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US3561705A Expired / Lapsed US ⏱️ 0.0 years remaining

Self-inflating target deployment container

Assignee: Individual
•
Filing: 1969-02-24
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Granted: 1971-02-09
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Expires: 1989-02-24
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Abstract

Abstract A container for deploying a self-inflating target from an aircraft comprising an elongate tubular casing for the target, a nose cap and a weighted tail portion which also serves as an airscoop. Upon release from the aircraft the weighted tail portion orients the container vertically. A valve positioned in the airscoop controls the amount of air entering the target to prevent target ejection and inflation until the falling container and target have decelerated to a safe opening speed.

Inventors

  • 👤 Raymond S Daughenbaugh

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-11-01 07:13
CPC Classifications
F; F41; F41J; F41J9/00; F41J9/08; B; B64; B64D; B64D1/00; B64D1/02

Claims Analysis

Total Claims: 8
Claim 1
Independent Claim 123 words
An air-droppable device for housing a target made of thin flexible material which target is adapted to be inflated by ram air forced thereinto when dropped through the earth''s atmosphere comprising: a container of elongate overall shape formed of a plurality of breakaway parts having interfitting edges; a weighted airscoop positioned at the aft end of said container with an opening leading into the interior of said target; and means for orienting the major axis of the container along the path of the container trajectory with the weighted airscoop directed forwardly when the container is dropped from a moving body; so that said container breaks up during its fall to free said target in order that it may become fully inflated before impact.
Claim 2
Dependent Claim 123 words
An air-droppable device for housing a target made of thin flexible material which target is adapted to be inflated by ram air forced thereinto when dropped through the earth''s atmosphere comprising: a container of elongate overall shape formed of a plurality of breakaway parts having interfitting edges; a weighted airscoop positioned at the aft end of said container with an opening leading into the interior of said target; and means for orienting the major axis of the container along the path of the container trajectory with the weighted airscoop directed forwardly when the container is dropped from a moving body; so that said container breaks up during its fall to free said target in order that it may become fully inflated before impact.
Claim 3
Dependent Claim 31 words
The device of claim 1 wherein the container comprises a nose section, a central body section and a tail section, said sections being interfitted together and forced off during the disassembly.
Claim 4
Dependent Claim 14 words
The device of claim 1 wherein the airscoop is provided with airflow control means.
Claim 5
Dependent Claim 41 words
The device of claim 3 wherein the airflow control means automatically responds to ram air pressure so as to prevent air ingress during periods of high ram air pressure and to permit air ingress during periods of low ram air pressure.
Claim 6
Dependent Claim 22 words
The device of claim 4 wherein the airflow control means if adjustable to vary the point at which air ingress is permitted.
Claim 7
Independent Claim 123 words
The method of erecting a collapsible target at a remote site comprising the steps of: collapsing said target into a small bundle; encapsulating said bundle within a breakaway container, said container having a weighted airscoop positioned at the aft end thereof with an opening leading into the interior of said target; transporting said container to a position above said site; releasing said container on a trajectory path directed toward said site, whereupon the container will become oriented with the airscoop directed forwardly; decelerating said container to its normal terminal velocity at free fall; and decapsulated said collapsed target when such normal terminal velocity is reached, so that the collapsed target may fully expand to its normal shape before impact at the target site.
Claim 8
Independent Claim 123 words
The method of erecting a collapsible target at a remote site comprising the steps of: collapsing said target into a small bundle; encapsulating said bundle within a breakaway container, said container having a weighted airscoop positioned at the aft end thereof with an opening leading into the interior of said target; transporting said container to a position above said site; releasing said container on a trajectory path directed toward said site, whereupon the container will become oriented with the airscoop directed forwardly; decelerating said container to its normal terminal velocity at free fall; and decapsulated said collapsed target when such normal terminal velocity is reached, so that the collapsed target may fully expand to its normal shape before impact at the target site.

References Cited (Backward Citations)

US1777188A Cited
US2382442A Cited
US3234503A Cited
US3221656A Cited
US3328750A Cited
US3508724A Cited

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1974-02-08 1974-08-10 1975-02-09 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1978-02-08 1978-08-10 1979-02-09 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 1982-02-08 1982-08-10 1983-02-09 $7700.00 Window Closed / Lapsed

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