U.S. patent number 3,744,744 [Application Number 05/231,335] was granted by the patent office on 1973-07-10 for paraballoon.
This patent grant is currently assigned to The United States of America as represented by the Secretary of the Army. Invention is credited to Bernie J. Cobb.
United States Patent |
3,744,744 |
Cobb |
July 10, 1973 |
PARABALLOON
Abstract
A paraballoon for use as a recovery aid in finding missile
carried instruts. The paraballoon will act as a radar reflective
parachute for controlled descent, but converts to a balloon upon
impact for aid in recovery. A canopy forms the upper portion of the
parachute and is adapted to form a chamber therein. Upon impact an
acceleration responsive actuator causes release of gas to inflate
the chamber and convert the canopy into a balloon for use as a
recovery aid.
Inventors: |
Cobb; Bernie J. (Huntsville,
AL) |
Assignee: |
The United States of America as
represented by the Secretary of the Army (Washington,
DC)
|
Family
ID: |
22868795 |
Appl.
No.: |
05/231,335 |
Filed: |
March 2, 1972 |
Current U.S.
Class: |
244/32;
116/210 |
Current CPC
Class: |
B64D
17/78 (20130101) |
Current International
Class: |
B64D
17/78 (20060101); B64D 17/00 (20060101); B64b
001/48 () |
Field of
Search: |
;244/2,29,30,31,32,142,145 ;325/115 ;340/61,262 ;116/124B |
References Cited
[Referenced By]
U.S. Patent Documents
Primary Examiner: Buchler; Milton
Assistant Examiner: Basinger; S. D.
Claims
I claim:
1. A paraballoon for use as a recovery aid in locating a missile
instrument container after impact comprising: a canopy forming the
upper portion of a parachute and adapted to form a chamber therein;
shroud lines having one end connected to said canopy; a swivel
connector secured to said container and having the other ends of
said shroud lines connected thereto; means to supply gas in said
chamber for inflation of said canopy and an acceleration responsive
actuator, responsive to impact of said container for opening said
gas supply to inflate said chamber.
2. A paraballoon as set forth in claim 1 wherein said chamber
comprises upper and lower sections of polyester plastic material
heat sealed around their inner and outer joining edges forming a
donut-shaped balloon upon inflation thereof.
3. A paraballoon as set forth in claim 2 wherein said canopy is
provided with lights, and a power source for illuminating the
lights.
4. A paraballoon as set forth in claim 3 wherein said canopy is
coated with a radar reflective colored fluorescent substance.
5. A paraballoon as set forth in claim 4 wherein said means for
supplying gas includes a self-contained gas bottle disposed in said
chamber and connected to said acceleration responsive actuator for
operation thereby.
6. A paraballoon as set forth in claim 4 wherein said means for
supplying gas is disposed in the instrument container; a conduit
connecting said gas supply to said chamber, said gas supply means
being actuated by said acceleration responsive actuator.
Description
BACKGROUND OF THE INVENTION
This invention relates to the field of recovery aids. Present
recovery aids include metalized parachutes for radar tracking,
flashing lights for night recovery; radio beacons; and scent for
dog tracking. However even with all of these aids incorporated in
one body, recovery has still proven to be less than desireable. For
example, the radar must discriminate between the actual body and
miscellaneous hardware as the missile re-enters the atmosphere; the
flashing lights could be covered by the parachute due to ground
winds; the radio beacon must have an antenna that stands
perpendicular to the ground after impact to be able to transmit for
any distance, and the dogs must get within 400 yards of the object
to pick-up the scent.
SUMMARY OF THE INVENTION
The present invention provides a less cumbersome recovery aid which
could supplement or replace the available recovery aids. It
consists of a paraballoon which acts as a radar reflective
parachute for controlled descent but converts into a balloon upon
impact of the instruments.
This invention may be better understood from the following detailed
description taken in conjunction with the accompanying drawing.
BRIEF DESCRIPTION OF THE DRAWING
FIG. 1 is a sectional view of the paraballoon in flight showing one
embodiment of balloon inflation means.
FIG. 2 is a sectional view of the paraballoon after impact showing
a second embodiment of balloon inflation means and the paraballoon
inflated.
DESCRIPTION OF THE PREFERRED EMBODIMENT
Reference numeral 10 identifies the canopy of a parachute and is
connected by shroud lines 12 to an instrument container 14 by a
swivel type connector 15. The canopy is adapted to form a chamber
16 consisting of upper and lower sections 18 and 20. These sections
are made of polyester plastic material heat sealed around their
inner edge 22 and outer edge 24. The sections are coated with a
radar reflective colored fluorescent substance 26 for radar
tracking and visual observation. Venting means 28 is provided for
controlling the descent of the paraballoon while it is acting as a
parachute. An acceleration responsive actuator 30 is carried in the
instrument container and is set into operation upon impact of the
container. In the embodiment shown in FIG. 1 a self-contained gas
bottle 32 is disposed in chamber 16 for inflating the chamber to
form a dough-nut shaped lighter-than-air balloon as shown in FIG.
2. The bottle is connected to a bottle opening squib 34 which is
connected by an electric line 36 to the accelerator actuator
30.
After release from a missile the paraballoon would descend as a
parachute shown in FIG. 1. When the instrument container 14 strikes
the ground the actuator 30 will transmit an electric signal through
line 36 to actuate squib 34 and thereby open gas bottle 32 for
inflating canopy chamber 16.
In the embodiment shown in FIG. 2, the gas supply 38 is carried in
the instrument container. When the instrument container strikes the
ground the actuator will operate a squib 40 through line 42 to open
gas supply 38 thereby allowing gas flow through conduit 44 for
inflating canopy chamber 16.
A plurality of illuminating lights 46 are sealed in the canopy and
connected by means 48 to a power source 50 in the instrument
container.
* * * * *