US2443856A - Flow measuring mechanism - Google Patents
Flow measuring mechanism Download PDFInfo
- Publication number
- US2443856A US2443856A US551739A US55173944A US2443856A US 2443856 A US2443856 A US 2443856A US 551739 A US551739 A US 551739A US 55173944 A US55173944 A US 55173944A US 2443856 A US2443856 A US 2443856A
- Authority
- US
- United States
- Prior art keywords
- impeller
- bearing
- support
- flow measuring
- measuring mechanism
- 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
Links
Images
Classifications
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01F—MEASURING VOLUME, VOLUME FLOW, MASS FLOW OR LIQUID LEVEL; METERING BY VOLUME
- G01F1/00—Measuring the volume flow or mass flow of fluid or fluent solid material wherein the fluid passes through a meter in a continuous flow
- G01F1/05—Measuring the volume flow or mass flow of fluid or fluent solid material wherein the fluid passes through a meter in a continuous flow by using mechanical effects
- G01F1/10—Measuring the volume flow or mass flow of fluid or fluent solid material wherein the fluid passes through a meter in a continuous flow by using mechanical effects using rotating vanes with axial admission
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01P—MEASURING LINEAR OR ANGULAR SPEED, ACCELERATION, DECELERATION, OR SHOCK; INDICATING PRESENCE, ABSENCE, OR DIRECTION, OF MOVEMENT
- G01P5/00—Measuring speed of fluids, e.g. of air stream; Measuring speed of bodies relative to fluids, e.g. of ship, of aircraft
- G01P5/02—Measuring speed of fluids, e.g. of air stream; Measuring speed of bodies relative to fluids, e.g. of ship, of aircraft by measuring forces exerted by the fluid on solid bodies, e.g. anemometer
- G01P5/06—Measuring speed of fluids, e.g. of air stream; Measuring speed of bodies relative to fluids, e.g. of ship, of aircraft by measuring forces exerted by the fluid on solid bodies, e.g. anemometer using rotation of vanes
Definitions
- the present invention relates to liquid flow measuring devices, and is more particularly concerned with flow mechanisms of the character in which a submerged spinner or impeller is employed to transmit electric impulses to an indi- :cator mechanism.
- Such devices are used to either indicate a ships speed of travel, or to indicate the rate of liquidfiow through a conduit.
- the invention is disclosed as applied to a ships leg, but it is not limited to such use.
- Another important object is to provide an impeller which, when incorporated in a ship's log, will accurately respond to all speeds of the ship, and yield a. speed of rotation which is substantially exactly proportional thereto, and which is so constructed that its response or sensitivity will not be impaired throughout its life, even when operated under extremely corrosive conditions.
- Another object is to provide a unitary impeller mechanism embodying an impeller which is so supported that it will in eifect float on a single pivot during operation, thereby minimizing wear and resistance to rotation.
- a further object is to provide a novel assembly for restraining fluid flow-actuated impellers against removal from their supporting shafts, and yet which may readily be removed when desired.
- Fig. l is a vertical sectional view through the impeller mechanism of the invention.
- Fig. 2 is an elevational view, on a reduced scale, of the retainer employed to hold the impeller on its shaft.
- the unit is carried by a cylindrical support I! which is supported on the ships hull below the water line in well-known manner, so as to subject the impeller to the force of the water in response to forward travel of the ship.
- Support l2 Tightly fitting within support ll, is-a flanged support l2, having a cylindrical forwardly directed shaft portion [3.
- Support l2 may be secured in place in any well-known manner, as for instance by means of a fusible ring i-l, coacting with flange [5 of the support, which forms a water-tight seal between the parts.
- the novel impeller of the invention is made up of two mating streamlined parts It and I! threadedly connected together at 18.
- Part I6 is provided with any suitable number of impeller blades 59 (preferably 4) having the desired pitch.
- Tightly threaded into impeller section i6 is a bushing 2
- Secured in place within impeller section 16, by means of the flange of sleeve 21 is a magnetic ring 23 for a purpose that will presently appear.
- is provided with a narrow face 24 having journalled engagement with shaft portion l3 of the support. This affords the sole support for the aft end of the impeller.
- most of the bearing load during operation is, taken by the forward bearing, which will now be described.
- the forward or cap portion of the impeller is provided with a recess into which a special corrosion-resistant bearing 25 is tightly fitted.
- the latter is provided with a generally conical bearing socket 2B, which cooperateswith a post or spindle bearing 21, which is also constructed of corrosion and wear-resistant material.
- Bearing 21 is of shouldered form and :has its shank tightly fitted into a bore 28 in the end of support I3.
- Bearings 25 and 21 may be constructed of any suitable material which has the requisite resistance to corrosion, and the ability to resist wear when exposed to the action of salt water in the absence of all lubrication. I have found that bearings constructed of tungsten carbide have proved very satisfactory. It is to be understood however, that other hard and corrosionresistant materials such as glass, and the like may be used. As seen in Fig. 1, the walls of bearing recess 26 diverge to a materially greater extent than the walls of bearing 21, and the radius of pivot 21 is also somewhat smaller than the radius of bearing recess .26, with the result that the area of contact is localized over a very small portion of the end of bearing 21, and friction is accordingly minimized.
- the impeller may be restrained against tendencies for it to be displaced from support l3, as for instance when the ship is proceeding astern, by any suitable means.
- support I3 is provided, adjacent its free end, with an annular recess 32 into which a split snap ring 33 is fitted. The latter bears against the hub section 3d of impeller section iii and limits forward travel of the impeller unit. A slight amount of end-play 30 is provided to insure against binding of the parts.
- Rotation of the impeller is transmitted to the indicating mechanism by means of a magnetic member 36 carried by a shaft 3? and disposed in flux linking relationship with magnetic member 23 through a Wall 38 of support I2.
- a second support 39 threaded into support i2, carries a contact make and break assembly actuated by shaft 3 1 (not shown).
- support 12 is made of stainless steel; bushing 2i of Phosphor bronze; the impeller of nickel silver or high nickel-copper alloys and retainer 33 of beryllium copper.
- the remaining parts may be made of bronze.
- an impeller mechanism' is provided which is of simple but yet efficient and rugged form, and one which does not require the use of sealing devices to exclude the ingress of sea water, and at the same time the bearing assembly is of such construction that the sea water is apparently capable of functioning as a lubricant, and friction is reduced to such a small value that accurate rotational response of the impeller in response to speed of the ship is achieved.
- an impeller mechanism a cylindrical member supported at one end and having an annular recess adjacent its free end; a two part impeller including an aft part journalled on said member and a cap portion fitting over the free end of said member and embodying thrust bearing means; and retainer means associated with said aft section and cooperating with said recess to prevent removal of said impeller from said member, said retainer means being housed by said cap portion.
- an impeller mechanism for a ships log or the like, a, generally cylindrical member supported at its aft end; a two-part impeller unit comprising an aft section journalled on said member and having xternal impeller vanes, and a cap section tightlysecured to said aft section and enclosing the free end of said member; thrust bearing means provided in said cap section for limiting aft movement of said impeller unit on said member; and retainer means coacting with said member and said impeller unit for limiting fore movement of saidimpeller assembly along said member, said retainer means being removable to permit said aft section to he slid off of the free end of said member, and said cap section, when in place on said aft section, being'operable to enclose and prevent removal of said retainer means.
Landscapes
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Fluid Mechanics (AREA)
- Sliding-Contact Bearings (AREA)
Description
'June 22, 1948. H N Y V 2,443,856
FLOW MEASURING MECHANISM Filed Aug. 29, 1944 INVENTOR. Hemr/ch Herman/7y BY ighz.
Afro/2N5 Y Patented June 22, 1948 UNITED STATES PATENT OFFICE FLOW MEASURING MECHANISM Heinrich Hermanny, Valley Stream, N. Y., assignor to Bendix Aviation Corporation, Brooklyn, N. Y., a corporation of Delaware Application August 29, 1944, Serial No. 551,739
3 Claims.
The present invention relates to liquid flow measuring devices, and is more particularly concerned with flow mechanisms of the character in which a submerged spinner or impeller is employed to transmit electric impulses to an indi- :cator mechanism. Such devices are used to either indicate a ships speed of travel, or to indicate the rate of liquidfiow through a conduit. The invention is disclosed as applied to a ships leg, but it is not limited to such use.
The devices of this character which have been heretofore proposed have not proven altogether satisfactory because they are of such construction as to require lubrication, and it has been found that after they have been in service for some time, sea water finds its way into the lubrication chamber, thereby contaminating the lubricant and causing corrosion of the bearing parts, with resultant failure of the unit to give correct speed indications. Also, it has been found that the substantial oil film, or other'means required for the purpose of forming an oil seal, imposes considerable resistance to rotation of the impeller, with the result that it is impossible to secure the desired ratio between impeller speed and the actual speed of the ship, in such prior devices.
It is accordingly the major object of this invention to provide a liquid-actuated, impeller which requires no lubrication and yet is of simple, long-lif e construction.
Another important object is to provide an impeller which, when incorporated in a ship's log, will accurately respond to all speeds of the ship, and yield a. speed of rotation which is substantially exactly proportional thereto, and which is so constructed that its response or sensitivity will not be impaired throughout its life, even when operated under extremely corrosive conditions.
Another object is to provide a unitary impeller mechanism embodying an impeller which is so supported that it will in eifect float on a single pivot during operation, thereby minimizing wear and resistance to rotation.
A further object is to provide a novel assembly for restraining fluid flow-actuated impellers against removal from their supporting shafts, and yet which may readily be removed when desired.
Further objects will become apparent as the specification proceeds in conjunction with the annexed drawings, and from the annexed claims.
In the drawings:
Fig. l is a vertical sectional view through the impeller mechanism of the invention, and
Fig. 2 is an elevational view, on a reduced scale, of the retainer employed to hold the impeller on its shaft.
With reference to the drawings, in which like reference characters have been employed to designate similar parts throughout the several views, the unit is carried by a cylindrical support I! which is supported on the ships hull below the water line in well-known manner, so as to subject the impeller to the force of the water in response to forward travel of the ship.
Tightly fitting within support ll, is-a flanged support l2, having a cylindrical forwardly directed shaft portion [3. Support l2 may be secured in place in any well-known manner, as for instance by means of a fusible ring i-l, coacting with flange [5 of the support, which forms a water-tight seal between the parts.
The novel impeller of the invention is made up of two mating streamlined parts It and I! threadedly connected together at 18. Part I6 is provided with any suitable number of impeller blades 59 (preferably 4) having the desired pitch. Tightly threaded into impeller section i6 is a bushing 2|, having a plurality of openings '22 for application of a spanner wrench. Secured in place within impeller section 16, by means of the flange of sleeve 21 is a magnetic ring 23 for a purpose that will presently appear. As seen in Fig. 1, bushing 2| is provided with a narrow face 24 having journalled engagement with shaft portion l3 of the support. This affords the sole support for the aft end of the impeller. However, due to the novel manner in which the assembly is made, most of the bearing load during operation is, taken by the forward bearing, which will now be described.
The forward or cap portion of the impeller is provided with a recess into which a special corrosion-resistant bearing 25 is tightly fitted. The latter is provided with a generally conical bearing socket 2B, which cooperateswith a post or spindle bearing 21, which is also constructed of corrosion and wear-resistant material. Bearing 21 is of shouldered form and :has its shank tightly fitted into a bore 28 in the end of support I3.
I have found that by constructing an impeller unit in the manner disclosed, and freely permitting the ingress of sea water along passage 29 into space 3|, a perfectly performing construction is achieved and one in which the sea water apparently functions as a lubricant for the bearings.
The impeller may be restrained against tendencies for it to be displaced from support l3, as for instance when the ship is proceeding astern, by any suitable means. However, I have found that the novel means which will now be described has proven very satisfactory, and is of simple and eilicient form. Support I3 is provided, adjacent its free end, with an annular recess 32 into which a split snap ring 33 is fitted. The latter bears against the hub section 3d of impeller section iii and limits forward travel of the impeller unit. A slight amount of end-play 30 is provided to insure against binding of the parts.
When it is desired to disassemble the unit, all that is necessary is to unscrew cap H from hub 34, remove snap ring 33, by shifting it radially and slide the impeller oil the end of the shaft, anopening 35 in the snap ring permitting insertion of a tool, in well-known manner.
Rotation of the impeller is transmitted to the indicating mechanism by means of a magnetic member 36 carried by a shaft 3? and disposed in flux linking relationship with magnetic member 23 through a Wall 38 of support I2. A second support 39, threaded into support i2, carries a contact make and break assembly actuated by shaft 3 1 (not shown).
While any suitable corrosion-resistant materials may be used for the other parts of the device, I have found that very satisfactory results are obtained when support 12 is made of stainless steel; bushing 2i of Phosphor bronze; the impeller of nickel silver or high nickel-copper alloys and retainer 33 of beryllium copper. The remaining parts may be made of bronze.
From the foregoing detailed disclosure of the invention, it is apparent that an impeller mechanism'is provided which is of simple but yet efficient and rugged form, and one which does not require the use of sealing devices to exclude the ingress of sea water, and at the same time the bearing assembly is of such construction that the sea water is apparently capable of functioning as a lubricant, and friction is reduced to such a small value that accurate rotational response of the impeller in response to speed of the ship is achieved. Also,
bearing 25 and 21 in engagement, so that the the force of the Water maintains,
7 are therefore intended to be embraced thereby.
What is claimed is:
1. 'In an impeller mechanism, a cylindrical member supported at one end and having an annular recess adjacent its free end; a two part impeller including an aft part journalled on said member and a cap portion fitting over the free end of said member and embodying thrust bearing means; and retainer means associated with said aft section and cooperating with said recess to prevent removal of said impeller from said member, said retainer means being housed by said cap portion.
2. The impeller mechanism defined in claim 1, wherein saidretainer means is removable by shifting it radially, and said cap, when in place on said aft section, is operable to prevent such removal.
3. In an impeller mechanism for a ships log or the like, a, generally cylindrical member supported at its aft end; a two-part impeller unit comprising an aft section journalled on said member and having xternal impeller vanes, and a cap section tightlysecured to said aft section and enclosing the free end of said member; thrust bearing means provided in said cap section for limiting aft movement of said impeller unit on said member; and retainer means coacting with said member and said impeller unit for limiting fore movement of saidimpeller assembly along said member, said retainer means being removable to permit said aft section to he slid off of the free end of said member, and said cap section, when in place on said aft section, being'operable to enclose and prevent removal of said retainer means.
HEINRICH HERMANNY.
REFERENCES CITED The following references are of record in the file of this patent:
UNITED STATES PATENTS Number Name Date 563,480 Greenleaf July 7, 1896 794,932 Fullerton July 18, 1905 986,423 Coleman Mar. 7, 1911 997,553 Hill July 11, 1911 1,421,405 Chernikeeff July 4, 1922 FOREIGN PATENTS Number Country I Date 610,705 France June 14, 1926
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US551739A US2443856A (en) | 1944-08-29 | 1944-08-29 | Flow measuring mechanism |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US551739A US2443856A (en) | 1944-08-29 | 1944-08-29 | Flow measuring mechanism |
Publications (1)
Publication Number | Publication Date |
---|---|
US2443856A true US2443856A (en) | 1948-06-22 |
Family
ID=24202483
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US551739A Expired - Lifetime US2443856A (en) | 1944-08-29 | 1944-08-29 | Flow measuring mechanism |
Country Status (1)
Country | Link |
---|---|
US (1) | US2443856A (en) |
Cited By (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2732021A (en) * | 1956-01-24 | Corrosion preventing fairwater caps | ||
US2770131A (en) * | 1954-07-19 | 1956-11-13 | Ray C Sparling | Flowmeter |
US3180625A (en) * | 1963-07-23 | 1965-04-27 | Wyco Tool Co | Power transmission means for concrete vibrator |
US3299721A (en) * | 1963-12-23 | 1967-01-24 | Gen Motors Corp | Windshield wiper drive and universal joint therefor |
US3329472A (en) * | 1963-08-13 | 1967-07-04 | Ampep Ind Products Ltd | Bearing units |
US3495884A (en) * | 1968-01-02 | 1970-02-17 | Texas Instruments Inc | Composite material for use in bearing structures and the like |
US3580170A (en) * | 1968-08-30 | 1971-05-25 | Texaco Inc | Support assembly for a travel cylinder having rolling contact with the bed of a printing machine |
US3614180A (en) * | 1969-03-19 | 1971-10-19 | Aga Ab | Bearing arrangement for a rotor |
US3726572A (en) * | 1969-05-14 | 1973-04-10 | Smiths Industries Ltd | Gas-lubricated bearings |
US4077742A (en) * | 1976-03-05 | 1978-03-07 | Goodwin Wendell W | Propeller shaft anodic protector kit |
US5261221A (en) * | 1990-06-27 | 1993-11-16 | Fritz Stahlecker | Open-end spinning rotor assembly |
Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US563480A (en) * | 1896-07-07 | Reenleaf | ||
US794932A (en) * | 1904-09-01 | 1905-07-18 | John D Fullerton | Propeller. |
US986423A (en) * | 1909-07-06 | 1911-03-07 | Edgar P Coleman | Fluid-meter. |
US997553A (en) * | 1910-12-14 | 1911-07-11 | Alva T Hill | Water-meter. |
US1421405A (en) * | 1921-12-09 | 1922-07-04 | Chernikeeff Basil | Ship's log |
FR610705A (en) * | 1926-02-06 | 1926-09-11 | Fluid flow rate measuring device |
-
1944
- 1944-08-29 US US551739A patent/US2443856A/en not_active Expired - Lifetime
Patent Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US563480A (en) * | 1896-07-07 | Reenleaf | ||
US794932A (en) * | 1904-09-01 | 1905-07-18 | John D Fullerton | Propeller. |
US986423A (en) * | 1909-07-06 | 1911-03-07 | Edgar P Coleman | Fluid-meter. |
US997553A (en) * | 1910-12-14 | 1911-07-11 | Alva T Hill | Water-meter. |
US1421405A (en) * | 1921-12-09 | 1922-07-04 | Chernikeeff Basil | Ship's log |
FR610705A (en) * | 1926-02-06 | 1926-09-11 | Fluid flow rate measuring device |
Cited By (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2732021A (en) * | 1956-01-24 | Corrosion preventing fairwater caps | ||
US2770131A (en) * | 1954-07-19 | 1956-11-13 | Ray C Sparling | Flowmeter |
US3180625A (en) * | 1963-07-23 | 1965-04-27 | Wyco Tool Co | Power transmission means for concrete vibrator |
US3329472A (en) * | 1963-08-13 | 1967-07-04 | Ampep Ind Products Ltd | Bearing units |
US3299721A (en) * | 1963-12-23 | 1967-01-24 | Gen Motors Corp | Windshield wiper drive and universal joint therefor |
US3495884A (en) * | 1968-01-02 | 1970-02-17 | Texas Instruments Inc | Composite material for use in bearing structures and the like |
US3580170A (en) * | 1968-08-30 | 1971-05-25 | Texaco Inc | Support assembly for a travel cylinder having rolling contact with the bed of a printing machine |
US3614180A (en) * | 1969-03-19 | 1971-10-19 | Aga Ab | Bearing arrangement for a rotor |
US3726572A (en) * | 1969-05-14 | 1973-04-10 | Smiths Industries Ltd | Gas-lubricated bearings |
US4077742A (en) * | 1976-03-05 | 1978-03-07 | Goodwin Wendell W | Propeller shaft anodic protector kit |
US5261221A (en) * | 1990-06-27 | 1993-11-16 | Fritz Stahlecker | Open-end spinning rotor assembly |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
US2443856A (en) | Flow measuring mechanism | |
US6617731B1 (en) | Rotary pump with bearing wear indicator | |
US2770131A (en) | Flowmeter | |
US3531988A (en) | Knotmeter | |
GB1159899A (en) | Consistometer | |
SE444056B (en) | SEALING DEVICE AT PROPELLER SHAFT | |
US3111904A (en) | Turbine pump | |
US2559767A (en) | Variable pitch propeller | |
US2300362A (en) | Bearing for integrating and like meters | |
US2405799A (en) | Bearing | |
US2465930A (en) | Bushing mounting for rotary pumps | |
US3614180A (en) | Bearing arrangement for a rotor | |
US3771362A (en) | Fluid velocity indicator | |
GB1138373A (en) | Bearing | |
US2862733A (en) | Outboard bearing seal for marine propellers | |
US2473061A (en) | Shaft seal | |
US3228236A (en) | Apparatus for corrosion-erosion testing | |
US2089134A (en) | Apparatus for indicating or recording the rate of flow of fluids | |
US2538921A (en) | Bearing | |
US3131943A (en) | Rotary mechanical seal | |
US3061384A (en) | Thrust bearing | |
US771826A (en) | Device for measuring the speed of flowing liquids. | |
US3201083A (en) | Slurry flowmeter | |
US2400028A (en) | Bearing | |
US2389125A (en) | Fluid meter |