
- Fig. 3 is a view similar to Fig. 1, but showing another embodiment of my invention.
- Fig. 4 and Fig. 5 are a view similar to Fig. 1, but showing another embodiment of my invention.
- the flow of spray liquid to the spray head can of course be stopped by suitable valve means in the supply passage, but means are needed for close control of the liquid which remains in the passage end after the closing of the valve, because with modern sprays, it is highly desirable, if not absolutely necessary, to limit the sprayed area with great accuracy. I have found that by introducing air into the passage after the flow of liquid has been cut off, the passage and spray head may be cleared almost instantly, whereas in the unvented passage, clearance may require up to five seconds.
- Another effect of introducing air into the liquid passage during a spraying operation is an increased fineness of spray which is very desirable under some conditions, although coarser or heavier spray is also desired under other conditions.
- My apparatus therefore gives a choice of fine or coarse spray as well as means for terminating the operation in a burst of fine spray practically instantaneously.
- a standard spray unit in which a body 2 including a valve housing 3 is mounted by means of a heavy feed pipe 4 on the wing of an airplane.
- a spray or atomizing head 6 fixed on one end of the shaft 1 is driven by the propeller 8 fixed on the other end.
- the shaft is journalled in the main portion of the body; and spray liquid flows into the body from the feed pipe, entering the passage 9 above the valve housing, thence into the'passage II! which extends through the'body to the spray head 6 which atomizes and throws it into the air.
- valve housing portion 3 of the body Arranged in the valve housing portion 3 of the body is a slightly tapered valve 12 of the plug valve type.
- the plug is secured snugly in the housing in the usual way, with a nut l3 and washer M on the small end, the larger end l6 being squared for the control lever l1, suitably connected for selective movement by the operator.
- the center portion of the plug is formed with a chamber [8, oppositely disposed ports I9 and 20 piercing the walls and permitting free flow through the passage 9 when the plug is turned to a position from that shown in Fig. 2. Also piercing the wall of the valve chamber on one side are three small aligned ports 2 I, positioned midway between the ports I9 and 20, and adapted to be placed in register with the housing ports 22, inside the scoop 23, which opens forwardly toward the propeller and in the direction taken by the plane in flight.
- the handle I! When it is desired to admit air into the flowing spray liquid, the handle I! is turned to register the port 20 in the larger passage 9, and the port IS in the larger passage l0; and the ports 2
- a full opening produces the finest atomization and the largest increase in volume of spray liquid distributed per unit of time.
- valve When conditions require a less finely atomized spray, the valve is turned to close the ports 22 with the unported wall 26 of the valve chamber, and align the ports 19 and 20 in the passages 9l0 respectively.
- valve may be turned to permit full flow of spray liquid without introduction of any air; or to cut off the flow of liquid while admitting air to scavenge the passage and spray head; or to admit air in controlled amounts into the flowing stream of the liquid.
- Figs. 3, 4 and 5 I have shown a modification of the structure just explained, using the spray apparatus of my Patent No. 2,090,950.
- is driven by the propeller 32, both being mounted on a shaft 33, journaled in the hollow body 34, which receives spray liquid through the feed pipe 36, controlled by the valve 31.
- the valve is wholly independent of the air intake and merely controls the flow of spray liquid into the passage 38 leading to the spray head.
- an air scoop is arranged to feed air tangentially into the passage.
- the scoop is formed by a vertically arranged elongated blister 39, cast integrally with the body, and having an aperture 4
- remains open at all times, contributing air to the stream of spray liquid flowing to the spray head, and scavenging the '4 passage of all liquid when the flow is cut off by the valve 31.
- a spray apparatus comprising a rotary spray head, a body on which the spray head is journaled and having a passage through the body through which spray liquid flows to the spray head, a valve housing in said body and enclosing a feed passage opening into said body passage, an aperture in the valve housing and opening into the feed passage, an air scoop on the valve housing around the aperture, and a valve in the valve housing to control simultaneously the flow of spray liquid through the feed passage and the flow of air from the scoop through said aperture to the feed passage.
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- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Nozzles (AREA)
Description
Jan 6, 1953 5 ROBERTSON 2,624,615
SPRAY APPARATUS Filed June 30, 1950 'I Tzg' J v //v VENTOP M/LTON S. ROBERTSON a K his AT TOFINEY Patented Jan. 6, 1953 UNITED STATES PATENT OFFICE Application June 30, 1950, Serial No. 171,385.
1 Claim.
My invention relates to apparatus for spraying liquid from airplanes and the principal object of my invention is to provide means by which air may be introduced into the body of spray liquid shortly before its passage into the spray forming head.
My invention has other objects and features of value, some of which with the foregoing will be set forth at length in the following description of my invention. It is to be understood that the invention is not limited to the forms shown in the drawings since the invention may be embodied in different forms as recited in the claim.
Referring to the drawings: Figure 1 is a side elevation of my spray apparatus, partly in section and with parts broken away to reduce the size of the figure. Fig. 2 is a vertical sectional view taken in the plane 2-2 of Fig. 1. Fig. 3 is a view similar to Fig. 1, but showing another embodiment of my invention. Fig. 4 and Fig. 5
are respectively vertical and horizontal sectional views taken in the planes 44 and -5 of Fig. 3, only the body shell being shown.
In recent years the spraying of orchards and field crops from airplanes has achieved major importance in the never ending fight against insect and other pest infestations. Close control of the liquid spray material has always been highly desirable, but with the advent of extremely powerful and poisonous insecticides accurate control has become essential.
The flow of spray liquid to the spray head can of course be stopped by suitable valve means in the supply passage, but means are needed for close control of the liquid which remains in the passage end after the closing of the valve, because with modern sprays, it is highly desirable, if not absolutely necessary, to limit the sprayed area with great accuracy. I have found that by introducing air into the passage after the flow of liquid has been cut off, the passage and spray head may be cleared almost instantly, whereas in the unvented passage, clearance may require up to five seconds.
Another effect of introducing air into the liquid passage during a spraying operation is an increased fineness of spray which is very desirable under some conditions, although coarser or heavier spray is also desired under other conditions. My apparatus therefore gives a choice of fine or coarse spray as well as means for terminating the operation in a burst of fine spray practically instantaneously.
In Fig. 1, I have shown a standard spray unit in which a body 2 including a valve housing 3 is mounted by means of a heavy feed pipe 4 on the wing of an airplane. A spray or atomizing head 6 fixed on one end of the shaft 1 is driven by the propeller 8 fixed on the other end. The shaft is journalled in the main portion of the body; and spray liquid flows into the body from the feed pipe, entering the passage 9 above the valve housing, thence into the'passage II! which extends through the'body to the spray head 6 which atomizes and throws it into the air.
Arranged in the valve housing portion 3 of the body is a slightly tapered valve 12 of the plug valve type. The plug is secured snugly in the housing in the usual way, with a nut l3 and washer M on the small end, the larger end l6 being squared for the control lever l1, suitably connected for selective movement by the operator.
The center portion of the plug is formed with a chamber [8, oppositely disposed ports I9 and 20 piercing the walls and permitting free flow through the passage 9 when the plug is turned to a position from that shown in Fig. 2. Also piercing the wall of the valve chamber on one side are three small aligned ports 2 I, positioned midway between the ports I9 and 20, and adapted to be placed in register with the housing ports 22, inside the scoop 23, which opens forwardly toward the propeller and in the direction taken by the plane in flight.
As shown in Fig. 2, flow of spray liquid through the valve and passage I!) has been cut off; and air from the scoop is flowing through the aligned ports 22 and 20, thence through the ports 2| into the passage I0. In this position of the valve, spray liquid in the passage Ill when the valve was turned to shut ofi the flow from the feed pipe, is rapidly forced to the spray head, the entire passage being cleared in the fraction of a second after closing of the valve.
When it is desired to admit air into the flowing spray liquid, the handle I! is turned to register the port 20 in the larger passage 9, and the port IS in the larger passage l0; and the ports 2| with the equal size ports 22, in more or less degree to give the effect desired, which can be observed by the operator. A full opening produces the finest atomization and the largest increase in volume of spray liquid distributed per unit of time.
When conditions require a less finely atomized spray, the valve is turned to close the ports 22 with the unported wall 26 of the valve chamber, and align the ports 19 and 20 in the passages 9l0 respectively.
Thus the valve may be turned to permit full flow of spray liquid without introduction of any air; or to cut off the flow of liquid while admitting air to scavenge the passage and spray head; or to admit air in controlled amounts into the flowing stream of the liquid.
In Figs. 3, 4 and 5, I have shown a modification of the structure just explained, using the spray apparatus of my Patent No. 2,090,950. The spray head 3| is driven by the propeller 32, both being mounted on a shaft 33, journaled in the hollow body 34, which receives spray liquid through the feed pipe 36, controlled by the valve 31. In this case the valve is wholly independent of the air intake and merely controls the flow of spray liquid into the passage 38 leading to the spray head.
On the side of the body 34 at the point where the spray liquid enters, an air scoop is arranged to feed air tangentially into the passage. Preferably the scoop is formed by a vertically arranged elongated blister 39, cast integrally with the body, and having an aperture 4| in the leading side near the top, and the enclosed chamber 42 opening at an angle into the bottom of the liquid passage as best shown in Figure 4.
The aperture 4| remains open at all times, contributing air to the stream of spray liquid flowing to the spray head, and scavenging the '4 passage of all liquid when the flow is cut off by the valve 31.
I claim:
A spray apparatus comprising a rotary spray head, a body on which the spray head is journaled and having a passage through the body through which spray liquid flows to the spray head, a valve housing in said body and enclosing a feed passage opening into said body passage, an aperture in the valve housing and opening into the feed passage, an air scoop on the valve housing around the aperture, and a valve in the valve housing to control simultaneously the flow of spray liquid through the feed passage and the flow of air from the scoop through said aperture to the feed passage.
MILTON S. ROBERTSON.
REFERENCES CITED The following references are of record in the file of this patent:
UNITED STATES PATENTS Number Name Date 2,048,847 Desmet July 28, 1936 2,090,950 Robertson Aug. 24, 1937 2,173,568 Streif Sept. 19, 1937 2,351,697 Nielsen June 20, 1944
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US171385A US2624615A (en) | 1950-06-30 | 1950-06-30 | Spray apparatus |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US171385A US2624615A (en) | 1950-06-30 | 1950-06-30 | Spray apparatus |
Publications (1)
Publication Number | Publication Date |
---|---|
US2624615A true US2624615A (en) | 1953-01-06 |
Family
ID=22623544
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US171385A Expired - Lifetime US2624615A (en) | 1950-06-30 | 1950-06-30 | Spray apparatus |
Country Status (1)
Country | Link |
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US (1) | US2624615A (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3114536A (en) * | 1958-11-26 | 1963-12-17 | Quigley Co | Furnace repair gun |
Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2048847A (en) * | 1934-04-02 | 1936-07-28 | E R Hawke | Liquid spray device |
US2090950A (en) * | 1936-06-12 | 1937-08-24 | Independent Crop Dusting Inc | Spray apparatus |
US2173568A (en) * | 1938-01-07 | 1939-09-19 | Robert J Streif | Liquid spray device for airplanes |
US2351697A (en) * | 1940-07-03 | 1944-06-20 | Nat Tube Co | Atomizer |
-
1950
- 1950-06-30 US US171385A patent/US2624615A/en not_active Expired - Lifetime
Patent Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2048847A (en) * | 1934-04-02 | 1936-07-28 | E R Hawke | Liquid spray device |
US2090950A (en) * | 1936-06-12 | 1937-08-24 | Independent Crop Dusting Inc | Spray apparatus |
US2173568A (en) * | 1938-01-07 | 1939-09-19 | Robert J Streif | Liquid spray device for airplanes |
US2351697A (en) * | 1940-07-03 | 1944-06-20 | Nat Tube Co | Atomizer |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3114536A (en) * | 1958-11-26 | 1963-12-17 | Quigley Co | Furnace repair gun |
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