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US4034675A Expired / Lapsed US ⏱️ 0.0 years remaining

Catalysts - containing ablative resonance suppressors

Assignee: United States Department of the Army
•
Filing: 1970-08-20
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Granted: 1977-07-12
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Expires: 1990-08-20
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Abstract

Abstract Burning rate promoter (e.g. n-butylferrocene, n-hexylcarborane) is incorporated into resonance rods that are used to eliminate combustion instability of solid propellant. As the solid propellant burning progresses the resonance rods undergo ablation, and as ablation takes place, subsurface quantities of the burning rate promoter are exposed and continuously released into the combustion zone to catalyze the combustion process. This invention also employs porous resonance rods which contain the burning rate promoter and a selected material for suppressing combustion instability as infiltrants.

Inventors

  • 👤 David C. Sayles

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-10-23 15:22
CPC Classifications
C; C06; C06B; C06B45/00; C06B23/00; C06B23/007

Claims Analysis

Total Claims: 10
Claim 1
Independent Claim 75 words
A resonance rod of the type used in a solid propellant rocket motor to control combustion instability, said resonance rod comprised of phenolformaldehyde resin; a filler selected from carbon black and asbestos; and a burning rate catalyst selected from n-butylferrocene and n-hexylcarborane for release into the combustion zone of said rocket motor, said catalyst being releasable continuously into the combustion zone of said rocket motor as the solid propellant burning progresses within said rocket motor.
Claim 2
Dependent Claim 75 words
A resonance rod of the type used in a solid propellant rocket motor to control combustion instability, said resonance rod comprised of phenolformaldehyde resin; a filler selected from carbon black and asbestos; and a burning rate catalyst selected from n-butylferrocene and n-hexylcarborane for release into the combustion zone of said rocket motor, said catalyst being releasable continuously into the combustion zone of said rocket motor as the solid propellant burning progresses within said rocket motor.
Claim 3
Dependent Claim 77 words
The resonance rod of claim 1 wherein said resin is present in said rod in the amount of from about 40 to about 60 percent by weight of said rod; said filler is present in said rod in the amount of from about 25 to about 55 percent by weight of said rod; and said catalyst is present in said rod in the amount of from about 5 to about 15 percent by weight of said rod.
Claim 4
Dependent Claim 73 words
The resonance rod of claim 2 wherein said resin is present in said rod in the amount of about 40 percent by weight of said rod; said filler is carbon black which is present in said rod in the amount of about 55 percent by weight of said rod; and said selected catalyst is n-butylferrocene which is present in said rod in the amount of about 5 percent by weight of said rod.
Claim 5
Dependent Claim 73 words
The resonance rod of claim 2 wherein said resin is present in said rod in the amount of about 50 percent by weight of said rod; said filler is carbon black which is present in said rod in the amount of about 40 percent by weight of said rod; and said selected catalyst is n-butylferrocene which is present in said rod in the amount of about 10 percent by weight of said rod.
Claim 6
Dependent Claim 73 words
The resonance rod of claim 2 wherein said resin is present in said rod in the amount of about 60 percent by weight of said rod; said filler is carbon black which is present in said rod in the amount of about 25 percent by weight of said rod; and said selected catalyst is n-butylferrocene which is present in said rod in the amount of about 15 percent by weight of said rod.
Claim 7
Dependent Claim 72 words
The resonance rod of claim 2 wherein said resin is present in said rod in the amount of about 40 percent by weight of said rod; said filler is carbon black which is present in said rod in the amount of about 55 percent weight of said rod; and said selected catalyst is n-hexylcarborane which is present in said rod in the amount of about 5 percent by weight of said rod.
Claim 8
Dependent Claim 73 words
The resonance rod of claim 2 wherein said resin is present in said rod in the amount of about 50 percent by weight of said rod; said filler is carbon black which is present in said rod in the amount of about 40 percent by weight of said rod; and said selected catalyst in n-hexylcarborane which is present in said rod in the amount of about 10 percent by weight of said rod.
Claim 9
Dependent Claim 73 words
The resonance rod of claim 2 wherein said resin is present in said rod in the amount of about 60 percent by weight of said rod; said filler is carbon black which is present in said rod in the amount of about 25 percent by weight of said rod; and said selected catalyst is n-hexylcarborane which is present in said rod in the amount of about 15 percent by weight of said rod.
Claim 10
Dependent Claim 30 words
The resonance rod of claim 1 wherein said rod is in the form of a porous rod infiltrated with additives; said additives comprising said burning rate catalyst and said filler.

References Cited (Backward Citations)

US3140663A Cited
US3109374A Cited
US3128706A Cited
US3447981A Cited
US3310946A Cited

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1980-07-11 1981-01-10 1981-07-12 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1984-07-11 1985-01-10 1985-07-12 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 1988-07-11 1989-01-10 1989-07-12 $7700.00 Window Closed / Lapsed

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