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Publication numberUS3903800 A
Publication typeGrant
Publication dateSep 9, 1975
Filing dateMay 17, 1967
Priority dateMar 26, 1965
Publication numberUS 3903800 A, US 3903800A, US-A-3903800, US3903800 A, US3903800A
InventorsKilmer Earl E
Original AssigneeUs Navy
Export CitationBiBTeX, EndNote, RefMan
External Links: USPTO, USPTO Assignment, Espacenet
Method for preparing heat resistant mild detonating fuse
US 3903800 A
Abstract  available in
Images(5)
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Claims  available in
Description  (OCR text may contain errors)

Bite States atent [1 1 [111 3,9 3,866

Kilmer Sept. 9, 1975 1 METHOD FOR PREPARING HEAT 2,982,210 5/1961 Andrew et a1. 86/] x RESISTANT MILD DETONATING FUSE 2,993,236 7/1961 Brimley et a]. 86/1 X [75] Inventor: Earl E. Kilmer, College Park, Md.

[73] Assignee: The United States of America as Primary Examiner samuel Feinbel'g represented by the Secretary of the Assistant Examinerl-laro1d Tudor Navy, Washington, Attorney, Agent, or Firm-R. S. Sciascia; J. A. Cooke [22] Filed: May 17, 1967 [21] Appl. No.: 651,339

Related US. Application Data [62] Division of Ser. No. 443,107, March 26, 1965, A process of preparing a mild detonating fuse from [57] ABSTRACT ab n n such heat resistant explosives as DIPAM, l-lNS and NONA and includes filling a tubular sheath made of a Cl 102/27 51 86/22 metal which can be annealed at temperatures below (12 F423 10 568F with an explosive material, reducing the explo- Field of Search 70 sive filled tubular sheath to a lesser diameter and annealing the sheath. [56] References Cited UNITED STATES PATENTS 1,741,380 12/1929 Snelling et a1. 86/1 7 Claims, No Drawings METHOD FOR PPARING HEAT RESISTANT MILD DETONATING FUSE The invention described herein may be manufactured andused by or for the Government of the United States of America for governmental purposes without the payment of any royalties thereon or therefor.

This application is a division of my copending application Ser. No. 443,107 filed Mar. 26, 1965, now abandoned.

This invention relates to explosive detonating cord- More particularly the invention relates to novel detonating cord characterized by resistance to high temper.- atures and low pressures.

Detonating cord consists of an outer tube or sheath of tin, lead, or other suitable metal or alloy encasing a continuous inner core of high explosive such as PETN, RDX, HMX and the like. Detonating cord was originally prepared by filling lead tubing with a molten explosive, permitting the explosive to harden, and then drawing the tubing down to a diameter of about 0.200 inch. The old form of detonating cord could not be bent to conform to the shape of an object or to conduct the cord past impediments without disturbing the continuity of the explosive train. Breaks were produced in the rigid cast explosive material by the bending of the casings, and these breaks were likely to cause a failure of the detonation wave as it proceeded down the length of the column. It therefore became the practice in the art to use explosive materials in particulate form in filling the tubular casings to insure that the continuity of the explosive train would not be disturbed by bending of the casing. In fact, some of the common high explosives, such as HMX, have such high melting points that they cannot be cast and can be used only in a particulate form.

The explosives and sheath materials used in the prior art detonating cords have been satisfactory for ordinary purposes. However, detonating cord in the form of mild detonating fuse and flexible linear shaped charge devices are finding increasing use in many aeronautic and space applications. The separation of missile stages from one another is just one of these applications. Aerodynamic heating can produce skin temperatures in missiles sufficiently high to melt most conventional explosives and thus to render inoperative detonating cord incorporating these explosives. High temperature explosives such as DATB have melting points above the expected temperatures but these explosives will decompose or sublime and thus be lost at the high temperatures and low atmospheric pressures which accompany high altitude operation. For example, DATB exhibits a weight loss of 53.8% when subjected to a temperature of 410F and a pressure of 2.5 mm of Hg.

Accordingly it is an object of the invention to provide detonating cord characterized by resistance to temperatures above 500F and to very low pressures. More particularly, an object of the invention is to provide detonating cord incorporating novel combinations of high temperature and low pressure resistant explosives and sheath metals.

A further object of the invention is to provide a method of manufacturing this novel detonating cord.

Briefly stated, the invention comprises fabricating detonating cord with high temperature resistant sheath materials and core loadings of explosive compounds which retain their crystalline structure at all temperatures up to 558! and which can, in addition, resist low pressures. Suitable sheath materials are silver and aluminum. Suitable explosives are 3,3-Diamino- 2,2',4,4,6,6-hexanitrobiphenyl (DIPAM), 2,2,2,4,- 4,4,6,6',6"-Nonanitroterphenyl (NONA), and 2,2,- 4,4',6,6-I-Iexanitrostilbene (HNS). The method of making the detonating cord of the invention adds to the conventional drawing, rolling and swaging operations a novel annealing step in which the cord is annealed to eliminate the cold work of the drawing and swaging steps with the explosive load in place and without in any way affecting the performance capabilities of the cord.

Other objects, advantages and new features of the invention will become apparent from a reading of the following detailed description. including the specific illustrative examples.

EXPLOS-IVES DIPAM may be prepared by means of a synthesis utilizing dipicric acid (3,3-dihydroxy-2,2',4,4,6,6- hexanitrobiphenyl) as a starting material, as has been described in the application of Joseph C. Dacons et al., Ser. No. 334,667, filed Dec. 30, 1963. In general, the synthesis involves conversion of dipicric acid to its dipyridinium salt, the conversion of the salt to dipicryl chloride and finally the conversion of the dipicryl chloride to DIPAM. As summarized in Table I, DIPAM melts at about 568F and shows substantially no weight loss at a pressure of 1 millimeter of mercury at 410F. DIPAM crystals are yellow and finally divided, in particle sizes of 10 to 40 microns with some agglomerates of up to 100 microns. DIPAM does not flow well in very humid atmospheres, but can be handled and loaded into detonating cord by normal techniques when the loading room is held at a relative humidity of about As will be indicated by the test results given in the examples below, the crystal geometry and particle size of DIPAM are adequate to meet the requirements of flexible detonating cord.

NONA is a polynitropolyphenyl compound having satisfactory properties for the present application as summarized in Table I. NONA may be prepared by the reaction of picryl halides and a halotrinitrobenzene by the various processes set out in application Ser. No. 320,579, of Joseph C. Dacons filed Oct. 31, 1963. NONA crystals are bladed or lathlike in form in particle sizes of 10 to microns. Loading is best performed at a controlled relative humidity of about 40-45%.

The preparation of HNS has been described in the application of Kathryn G. Shipp, Ser. No. 365,572, filed May 5, 1964. The method as there described involves a simple one step reaction which comprises the addition of a solution of 2,4,6-trinitrotoluene to an TABLE I Physical Properties DIPAM' HNS NONA Melting Point (C) 298-299 316 440-450 (F) 568 601 824-842 Theoretical Maximum 1.79 1.74 1.78 Density Volatility at 410F Pressure (mm of Hg) 1.0 0.9 0.8 Weight Loss (7:) Nil Nil 0.5 Macroscopic Crystal Data Shape Equant Acicular Bladcd Size (microns) 10-40;. 500p. lU-50p.

SHEATH MATERIALS Ordinary lead sheathed detonating cord is made with an antimony-lead alloy containing about 6% antimony. This alloy is not suitable for the present application, however, since it melts at 518F, well below the anticipated temperatures. For temperatures up to 590F, a 2 percent antimony-lead alloy would be suitable, but for higher temperature operation, other sheath materials are required. Silver and aluminum have been investigated as possible high temperature sheath materials and have been found suitable. The materials can be easily worked and, as will be indicated in the examples below, produce results which are equal to or superior to those obtainable from prior detonating cord.

FABRICATION One of the primary advantages of using silver or aluminum as the sheating material is the ability of these materials to be annealed at temperatures well below their melting points. Thus, it is possible to load and fabricate the detonating cord in the standard manner, or with additional working, and then to anneal the cord with the explosive in place without affecting the explosive in any way.

Detonating cord is ordinarily constructed by first pouring a desired quantity of explosive into the tubular sheath and then reducing the diameter and thus compacting the explosive by means of a series of drawing operations. It is also known to increase the apparent density of the explosive by swaging the tube to a smaller diameter. All of these mechanical forming operations introduce cold work into the metal, reducing its ductility and flexibility. This cold work was no problem in the lead sheaths of the prior art.

Silver and aluminum, however, must be annealed at intermediate stages in the forming process and after being worked in order to maintain their flexibility. As stated above, this annealing can be accomplished at temperatures well below their melting points, and well below the melting points of DIPAM, HNS, and NONA.

Aluminum sheathing can be annealed at 500F, with an annealing period of about hours. Higher temperatures can be used if they can be tolerated by the particular explosive involved.

The annealing time and temperature for silver sheathing is dependent on the size of the tube and the amount of cold work. For thin walled tubes, a temperature of 350F held for one-half hour, followed by cooling in air, is satisfactory. For thick Walled tubes, 460F for at least one hour is required.

The annealing process has no effect on the detonation velocity or on the ability of the explosive to be detonated. No change in the performance of detonating cord in the form of flexible linear shaped charge was observed after the annealing operation.

To further describe this invention,'attention is now directed to specific examples of detonating cord according to the invention. The examples are illustrative only, the invention not being limited thereby.

EXAMPLE I Several lengths of detonating cord were fabricated with core loadings of DIPAM in the amounts of 5, 10 and 15 grains per foot in a 6 /2 percent antimony-lead alloy as the sheath material. The explosive was found to support detonation in the loading of 5 grains per foot, which represents a column diameter of approximately 0.030 inch. The detonation velocity was uniform in all the loadings at approximately 5,440 meters per second.

Each of the detonating cords of this example was able to propagate the detonation around a bend. The cornering tests were divided into two groups, spirals and sharp bends. In the spiral test the detonating cord was wrapped around aluminum rods of 1% inch and /8 inch diametes. The spiral arrangement did not affect the performance of the explosive. In the sharp bend test, a one foot length of detonating cord was bent into a shape containing seven or eight 90 bends. The detonating cord so bent was placed on an aluminum witness plate and detonated. The bends did not affect the performance of the DIPAM detonating cord.

A high altitude simulating chamber was used to determine the suitability of the DIPAM explosive for the high altitude application. Tests were conducted by detonating the samples on aluminum witness plates, at room temperature and atmopsheric pressure, as well as at temperatures above 500F and pressures of 0.13 millimeters of mercurcy. The results of the tests are summarized in Table II. Note that one sample initiated and functioned successfully at 567F which is very close to the melting point of DIPAM. No variation in the propagation properties was observed as a result of the variation in temperature or the variation in pressure in this test.

TABLE II Functioning of DIPAM Detonating Cord Functioning Temp Simulated fiF Pressure Altitude (F) (C) (mm of Hg) (feet) Result 24 760 250 528 275 760 250 Complete 552 289 760 250 Propa- 567 297 760 250 gation 530 277 0.13 205,000 (Several runs) EXAMPLE II cated and were detonated at the end of those times. The heating rate was about 32F per minute.

TABLE III High Temperature Performance of HNS Detonating Cord Soak Soak Time Temperature Loading (minutes) (C) (F) Results 1 1.4 grains/ft. 8 280 536 l 1.4 grains/ft. 13 312 594 Complete 1 1.4 grains/ft. 28 310 590 Detonation EXAMPLE lIl Linear shaped charge has been fabricated with DIPAM as the explosive and silver as the sheath material. A number of charges, differing in cross-sectional shape and dimensions were prepared and fired to determine detonation velocity and performance as measured by the penetration distance of the shaped charge into an aluminum alloy target. The effect of stand-off distance was investigated and it was found that an optimum stand-off distance lies between 0.035 inch and 0.125 inch. The best performance was obtained with a 17.1 grain per foot charge, which gave a penetration of 0.106 inch at 0.125 inch standoff. A 15.5 grain per foot sample gave a mean penetration of 0.072 inch and a maximum of 0.099 inch. This is approximately equal to the perfonnance of standard 15 grains per foot RDX in lead.

Detonation velocity for all the DIPAM in silver linear shaped charge devices was approximately 6900 meters per second.

EXAMPLE IV Linear shaped charges of HNS in silver showed performances approximately equal to those exhibited by DIPAM in silver. The best performance was exhibited by a sample having a core loading of 15.42 grains per foot which gave a 0.090 inch mean penetration at a stand-off of O. 125 inch.

EXAMPLE V Several samples of NONA-silver linear shaped charge were constructed and were found to give satisfactory results. Detonation velocities for NONA in silver are slightly higher than for the other explosives, being approximately 7150 meters per second. The best performance for this combination of materials was 0.089 inch mean penetration at a stand-off of 0.125 inch and a core leading of 14.93 grains per foot.

EXAMPLE VI Several samples of detonating cord were constructed with DIPAM, HNS and NONA as the explosive core materials in fine silver as the sheath material. These cords were constructed in various loadings and column diameters ranging from 0.174 inch in outside diameter to 0.0395 inch in outside diameter. The range of explosive loadings for these diameters was from 42 grains per foot to 1.9 grains per foot in each of the explosives. The average detonation velocity for DIPAM loaded MDF was approximately 6900 meters per second with no diameter effect being noted. The detonation velocity for HNS was 6700 meters per second with no diameter effect, and the detonation velocity of NONAwas 7000 meters per second, no obvious diameter effect being observed.

EXAMPLE VII A sample of detonating cord was made with an aluminum sheath and NONA as theexplosive, with a core loading of 10 grains per foot. This sample has been sub jected to the high temperature, low pressure test and has been found to function satisfactorily, that is with complete detonation, after being held at a temperature of 772F for a period of 30 minutes.

As to safety, each of the explosives under consideration is relatively insensitive to impact and may therefore be easily handled. The explosives are safe from inadvertent initiation by electrostatic discharges.

The detonating cord and the process of making it, including the annealing step, are subject to wide modification as will be apparent to those skilled in the art after considering the above detailed description. Accordingly within the scope of the appended claims, the invention may be practiced other than as herein specifically described.

What is claimed is:

l. A method of making detonating cord comprising the steps of filling a tubular sheath made of a metal which can be annealed at temperatures below 568F with an explosive material in particulate form selected from the group consisting of 3,3-diamino-2,2',4,4',6,6'- hexanitrobiphenyl; 2,2,2",4,4',4",6,6',6"- Nonanitroterphenyl; and 2,2,4,4',6,6'-l-lexanitrostilbene,

reducing said explosive filled tubular sheath to a lesser diameter to thus compact said explosive,

and annealing by application of heat said sheath at a temperature below 568F. 2. A method as recited in claim 1 wherein said metal is silver and said annealing step is carried out at temperatures in the range of 350F to 460F for periods of at least one-half hour.

3. A method as recited in claim 1 wherein said metal is aluminum and said annealing step is carried out at a temperature of 500F for a period of at least approximately 5 hours.

4. A method according to claim 1, wherein said filling step is carried out in a regulated atmosphere at a relative humidity of less than 45%.

5. A method of fabricating detonating cord comprismg filling a tubular sheath made of a metal selected from the group consisting of silver and aluminum with an explosive material in particulate form selected from the group consisting of 3,3'-diamino- 2,2,4,4',6,6'-hexanitrobiphenyl; 2,2',2",4,4,4,- 6,6',6"-Nonanitroterphenyl; and 2,2',4,4',6,6- Hexanitrostilbene, said filling step being carried out in an atmosphere in which the relative humidity is maintained below 45%,

compressing said sheath to a lesser diameter by a series of drawing and swaging steps to thus compact said explosive, and

sisting of aluminum and silver.

7. A flexible detonating cord made by the process of claim 1.

Patent Citations
Cited PatentFiling datePublication dateApplicantTitle
US1741380 *Sep 30, 1925Dec 31, 1929Trojan Powder CoManufacture of cordeau
US2982210 *Jun 25, 1958May 2, 1961Ensign Bickford CoConnecting cord
US2993236 *Aug 29, 1957Jul 25, 1961Ici LtdMethod of producing cord-like product
Referenced by
Citing PatentFiling datePublication dateApplicantTitle
US4080902 *Nov 4, 1976Mar 28, 1978Teledyne Mccormick SelphHigh speed igniter device
US4083305 *Apr 28, 1976Apr 11, 1978Teledyne Mccormick Selph, An Operating Division Of Teledyne Ind. Inc.Mild detonating cord confinement
US4178853 *Apr 11, 1978Dec 18, 1979Teledyne Mccormick Selph, An Operating Division Of Teledyne Industries, Inc.Mild detonating cord confinement
US4913053 *Apr 18, 1988Apr 3, 1990Western Atlas International, Inc.Method of increasing the detonation velocity of detonating fuse
US5223664 *Sep 11, 1990Jun 29, 1993The Secretary Of State For Defence In Her Britannic Majesty's Government Of The United Kingdom Of Great Britain And Northern IrelandFlexible detonating cord
US5333550 *Jul 6, 1993Aug 2, 1994Teledyne Mccormick SelphTin alloy sheath material for explosive-pyrotechnic linear products
US5501154 *Jun 14, 1994Mar 26, 1996Teledyne Industries, Inc.Substantially lead-free tin alloy sheath material for explosive-pyrotechnic linear products
US6546837 *Nov 2, 2001Apr 15, 2003Perkinelmer, Inc.Dual load charge manufacturing method and press therefore
EP0712822A1 *Sep 11, 1990May 22, 1996Secretary Of State For Defence In Her Britannic Majesty's Gov. Of The United Kingdom Of Great Britain And Northern IrelandFlexible detonating cord
EP0794163A1 *Mar 4, 1997Sep 10, 1997Schlumberger LimitedShaped charge containing triaminotrinitrobenzene
WO1991004235A2 *Sep 11, 1990Apr 4, 1991Secr Defence BritFlexible detonating cord
Classifications
U.S. Classification102/275.8, 86/22, 86/1.1
International ClassificationC06C5/00, C06B25/00, C06C5/04, F42B3/00
Cooperative ClassificationC06C5/04, C06B25/00, F42B3/00
European ClassificationF42B3/00, C06C5/04, C06B25/00