US707135A - Device for the prevention of erosion in ordnance. - Google Patents
Device for the prevention of erosion in ordnance. Download PDFInfo
- Publication number
- US707135A US707135A US69692798A US1898696927A US707135A US 707135 A US707135 A US 707135A US 69692798 A US69692798 A US 69692798A US 1898696927 A US1898696927 A US 1898696927A US 707135 A US707135 A US 707135A
- Authority
- US
- United States
- Prior art keywords
- ring
- pressure
- projectile
- obturating
- base
- 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
- 230000003628 erosive effect Effects 0.000 title description 5
- 230000002265 prevention Effects 0.000 title description 5
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 description 8
- 229910052802 copper Inorganic materials 0.000 description 8
- 239000010949 copper Substances 0.000 description 8
- 229940108928 copper Drugs 0.000 description 8
- 239000007789 gas Substances 0.000 description 8
- 239000000463 material Substances 0.000 description 6
- 230000002093 peripheral effect Effects 0.000 description 5
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 description 4
- 239000002657 fibrous material Substances 0.000 description 3
- 239000002184 metal Substances 0.000 description 3
- 229910052751 metal Inorganic materials 0.000 description 3
- 229910000831 Steel Inorganic materials 0.000 description 2
- 229910052742 iron Inorganic materials 0.000 description 2
- 239000010959 steel Substances 0.000 description 2
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 1
- 229920000742 Cotton Polymers 0.000 description 1
- 240000003936 Plumbago auriculata Species 0.000 description 1
- 239000010425 asbestos Substances 0.000 description 1
- 238000002485 combustion reaction Methods 0.000 description 1
- 235000014987 copper Nutrition 0.000 description 1
- 239000003984 copper intrauterine device Substances 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 239000004744 fabric Substances 0.000 description 1
- 239000010439 graphite Substances 0.000 description 1
- 235000015250 liver sausages Nutrition 0.000 description 1
- 239000000314 lubricant Substances 0.000 description 1
- 230000001050 lubricating effect Effects 0.000 description 1
- 239000000203 mixture Substances 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 239000003921 oil Substances 0.000 description 1
- 239000012188 paraffin wax Substances 0.000 description 1
- 239000000843 powder Substances 0.000 description 1
- 230000002028 premature Effects 0.000 description 1
- 229910052895 riebeckite Inorganic materials 0.000 description 1
- XYSQXZCMOLNHOI-UHFFFAOYSA-N s-[2-[[4-(acetylsulfamoyl)phenyl]carbamoyl]phenyl] 5-pyridin-1-ium-1-ylpentanethioate;bromide Chemical compound [Br-].C1=CC(S(=O)(=O)NC(=O)C)=CC=C1NC(=O)C1=CC=CC=C1SC(=O)CCCC[N+]1=CC=CC=C1 XYSQXZCMOLNHOI-UHFFFAOYSA-N 0.000 description 1
Images
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B14/00—Projectiles or missiles characterised by arrangements for guiding or sealing them inside barrels, or for lubricating or cleaning barrels
- F42B14/02—Driving bands; Rotating bands
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T29/00—Metal working
- Y10T29/49—Method of mechanical manufacture
- Y10T29/49826—Assembling or joining
- Y10T29/49863—Assembling or joining with prestressing of part
- Y10T29/49865—Assembling or joining with prestressing of part by temperature differential [e.g., shrink fit]
Definitions
- the present invention relates mainly to improvements in gas-checks'or obturatingrings,'and has for its'object, chiefly, the prevention of erosion of thebore of the gun by protecting the gun from the scoring or eroding action of the products of combustion of the powder charge.
- the invention consists chiefly of an obtunear its base and between the driving-ring proper and the base of the projectile.
- the obturating-ring is made of some material sufficiently yielding or plastic to flow under great pressure, such as the pressure of the powder-gases exerted upon it, as hereinafter explained.
- At the rear of the obturating ring is another peripheral ring about the projectile and made gas-tight therewith.
- An interior space or groove is provided forward of the last-mentioned peripheral ring, hereinafter referred to as the ,fpressure-ring, whereby it is permitted, "under the pressure of the powder-gases, to move forwardaud to exert a greater pressure upon the obturatingring than the actual pressure of the powdergases and under which pressure the obturat- 1ng-ring is compressed and'caused to flow outward and to be forced into the lands of the gun with a pressure considerably in excess of the pressure of the powder-gases upon the bore of the gun, whereby a perfect seal is secured against all windage or flow of the powderrgases' past the projectile in its flight throughout the entire length of the gun.
- pressure-ring may be I order that the proper function of the same may not be impeded.
- the pressure ring may be affixed very tightlyto the base" of the shell orprojectile' and'still be caused to move freely forward under the great pressure of the powder-gases, and the pressure-ring may therefore be forced over and upon the base of the shell by hydraulic pressure or may be heated and shrunk upon the shell or projectile.
- the usual groove may be cut in the pressure-ring for handling the projectile, and the projectile may be handled by the pressure-ring without'danger of cansing the same to shift or move from its proper position.
- a band or layer of copper or'other suitable metal softer than steel or iron is preferably interposed between the pressure-ring and the body of the shell or projectile, and the pressure-ring is shrunk onto the same or forced thereupon with sufficient stress upon the copper to cause the same to flow under the ringv and to act as a perfect seal.
- the copper furthermore, acts as a lubricant,and by its useless pressure is required to overcome the friction between the pressure -ring and the shell, and a consequently greater pressure is expended upon the obturating-ring.
- Figure '1 is a half-elevation and half-longi tudinal section of the projectile withthe improved gas-check.
- Fig. 2 is one part of an enlarged sectional view of one formlof the gas check.
- Figs. 3, 4, 5, and 7 areisimilar enlarged sectional views of modified forms of the gas-check.
- Fig. 6 is part of a transverse section on the line 6 6 of Fig. 5, showing the obturating-ring in elevation.
- Fig. 8 is a simi-.
- the projectile 1 may be of any usual form, provided with a driving-ring 2 and an obturating-ring 3, rectangular in cross-section and placed in an annular recess in the projectile in contact on its rear side with the pressure-ring 4, securely held on the projectile-base, which is reduced in its diameter for the purpose.
- a portion of the pressure-ring lies across the inner side of the obturating-ring 3 and longitudinally extends partly into a recess 6 in the projectile.
- the ring 4 is also pressed with great force upon the obturating-ring, so as to prevent the entrance of the powder-gases between and to the space 6.
- the seat of the pressure-ring over the projectile-base is preferably slightly conical or tapering toward the rear, and the ring is of such diameter as to pass over the projectile-base with great difficulty and only with the employment of great pressure in order to secure its firm attachment, but not with so great difficulty as to prevent the further forward movement of the said ring under the pressure of the gases when the gun is fired.
- the seat is provided with a comparatively thin layer or sheet of copper 7, which, owing to its softer nature when the ring is forced into position, forms a very perfect joint between the ring and the shell and when the gun is fired prevents the gases of the fired charge from entering into the recess 6 and creating a pressure therein to resist the forward movement of the said ring.
- the rear of the ring 4 lies flush with the base of the projectile and is provided on its outer edge or periphery with a draw-hook groove 5.
- ring 4 is beveled on its rear inner edge in order to expose a portion of the side of the projectile-base, which is provided with a draw-hook groove 5.
- the draw-hook groove is constructed in the base of the projectile proper.
- the ring may be divided up into sections 9, having interposed between them laminre 8 of any suitable metal, such as copper.
- laminre 8 of any suitable metal, such as copper.
- the forward side of the pressure-ring and. the surface of the projectile opposite in contact with the obturating-ring are serrated or notched, 24, to prevent the ring 3 from being dislodged or moved from its position.
- the pressure-ring 4 does not extend within the obturating-ring, as in Figs. 2 and 3, but is held in position by its portion 13 projecting over the usual conical seat and copper sheet 7 into the space 6, which in this case is separated from the obturating-ring by a portion of the projectile that extends into a corresponding space or groove 12 in the pressure-ring.
- the pressure-ring is constructed integrally on the projectile-base and is united thereto by a thin portion or web 10, which allows the ring 4 to be sprung back and the split ring 11 to be placed in position beneath the space occupied by the obturatingring 3.
- the web is sprung forward or even disrupted or sheared longitudinally and the pressure-ring 4 caused to act upon the obturating-ring in the usual manner.
- Figs. 7 and 8 shows a split pressure-ring 4, similar in cross-section to that in Figs. 1 and 2, but placed in a groove immediately forward of the projectile-base.
- a layer or band 14 of softer metal than iron or steel, preferably copper is forced over the ring 4 into the space to be occupied by the obturating-ring between the rear of the pressure-ring and the base of the projectile and in the draw-hook groove 5, where it tightly fits or looks into a small dovetailed-shaped groove l5,which prevents any premature movement of the cop per band or pressure-ring and keeps the band from flying or fraying out when the projectile is fired.
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
Description
No. 707,135. Patented Aug. 19,1902.
H. MA DEVICE FOR THE- PREVENTION ROSION IN ORDNANGE.
Application flled Nov. 19, 1898.
' r35. E v E INVENTOR r 26M 774M? M ATTORNEY "cams PETERS Puc'rom'no wnsmnm'ou c I rating-ring about theprojectile, preferably UNITE STATES PATE T OFFICE.
- HUDSON MAXIM, OF YORK, N. Y. Y
DEVICE FOR THE PREVENTION OF EROSION IN ORDNANCE.
SPECIFICATION forming partof Letters Patent No. 707,135, dated August 1 19 1902. Q Application filed November 19.1898. Serial No. 696,927. (No model.)
To aZZ whom it may concern:
Be it known thatI, HUDSON MAXIM, a citizen of the United States, and a resident of the city and State of New York, have-invented new and useful Improvements in Devices for Prevention of Erosion in Ordnance, which are fully set forth in the following specification.
The present invention relates mainly to improvements in gas-checks'or obturatingrings,'and has for its'object, chiefly, the prevention of erosion of thebore of the gun by protecting the gun from the scoring or eroding action of the products of combustion of the powder charge. V
The invention consists chiefly of an obtunear its base and between the driving-ring proper and the base of the projectile. The obturating-ring is made of some material sufficiently yielding or plastic to flow under great pressure, such as the pressure of the powder-gases exerted upon it, as hereinafter explained. At the rear of the obturating ring is another peripheral ring about the projectile and made gas-tight therewith. An interior space or groove is provided forward of the last-mentioned peripheral ring, hereinafter referred to as the ,fpressure-ring, whereby it is permitted, "under the pressure of the powder-gases, to move forwardaud to exert a greater pressure upon the obturatingring than the actual pressure of the powdergases and under which pressure the obturat- 1ng-ring is compressed and'caused to flow outward and to be forced into the lands of the gun with a pressure considerably in excess of the pressure of the powder-gases upon the bore of the gun, whereby a perfect seal is secured against all windage or flow of the powderrgases' past the projectile in its flight throughout the entire length of the gun.
It is obvious that the pressure-ring may be I order that the proper function of the same may not be impeded.
' -It is obvious, furthermore, thatthe pressure ring may be affixed very tightlyto the base" of the shell orprojectile' and'still be caused to move freely forward under the great pressure of the powder-gases, and the pressure-ring may therefore be forced over and upon the base of the shell by hydraulic pressure or may be heated and shrunk upon the shell or projectile. The usual groove may be cut in the pressure-ring for handling the projectile, and the projectile may be handled by the pressure-ring without'danger of cansing the same to shift or move from its proper position.
In order to effectually secure a perfect joint or seal between the interior space forward of the pressure-ring and the powderchamber of the gun, a band or layer of copper or'other suitable metal softer than steel or iron is preferably interposed between the pressure-ring and the body of the shell or projectile, and the pressure-ring is shrunk onto the same or forced thereupon with sufficient stress upon the copper to cause the same to flow under the ringv and to act as a perfect seal. The copper, furthermore, acts as a lubricant,and by its useless pressure is required to overcome the friction between the pressure -ring and the shell, and a consequently greater pressure is expended upon the obturating-ring. i
With this general statement of the leading features of the invention I have, in order to make the same more clearly understood, shown in the accompanying drawings means for carrying it into practical effect without thereby limiting the improvements in their useful applications to the particular constructiontaken for illustration herein.
Figure '1 is a half-elevation and half-longi tudinal section of the projectile withthe improved gas-check. Fig. 2 is one part of an enlarged sectional view of one formlof the gas check. Figs. 3, 4, 5, and 7 areisimilar enlarged sectional views of modified forms of the gas-check. Fig. 6 is part of a transverse section on the line 6 6 of Fig. 5, showing the obturating-ring in elevation. Fig. 8 is a simi-.
lar view on the line 8 8 of Fig. 7.
Referring to the drawings in the preferred I oo form, Figs. 1 and 2, the projectile 1 may be of any usual form, provided with a driving-ring 2 and an obturating-ring 3, rectangular in cross-section and placed in an annular recess in the projectile in contact on its rear side with the pressure-ring 4, securely held on the projectile-base, which is reduced in its diameter for the purpose. A portion of the pressure-ring lies across the inner side of the obturating-ring 3 and longitudinally extends partly into a recess 6 in the projectile. The ring 4 is also pressed with great force upon the obturating-ring, so as to prevent the entrance of the powder-gases between and to the space 6. The seat of the pressure-ring over the projectile-base is preferably slightly conical or tapering toward the rear, and the ring is of such diameter as to pass over the projectile-base with great difficulty and only with the employment of great pressure in order to secure its firm attachment, but not with so great difficulty as to prevent the further forward movement of the said ring under the pressure of the gases when the gun is fired. The seat is provided with a comparatively thin layer or sheet of copper 7, which, owing to its softer nature when the ring is forced into position, forms a very perfect joint between the ring and the shell and when the gun is fired prevents the gases of the fired charge from entering into the recess 6 and creating a pressure therein to resist the forward movement of the said ring. The rear of the ring 4 lies flush with the base of the projectile and is provided on its outer edge or periphery with a draw-hook groove 5.
It will be seen from the foregoing that when the gun is fired the pressure upon the rear of the ring 4, being unbalanced by the space 6 and the resistance of the obturating-ring and the pressure on that portion of the obturating-ring exposed outside the projectile, forces the pressure-ring into the space 6 and into part of the space occupied by the obturatingring, causing the latter to be pressed out of its normal position into the space behind the driving-ring 2 and into the lands of the gun as the projectile moves through the bore.
In Fig. 3 the ring 4 is beveled on its rear inner edge in order to expose a portion of the side of the projectile-base, which is provided with a draw-hook groove 5. Although in Figs. 1 and 2 the pressure with which the ring 4 binds onto the rear of the projectile will prevent its being pulled away by any accident or ordinary force, yet for further surety in this respect the form shown in Fig. 3 may be used, in which the draw-hook groove is constructed in the base of the projectile proper. I have shown in the said figure an improved obturating-ring, preferably consisting of linen, cotton, or asbestos fabric or any other suitable fibrous material or a mixture of them interwoven with any suitable metallic wire or gauze, preferably of copper, and impregnated with oil, paraffin, plumbago,
or other suitable plastic and lubricating material. The ring may be divided up into sections 9, having interposed between them laminre 8 of any suitable metal, such as copper. The forward side of the pressure-ring and. the surface of the projectile opposite in contact with the obturating-ring are serrated or notched, 24, to prevent the ring 3 from being dislodged or moved from its position.
In Fig. 4 the pressure-ring 4 does not extend within the obturating-ring, as in Figs. 2 and 3, but is held in position by its portion 13 projecting over the usual conical seat and copper sheet 7 into the space 6, which in this case is separated from the obturating-ring by a portion of the projectile that extends into a corresponding space or groove 12 in the pressure-ring.
In Figs. 5 and 6 the pressure-ring is constructed integrally on the projectile-base and is united thereto by a thin portion or web 10, which allows the ring 4 to be sprung back and the split ring 11 to be placed in position beneath the space occupied by the obturatingring 3. When the gun is fired, the web is sprung forward or even disrupted or sheared longitudinally and the pressure-ring 4 caused to act upon the obturating-ring in the usual manner.
The modification in Figs. 7 and 8 shows a split pressure-ring 4, similar in cross-section to that in Figs. 1 and 2, but placed in a groove immediately forward of the projectile-base. In this case before the obturatingring is placed in position a layer or band 14, of softer metal than iron or steel, preferably copper, is forced over the ring 4 into the space to be occupied by the obturating-ring between the rear of the pressure-ring and the base of the projectile and in the draw-hook groove 5, where it tightly fits or looks into a small dovetailed-shaped groove l5,which prevents any premature movement of the cop per band or pressure-ring and keeps the band from flying or fraying out when the projectile is fired.
What is claimed is- 1. The combination of a projectile having a peripheral shoulder and a conical rearwardly-tapering rear portion, a pressure-ring surrounding and capable of longitudinal movement on said rear portion, and an obturating-ring of plastic material between the pressure-ring and said shoulder on the pro-.
jectile.
2. The combination of a projectile having a peripheral shoulder near its base and a conical rearwardly-tapering rear portion, apres sure-ring surrounding and capable of longitudinal movement on said rear portion, a gascheck ring or seal between said pressure-ringand rear portion and an obturating-ring of plastic material between the pressure-ring and said shoulder on the projectile.
3. The combination of a projectile having a peripheral shoulder and a draw-hook groove formed in an integral portion of the projectile, and also having a conical rearwardlytapering rear portion witha pressure-ring ing said reduced rear portion and cut away so as to expose said draw-hook groove and an obturating-ring between said pressure-ring andperipheral shoulder.
5. The combination with a projectile of an obturating-ring composed of fibrous material interwoven with metallic wire or gauze and impregnated with a plastic material.
' 6. The combination 'with'a projectile of an obturator composed of a plurality of rings of fibrous material interwoven with'metallic Wire or gauze and impregnated with a plastic material, said rings having laminae of soft metalinterposed between them;
In testimony'whereof I have signed this specifioation'in the presence of two subscribing witnesses.
HUDSON MAXIM. Witnesses:
PHILIP MAURO, O. A. LQMAsSIE.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US69692798A US707135A (en) | 1898-11-19 | 1898-11-19 | Device for the prevention of erosion in ordnance. |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US69692798A US707135A (en) | 1898-11-19 | 1898-11-19 | Device for the prevention of erosion in ordnance. |
Publications (1)
Publication Number | Publication Date |
---|---|
US707135A true US707135A (en) | 1902-08-19 |
Family
ID=2775664
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US69692798A Expired - Lifetime US707135A (en) | 1898-11-19 | 1898-11-19 | Device for the prevention of erosion in ordnance. |
Country Status (1)
Country | Link |
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US (1) | US707135A (en) |
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2928348A (en) * | 1955-01-07 | 1960-03-15 | William A Zisman | Projectile rotating band |
US2996012A (en) * | 1955-11-17 | 1961-08-15 | Rex B Butler | Rotating band and seat therefor |
US3677132A (en) * | 1969-08-05 | 1972-07-18 | Us Navy | Waterproof sound, flash and recoil suppressor for firearms |
US5682011A (en) * | 1995-09-05 | 1997-10-28 | Rheinmetall Industrie Aktiengesellschaft | Sealing ring arrangement for a spin-stabilized projectile |
US20230228545A1 (en) * | 2022-01-17 | 2023-07-20 | Seismic Ammunition, Inc. | Training cartridge |
-
1898
- 1898-11-19 US US69692798A patent/US707135A/en not_active Expired - Lifetime
Cited By (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2928348A (en) * | 1955-01-07 | 1960-03-15 | William A Zisman | Projectile rotating band |
US2996012A (en) * | 1955-11-17 | 1961-08-15 | Rex B Butler | Rotating band and seat therefor |
US3677132A (en) * | 1969-08-05 | 1972-07-18 | Us Navy | Waterproof sound, flash and recoil suppressor for firearms |
US5682011A (en) * | 1995-09-05 | 1997-10-28 | Rheinmetall Industrie Aktiengesellschaft | Sealing ring arrangement for a spin-stabilized projectile |
US20230228545A1 (en) * | 2022-01-17 | 2023-07-20 | Seismic Ammunition, Inc. | Training cartridge |
US11959734B2 (en) * | 2022-01-17 | 2024-04-16 | Seismic Ammunition, Inc. | Training cartridge |
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