Patent US3973499A successfully refreshed from Google Patents.
US3973499A
Expired / Lapsed
US
⏱️ 0.0 years remaining
Safe rocket motor igniter using sequenced initiation to an explosive logic network
Assignee: United States Department of the Navy
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Filing: 1974-08-27
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Granted: 1976-08-10
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Expires: 1994-08-27
Abstract
Abstract An apparatus for providing ignition of rocket motors by using sequenced initiation to an explosive logic network that is fail safe in case of accidental initiation. The explosive logic network has a multiplicity of input detonators for ignition of the explosive logic in a predetermined time program which must be accomplished in a specific ignition sequence to achieve a single explosive output to ignite the rocket motor squib and fire the motor. A deviation from the predetermined timed sequence or ignition of one or more of the input detonators will dud the system causing a fail safe condition of the logic network that prevents rocket motor ignition.
Inventors
- 👤 Matthew E. Anderson
- 👤 Fredric L. Menz
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-11-04 15:45
CPC Classifications
F; F42; F42D; F42D1/00; F42D1/04; F42D1/042; Y; Y10; Y10S; Y10S102/00; Y10S102/701
Claims Analysis
Total Claims: 3
Claim 1
Independent Claim
225 words
A safing apparatus for use in fail safing a squib used to fire a rocket motor comprising: a support plate of inert material having first and second continuous uniform explosive trails formed thereon; first and second electrically actuated igniting means attached to said first and second explosive trails respectively; said first explosive trail branching at an angle of 30 degrees or less into a curved branch and a straight branch with said curved branch meeting said straight branch in a first right angled junction at their extremities to form a single first output explosive trail; said second explosive trail branching into a first and second time delay means with said first time delay means meeting at its extremity said first explosive trail straight branch to form a second right angled junction; said second time delay means having a substantially longer time delay than said first time delay means and meeting at its extremity said first output explosive trail to form a third right angled junction; transfer charge means attached to said first output explosive trail and to a squib for firing said squib upon the arrival of a detonation wave at said transfer charge; said safing apparatus operative to provide said detonation wave along said first output explosive trail only when said first and second ignition means are electrically actuated in a predetermined time sequence.
Claim 2
Dependent Claim
225 words
A safing apparatus for use in fail safing a squib used to fire a rocket motor comprising: a support plate of inert material having first and second continuous uniform explosive trails formed thereon; first and second electrically actuated igniting means attached to said first and second explosive trails respectively; said first explosive trail branching at an angle of 30 degrees or less into a curved branch and a straight branch with said curved branch meeting said straight branch in a first right angled junction at their extremities to form a single first output explosive trail; said second explosive trail branching into a first and second time delay means with said first time delay means meeting at its extremity said first explosive trail straight branch to form a second right angled junction; said second time delay means having a substantially longer time delay than said first time delay means and meeting at its extremity said first output explosive trail to form a third right angled junction; transfer charge means attached to said first output explosive trail and to a squib for firing said squib upon the arrival of a detonation wave at said transfer charge; said safing apparatus operative to provide said detonation wave along said first output explosive trail only when said first and second ignition means are electrically actuated in a predetermined time sequence.
Claim 3
Dependent Claim
187 words
The safing apparatus of claim 1, and further including a third continuous uniform explosive trail formed on said support plate, and a third electrically actuated igniting means attached to said third explosive trail, and said first output explosive trail branching into a curved branch and a straight branch with said curved branch meeting said straight branch in a fourth right angled junction to form a single second output explosive trail, and; said third explosive trail branching into a straight branch and a third time delay means with said third time delay means having substantially longer length than said straight branch and meeting at its extremity said first output explosive trail to form a fifth right angled junction and said third explosive trail straight branch meeting at its extremity said first output explosive trail straight branch to form a sixth right angled junction and said transfer change means attached to said second output explosive trail, and said safing apparatus operative to provide said detonation wave along said second output explosive trail only when said first, second and third igniting means are electrically actuated in a predetermined time sequence.
References Cited (Backward Citations)
USPTO Annuity & Maintenance Windows
| Annuity Stage | Window Opens | Payment Deadline | Surcharge Period Until | Estimated Fee | Status |
|---|---|---|---|---|---|
| 3.5 Years (Year 4) | 1979-08-10 | 1980-02-09 | 1980-08-10 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1983-08-10 | 1984-02-09 | 1984-08-10 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1987-08-10 | 1988-02-09 | 1988-08-10 | $7700.00 | Window Closed / Lapsed |