IP Library Granted Patent US 9,708,227
Granted Patent B2
US 9,708,227 · App. 14/195,033 · Granted Jul 18, 2017

Method for producing a fragment / reactive material assembly

Inventor: David A. Alven (Johnson City, TN)
Assignee: AEROJET ROCKETDYNE, INC.
C06B21/0041B22F3/1007B22F3/1283B22F5/00C06B43/00C06B45/00C06C15/00C22C1/045C22C33/0207F42B12/32F42B12/44F42B12/74B22F2998/10B22F2999/00
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Quick Facts
Patent No.
US 9,708,227
App. No.
14/195,033
Granted
Jul 18, 2017
Kind
B2
Abstract

A method for the manufacture of a composite fragmenting material having exothermic properties includes the steps of packing a mold with preformed metal fragments; filling interstitial spaces surrounding the metal fragments with a reactive metal powder to form a mixture; and then sintering the mixture at a temperature effective to both coat the metal fragments with the reactive metal powder and to bond the metal fragments together. In one embodiment the composite fragmenting material is formed into a nosecone for a warhead.

Claims (9)

1. A method for the manufacture of a composite fragmenting material having exothermic properties, comprising the steps of:

packing a mold with preformed metal fragments;

filling interstitial spaces surrounding said metal fragments with a reactive metal powder to form a mixture; and

sintering said mixture at a temperature effective to both coat said metal fragments with said reactive metal powder and to bond said metal fragments together, wherein the reactive metal powder is a material that is exothermic on fragmentation of a warhead.

2. The method of claim 1 wherein said reactive metal powder is selected to be pyrophoric in the presence of oxygen at temperatures reached during detonation of the warhead.

3. The method of claim 2 wherein said reactive metal powder is selected from the group consisting of zirconium, niobium, hafnium, aluminum, titanium, magnesium and alloys of those metals containing more than 50%, by weight, of those metals.

4. The method of claim 3 wherein said reactive metal is selected to be zirconium or a zirconium-base alloy.

5. The method of claim 4 wherein said mixture is sintered at a temperature of between 1200° C. and 1500° C.

6. The method of claim 5 wherein a vacuum of between 10 −3 torr and 10 −6 torr is applied to said mixture during the step of sintering.

Assignments (6)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Jun 16, 2025
From: AEROJET ROCKETDYNE, INC.
To: AEROJET ORDNANCE TENNESSEE, INC.
Reel/Frame 071426/0688 →
CERTIFICATE OF CONVERSION Recorded Jun 16, 2025
From: BWXT ORDNANCE TENNESSEE, LLC
To: BWXT ORDNANCE TENNESSEE, INC.
Reel/Frame 071656/0086 →
CERTIFICATE OF CONVERSION WITH NAME CHANGE Recorded Jun 16, 2025
From: AEROJET ORDNANCE TENNESSEE, INC.
To: BWXT ORDNANCE TENNESSEE, LLC
Reel/Frame 071693/0429 →
TERMINATION AND RELEASE OF SECURITY INTEREST IN PATENTS Recorded Jul 28, 2023
From: BANK OF AMERICA, N.A., AS ADMINISTRATIVE AGENT
To: AEROJET ROCKETDYNE, INC.
Reel/Frame 064424/0109 →
NOTICE OF GRANT OF SECURITY INTEREST IN PATENTS Recorded Jun 17, 2016
From: AEROJET ROCKETDYNE, INC., SUCCESSOR-IN-INTEREST TO RPW ACQUISITION LLC
To: BANK OF AMERICA, N.A., AS ADMINISTRATIVE AGENT
Reel/Frame 039197/0125 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded May 16, 2016
From: ALVEN, DAVID A
To: AEROJET ROCKETDYNE, INC.
Reel/Frame 038606/0553 →
Continuity (2)
Provisional Application 61788608 · Mar 15, 2013
Related Publication 20140360635A1 · Dec 11, 2014