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US3670180A Expired / Lapsed US ⏱️ 0.0 years remaining

Intervalometer

Assignee: Concord Control Inc
•
Filing: 1969-11-19
•
Granted: 1972-06-13
•
Expires: 1989-11-19
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Abstract

Abstract A solid-state rocket firing intervalometer is disclosed which employs a plurality of SCRs (silicon controlled rectifiers) for controlling the launching of respective electrically fired rockets, the gate circuit of each SCR being responsive to an input voltage above a predetermined threshold for triggering the SCR thereby to fire the rocket. The charging of a capacitor provides a progressively rising control voltage and a voltage divider applies a different portion of the rising control voltage to each of the gate circuits. Accordingly, each rocket is fired when the respective portion of the control voltage reaches the gate circuit threshold of the respective SCR.

Inventors

  • 👤 Herbert P Grossimon
  • 👤 James O Mcdonough
  • 👤 James K Roberge

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-10-29 13:08
CPC Classifications
H; H03; H03K; H03K5/00; H03K5/15; H03K5/15013; H03K5/1506; H03K5/15073

Claims Analysis

Total Claims: 5
Claim 1
Independent Claim 166 words
Apparatus for launching a plurality of electrically fired rockets in a predetermined sequence, said apparatus comprising: a plurality of triggerable semiconductor current switching devices connected for selectively firing respective ones of said rockets, each device having a control terminal which is responsive to an input voltage above a predetermined threshold applied thereto for triggering the respective device to fire the respective rocket; a capacitor; means for charging said capacitor thereby to generate a progressively rising control voltage; and a resistive voltage divider for applying a different proportion of said control voltage to each of said control terminals; means for sensing the current drawn by said semiconductor switching devices in firing respective rockets and for generating a signal when each rocket is fired; and means responsive to said signal for discharging said capacitor and for providing a predetermined delay after said current ceases before permitting said capacitor to resume charging whereby the different rockets are launched in a sequence corresponding to the sequence of the different portions.
Claim 2
Dependent Claim 166 words
Apparatus for launching a plurality of electrically fired rockets in a predetermined sequence, said apparatus comprising: a plurality of triggerable semiconductor current switching devices connected for selectively firing respective ones of said rockets, each device having a control terminal which is responsive to an input voltage above a predetermined threshold applied thereto for triggering the respective device to fire the respective rocket; a capacitor; means for charging said capacitor thereby to generate a progressively rising control voltage; and a resistive voltage divider for applying a different proportion of said control voltage to each of said control terminals; means for sensing the current drawn by said semiconductor switching devices in firing respective rockets and for generating a signal when each rocket is fired; and means responsive to said signal for discharging said capacitor and for providing a predetermined delay after said current ceases before permitting said capacitor to resume charging whereby the different rockets are launched in a sequence corresponding to the sequence of the different portions.
Claim 3
Dependent Claim 33 words
Apparatus as set forth in claim 1 wherein said means for discharging said capacitor includes a transistor amplifying means which is biased into conduction in response to current drawn by said switching devices.
Claim 4
Dependent Claim 175 words
Apparatus for launching a plurality of electrically fired rockets in a predetermined sequence, said apparatus comprising: a plurality of triggerable semiconductor current switching devices connected for selectively firing respective ones of said rockets, each device having a control terminal which is responsive to an input voltage above a predetermined threshold applied thereto for triggering the respective device to fire the respective rocket; a capacitor; means for charging said capacitor thereby to generate a progresSively rising control voltage; and a resistive voltage divider for applying a different proportion of said control voltage to each of said control terminals; and means including transistor amplifying means biased into conduction in response to the current drawn by any one of said switching devices in firing the respective rocket for discharging said capacitor and including also a second capacitor which maintains conduction through said transistor amplifying means to provide a predetermined delay after said current ceases before permitting said capacitor to resume charging whereby the different rockets are launched in a sequence corresponding to the sequence of the different portions.
Claim 5
Dependent Claim 175 words
Apparatus for launching a plurality of electrically fired rockets in a predetermined sequence, said apparatus comprising: a plurality of triggerable semiconductor current switching devices connected for selectively firing respective ones of said rockets, each device having a control terminal which is responsive to an input voltage above a predetermined threshold applied thereto for triggering the respective device to fire the respective rocket; a capacitor; means for charging said capacitor thereby to generate a progresSively rising control voltage; and a resistive voltage divider for applying a different proportion of said control voltage to each of said control terminals; and means including transistor amplifying means biased into conduction in response to the current drawn by any one of said switching devices in firing the respective rocket for discharging said capacitor and including also a second capacitor which maintains conduction through said transistor amplifying means to provide a predetermined delay after said current ceases before permitting said capacitor to resume charging whereby the different rockets are launched in a sequence corresponding to the sequence of the different portions.

References Cited (Backward Citations)

GB809669A Cited
US3122058A Cited
US3100268A Cited
US3058013A Cited
US3435257A Cited
US3396628A Cited
US3453496A Cited
US3504189A Cited

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1975-06-13 1975-12-13 1976-06-13 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1979-06-13 1979-12-13 1980-06-13 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 1983-06-13 1983-12-13 1984-06-13 $7700.00 Window Closed / Lapsed

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