US3392669A - Erosion reducer - Google Patents
Erosion reducer Download PDFInfo
- Publication number
- US3392669A US3392669A US610698A US61069867A US3392669A US 3392669 A US3392669 A US 3392669A US 610698 A US610698 A US 610698A US 61069867 A US61069867 A US 61069867A US 3392669 A US3392669 A US 3392669A
- Authority
- US
- United States
- Prior art keywords
- propellant
- additives
- additive
- cartridge
- pts
- 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
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B5/00—Cartridge ammunition, e.g. separately-loaded propellant charges
- F42B5/02—Cartridges, i.e. cases with charge and missile
- F42B5/24—Cartridges, i.e. cases with charge and missile for cleaning; for cooling; for lubricating ; for wear reducing
-
- C—CHEMISTRY; METALLURGY
- C06—EXPLOSIVES; MATCHES
- C06B—EXPLOSIVES OR THERMIC COMPOSITIONS; MANUFACTURE THEREOF; USE OF SINGLE SUBSTANCES AS EXPLOSIVES
- C06B23/00—Compositions characterised by non-explosive or non-thermic constituents
- C06B23/04—Compositions characterised by non-explosive or non-thermic constituents for cooling the explosion gases including antifouling and flash suppressing agents
-
- C—CHEMISTRY; METALLURGY
- C06—EXPLOSIVES; MATCHES
- C06B—EXPLOSIVES OR THERMIC COMPOSITIONS; MANUFACTURE THEREOF; USE OF SINGLE SUBSTANCES AS EXPLOSIVES
- C06B45/00—Compositions or products which are defined by structure or arrangement of component of product
- C06B45/12—Compositions or products which are defined by structure or arrangement of component of product having contiguous layers or zones
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B5/00—Cartridge ammunition, e.g. separately-loaded propellant charges
- F42B5/02—Cartridges, i.e. cases with charge and missile
- F42B5/16—Cartridges, i.e. cases with charge and missile characterised by composition or physical dimensions or form of propellant charge, with or without projectile, or powder
-
- 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
- Y10S—TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10S102/00—Ammunition and explosives
- Y10S102/704—Coolants
Definitions
- FIGS. 3 and 4 are modified cartridges of FIG. 1.
- the textile 16 for a 105 mm. high explosive anti-tank shell was a piece of rayon woven from spun viscose rayon yarn containing a durable water repellant of melamine resin base and weighed between 2.80 and 3.20 ounces per square yard.
- the rayon was pl-aced on a smooth surface and my additives poured thereon and spread evenly by scraping with a blade and resulted in a sheet slightly under 1/16 inch in thickness. Determination of minimum sheet thickness can be readily computed for any calibre weapon from the formula aforementioned. In the case of impregnated polyurethane foams, the identical formula for calculating sheet thickness will be used.
- the oxides used were of a particle size of about 1 to 60 microns and the Wax had a melting point of ⁇ about 180 F., unless otherwise indicated.
- Example I 47 grams of kaolinite having a particle size ranging between 3 to 60 microns are stirred into 53 grams of melted paraffin wax having a melting point of 180 F. The resultant mixture was thoroughly mixed while maintaining the temperature at about 100 C. and then poured onto a piece of spun viscose rayon yarn of melamine resin base, the rayon yarn having been placed on a smooth surface. By means of a scraping blade, a uniform thickness of about 1/16 inch of additive wax was obtained. If desired, the melted additive wax mixture can readily be poured in molds of varying configurations.
- nitrocellulose screened through an S-mesh screen and then placed in a mixer, such as a sigma blade type, for example, was added 2.5 percent by weight of talc and the required quantity of potassium sulfate and the whole mass dry blended for tive minutes. Then the solvent containing diphenylamine was added while the mixer was still running. The mixing operation was carried out for one hour with cold water running through the mixer jacket. The propellant composition was then removed from the mixer and stored in a tight container until time for extrusion into desired web sizes. All screen sizes hereinabove and hereinafter referred to were U.S. Standard Sieve type.
- Example V Propellant formulation CR7814 aforedescribed containing various additives such as talc, feldspar, kaolin, kaolinite and related materials belonging to the silicates family in quantities varying from 1 to 5% of propellant formulation weight were processed in accordance with the following:
Landscapes
- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Organic Chemistry (AREA)
- Crystallography & Structural Chemistry (AREA)
- Compositions Of Macromolecular Compounds (AREA)
- Chemical Or Physical Treatment Of Fibers (AREA)
- Treatments For Attaching Organic Compounds To Fibrous Goods (AREA)
- Lubricants (AREA)
Priority Applications (7)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US610698A US3392669A (en) | 1966-01-24 | 1967-01-20 | Erosion reducer |
GB685/68A GB1215401A (en) | 1966-01-24 | 1968-01-04 | Projectile propellant device including an erosion reducing additive |
BE708978D BE708978A (fr) | 1966-01-24 | 1968-01-05 | |
CH18068A CH525463A (fr) | 1966-01-24 | 1968-01-08 | Munition pour arme à feu |
DE19681678211 DE1678211B1 (de) | 1966-01-24 | 1968-01-13 | Kartusche od.dgl.fuer Feuerwaffen |
NL686800762A NL146475B (nl) | 1966-01-24 | 1968-01-17 | Patroon of granaat met erosieverminderende toeslag. |
FR136747A FR93891E (fr) | 1966-01-24 | 1968-01-19 | Réducteur d'érosion. |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US52279666A | 1966-01-24 | 1966-01-24 | |
US610698A US3392669A (en) | 1966-01-24 | 1967-01-20 | Erosion reducer |
Publications (1)
Publication Number | Publication Date |
---|---|
US3392669A true US3392669A (en) | 1968-07-16 |
Family
ID=27060941
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US610698A Expired - Lifetime US3392669A (en) | 1966-01-24 | 1967-01-20 | Erosion reducer |
Country Status (7)
Country | Link |
---|---|
US (1) | US3392669A (fr) |
BE (1) | BE708978A (fr) |
CH (1) | CH525463A (fr) |
DE (1) | DE1678211B1 (fr) |
FR (1) | FR93891E (fr) |
GB (1) | GB1215401A (fr) |
NL (1) | NL146475B (fr) |
Cited By (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3491690A (en) * | 1968-01-10 | 1970-01-27 | Verran Lane Knight | Water boosted shotshell |
USH18H (en) | 1983-11-21 | 1986-02-04 | The United States Of America As Represented By The Secretary Of The Army | Reduction of erosion and muzzle flash of gun tubes |
US5151557A (en) * | 1991-07-01 | 1992-09-29 | The United States Of America As Represented By The Secretary Of The Army | Additive for propelling charge |
US5463956A (en) * | 1994-02-08 | 1995-11-07 | Ici Americas Inc. | Wear decoppering liner |
EP0805943A1 (fr) * | 1994-12-16 | 1997-11-12 | Primex Technologies, Inc. | Additif composite de decuivrage pour poudre |
US6444062B2 (en) * | 1999-02-23 | 2002-09-03 | General Dynamics Ordnance & Tactical Systems, Inc. | Perforated propellant and method of manufacturing same |
US6984275B1 (en) | 2003-02-12 | 2006-01-10 | The United States Of America As Represented By The Secretary Of The Navy | Reduced erosion additive for a propelling charge |
Families Citing this family (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2193491B (en) * | 1978-07-21 | 1988-09-14 | Imi Kynoch Limited Kynoch Work | Improvements in propellants |
UA35271C2 (uk) * | 1999-09-14 | 2001-07-16 | Сергій Миколайович Александров | Спосіб виготовлення зносостійкого ствола вогнепальної зброї |
Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3148620A (en) * | 1959-08-14 | 1964-09-15 | Wegematic Corp | Wear reduction additives |
US3204588A (en) * | 1961-08-11 | 1965-09-07 | Deere & Co | Herbicide dispenser |
US3209689A (en) * | 1956-11-14 | 1965-10-05 | Mclennan Donald Elmore | Reduction of gun barrel wear |
-
1967
- 1967-01-20 US US610698A patent/US3392669A/en not_active Expired - Lifetime
-
1968
- 1968-01-04 GB GB685/68A patent/GB1215401A/en not_active Expired
- 1968-01-05 BE BE708978D patent/BE708978A/xx unknown
- 1968-01-08 CH CH18068A patent/CH525463A/fr unknown
- 1968-01-13 DE DE19681678211 patent/DE1678211B1/de not_active Withdrawn
- 1968-01-17 NL NL686800762A patent/NL146475B/xx unknown
- 1968-01-19 FR FR136747A patent/FR93891E/fr not_active Expired
Patent Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3209689A (en) * | 1956-11-14 | 1965-10-05 | Mclennan Donald Elmore | Reduction of gun barrel wear |
US3148620A (en) * | 1959-08-14 | 1964-09-15 | Wegematic Corp | Wear reduction additives |
US3204588A (en) * | 1961-08-11 | 1965-09-07 | Deere & Co | Herbicide dispenser |
Cited By (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3491690A (en) * | 1968-01-10 | 1970-01-27 | Verran Lane Knight | Water boosted shotshell |
USH18H (en) | 1983-11-21 | 1986-02-04 | The United States Of America As Represented By The Secretary Of The Army | Reduction of erosion and muzzle flash of gun tubes |
US5151557A (en) * | 1991-07-01 | 1992-09-29 | The United States Of America As Represented By The Secretary Of The Army | Additive for propelling charge |
US5463956A (en) * | 1994-02-08 | 1995-11-07 | Ici Americas Inc. | Wear decoppering liner |
EP0805943A1 (fr) * | 1994-12-16 | 1997-11-12 | Primex Technologies, Inc. | Additif composite de decuivrage pour poudre |
EP0805943A4 (fr) * | 1994-12-16 | 1998-04-29 | Primex Tech Inc | Additif composite de decuivrage pour poudre |
US6444062B2 (en) * | 1999-02-23 | 2002-09-03 | General Dynamics Ordnance & Tactical Systems, Inc. | Perforated propellant and method of manufacturing same |
US6984275B1 (en) | 2003-02-12 | 2006-01-10 | The United States Of America As Represented By The Secretary Of The Navy | Reduced erosion additive for a propelling charge |
Also Published As
Publication number | Publication date |
---|---|
FR93891E (fr) | 1969-05-30 |
CH525463A (fr) | 1972-07-15 |
BE708978A (fr) | 1968-05-16 |
NL146475B (nl) | 1975-07-15 |
DE1678211B1 (de) | 1971-11-18 |
GB1215401A (en) | 1970-12-09 |
NL6800762A (fr) | 1968-07-22 |
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