US3328750A - Entrapped air flotation device - Google Patents
Entrapped air flotation device Download PDFInfo
- Publication number
- US3328750A US3328750A US484135A US48413565A US3328750A US 3328750 A US3328750 A US 3328750A US 484135 A US484135 A US 484135A US 48413565 A US48413565 A US 48413565A US 3328750 A US3328750 A US 3328750A
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- bag
- compartment
- air
- end compartment
- diaphragm
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- 238000005188 flotation Methods 0.000 title claims description 17
- 238000004891 communication Methods 0.000 claims description 5
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 9
- 238000007667 floating Methods 0.000 description 6
- 239000000463 material Substances 0.000 description 3
- 238000000034 method Methods 0.000 description 2
- 230000003416 augmentation Effects 0.000 description 1
- 230000005540 biological transmission Effects 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 230000008878 coupling Effects 0.000 description 1
- 238000010168 coupling process Methods 0.000 description 1
- 238000005859 coupling reaction Methods 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 230000000284 resting effect Effects 0.000 description 1
Images
Classifications
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01Q—ANTENNAS, i.e. RADIO AERIALS
- H01Q1/00—Details of, or arrangements associated with, antennas
- H01Q1/08—Means for collapsing antennas or parts thereof
- H01Q1/081—Inflatable antennas
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D1/00—Dropping, ejecting, releasing, or receiving articles, liquids, or the like, in flight
- B64D1/02—Dropping, ejecting, or releasing articles
-
- G—PHYSICS
- G10—MUSICAL INSTRUMENTS; ACOUSTICS
- G10K—SOUND-PRODUCING DEVICES; METHODS OR DEVICES FOR PROTECTING AGAINST, OR FOR DAMPING, NOISE OR OTHER ACOUSTIC WAVES IN GENERAL; ACOUSTICS NOT OTHERWISE PROVIDED FOR
- G10K11/00—Methods or devices for transmitting, conducting or directing sound in general; Methods or devices for protecting against, or for damping, noise or other acoustic waves in general
- G10K11/004—Mounting transducers, e.g. provided with mechanical moving or orienting device
- G10K11/006—Transducer mounting in underwater equipment, e.g. sonobuoys
Definitions
- ABSTRACT OF THE DISCLOSURE An entrapped air inflated antenna erection and flotation device for a sonobuoy deployed in the sea. A pair of contiguous diaphragms are positioned intermediate the ends of the inflated device to maintain the maximum entrapped air pressure reached during water entry in the antenna erecting portion.
- the present invention relates to flotation devices and more particularly to an entrapped air flotation device for air-dropped stores.
- ASW antisubmarine warfare
- stores of various kinds are dropped extensively from aircraft into the sea, and then floated for subsequent operation.
- Such a store could be a sonobuoy as disclosed in U.S. Patent 3,093,808, issued June 11, 1963 to Tatnall et al., for an Air-dropped Miniature Sonobuoy.
- the store is usually retarded by a speed brake or parachute and is buoyed by a gas cartridge-inflated bag.
- a more simplified technique has been attempted wherein the retardation and inflation both utilize properties of the environment.
- the flotation bag is modified to be inflated by ram air pressure during descent while concomitantly producing retardation.
- This technique is disclosed in U.S. Patent 3,161,896 to Holt et al., issued Dec. 22, 1964.
- insutficient entrapped air pressure is maintained after the store and flotation bag reach their normal floating positions in the water. Incomplete antenna erection occurs resulting in poor radio reception and transmission. Complete antenna erection is essential especially in high seastate conditions.
- Another object of the invention is to provide an entrapped air flotation device which is capable of positively erecting an antenna therewithin for operation of radio apparatus associated therewith under various sea-state conditions.
- Still another object of the invention is to provide an entrapped air flotation device which is relatively simple in construction and inexpensive to manufacture, which is compact and easy to package, and which is rugged and reliable in the most severe of operating environments.
- the invention to be described hereinbelow contemplates an inflatable bag connected by shroud lines at its open end to an air-to-sea launchable store such as a transducer and radio combination. After being launched from an aircraft, the bag pays out and scoops in air causing it to inflate and retard the store. An auxiliary parachute about the periphery of the bag assists in these functions, but may be omitted as conditions dictate.
- the bag is internally divided along its length into an upper compartment and lower compartment which communicate through a one-way valve that permits air to flow in one direction only from lower to the upper compartment.
- the upper compartment becomes fully inflated and retains this pressure level irrespective of any subsequent reduction of pressure in the lower compartment as the store and bag assume their normal floating positions relative to each other in the water.
- the amount of entrapped air in the upper compartment is suflicient to maintain full inflation of the upper portion of the bag, and complete erection of any antenna supported therewithin.
- FIG. 1 is a pictorial representation in elevation of one embodiment of the invention as applied to an air-to-sea launched sonobuoy resting in water at its normal floating position;
- FIG. 2 represents a longitudinal cross section of the upper portion of the inventive embodiment shown in FIG. 1;
- FIG. 3 represents a transverse cross section of the inventive embodiment taken along the line 33 of FIG.
- FIG. 1 shows a sonobuoy floating in water in its normal operating position wherein a transducer or hydrophone 10' depends by a cable 11 from a housing 12.
- the housing 12 contains radio equipment for electronically coupling the hydrophone 10 to an antenna 13.
- the antenna 13 is erected by means of an entrapped air flotation bag 15 which is attached to the housing 12 by a plurality of shroud lines 6.
- the inflation bag 15 comprises a generally elongated cylindrical configuration of air-impermeable, flexible material closed at the socalled upper or free end and open at the so-called lower or shroud-connected end.
- the diameter of the bag 15 varies along its length: beginning at its open end, the bag tapers inward slightly, then tapers outward to a diameter greater than at the open end, and finally tapers inward again at any convenient angle or angles until it reaches the closed end.
- the precise taper profile of the bag for achieving optimum retardation and air entrapment is a matter of design and is not critical except to the extent that the bag functions in the manner contemplated by the invention as described and claimed herein.
- a check valve comprised of two adjacent circular diaphragms 18 and 19 each sealingly secured at their circumference to the inner surface of the bag 15 forming thereby two compartments: a lower compartment between the bag opening and the diaphragm 18, and an upper compartment between the closed end of the bag and the diaphragm 19.
- the diaphragm 19 includes a plurality of through 'holes 21 arranged in a circular array about its center, and the diaphragm 18 includes a single through hole 22 at its center.
- the diaphragm 19 is constructed in a manner and material so that it can deflect away from the diaphragm 18 into the dotted outline position whenever the pressure in the lower compartment is greater than in the upper compartment. Under this pressure differential condition, communication is established to permit air to flow upward through the openings 22 and 21, respectively. No air is permitted to flow from the upper compartment to the lower compartment whenever the pressure in the upper compartment exceeds the pressure in the lower compartment by virtue of the contiguous relationship established by the diaphragms 18 and 19.
- the antenna 13 is also flexible and passes from the lower to the upper compartment through a seal 23. It is secured by any convenient means to the closed end of the bag 15. Of course the antenna length in the upper compartment must be sutficient to permit the diaphragm 19 to move to its contiguous position while the upper compartment remains fully inflated.
- an annular parachute 26 be placed about the bag 15 near the point of maximum diameter, such as by a plurality of straps 27 each secured at its ends to the bag in any convenient manner.
- the parachute'26 will assist inflation by tending to pull the bag 15 radially outward near the point of maximum diameter. concomitantly, the parachute 26 will augment the retardation produced by the open end. of the bag in the same Way as an ordinary parachute.
- the time of maximum entrapped air pressure in the bag 15 occurs during entry into the water.
- the level of the water within the bag is, at this instant, illustrated by the dotted line A in FIG. 2.
- the water level within the bag drops to the level shown at line B. Since there is an increase in volume in the lower compartment, the pressure drops but the diaphragms 18 and 19 prevent the high pressure entrapped air in the upper compartment from escaping, thereby sustaining complete inflation of the upper portion of the bag 15 and full erection of the antenna 13.
- An entrapped air flotation device for air-to-sea launched stores comprising:
- an elongated inflatable bag open at one end for admitting air therein, said bag generally tapering toward the ends from an annular surface of the bag lying in the plane normal to and intermediate of the ends;
- each diaphragm having a hole oflset from the other for establishing communication between the compartments when said diaphragms are noncontiguous, and the diaphragm nearest said closed compartment being constructed to deflect away from the other diaphragm whenever the pressure in the open end compartment is greater than in the closed end compartment;
- An entrapped air flotation device as set forth in claim 1 further comprising shroud lines secured at the open end of said bag and adapted to be connected to the store.
- An entrapped air flotation device as set forth in claim 2 further comprising:
- a flexible antenna secured at one end to the closed end of said bag and adapted to be connected at the other end to the store.
- An entrapped air flotation device as set forth in claim 3 further comprising:
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- Acoustics & Sound (AREA)
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Description
June 27, 1967 G. A. GIMBER ETAL ENTRAFPED AIR FLOTATION DEVICE Filed Aug. 31 1965 INVENTORS GEORGE A. GIMBER ROY L. SHIPMAN H H :5. w l 6 if m m b i m imiff" w t w j/ m m R v ATTORNEY United States Patent 3,328,750 ENTRAPPED AIR FLOTATION DEVICE George A. Gimber, Hatboro, and Roy L. Shipman, Willow Grove, Pa., assignors to the United States of America as represented by the Secretary of the Navy Filed Aug. 31, 1965, Ser. No. 484,135 4 Claims. (Cl. 340-2) ABSTRACT OF THE DISCLOSURE An entrapped air inflated antenna erection and flotation device for a sonobuoy deployed in the sea. A pair of contiguous diaphragms are positioned intermediate the ends of the inflated device to maintain the maximum entrapped air pressure reached during water entry in the antenna erecting portion.
The invention described herein may be manufactured and used by or for the Government of the United States of America for governmental purposes without the payment of any royalties thereon or therefor.
The present invention relates to flotation devices and more particularly to an entrapped air flotation device for air-dropped stores.
In airborne ASW (antisubmarine warfare), stores of various kinds are dropped extensively from aircraft into the sea, and then floated for subsequent operation. Such a store could be a sonobuoy as disclosed in U.S. Patent 3,093,808, issued June 11, 1963 to Tatnall et al., for an Air-dropped Miniature Sonobuoy. During its descent in the air, the store is usually retarded by a speed brake or parachute and is buoyed by a gas cartridge-inflated bag. For some applications where smooth deceleration and placement accuracy are not critical, a more simplified technique has been attempted wherein the retardation and inflation both utilize properties of the environment. That is, the flotation bag is modified to be inflated by ram air pressure during descent while concomitantly producing retardation. This technique is disclosed in U.S. Patent 3,161,896 to Holt et al., issued Dec. 22, 1964. However, where the bag is of an elongated configuration, as may be required for erecting an antenna therewithin, insutficient entrapped air pressure is maintained after the store and flotation bag reach their normal floating positions in the water. Incomplete antenna erection occurs resulting in poor radio reception and transmission. Complete antenna erection is essential especially in high seastate conditions.
Accordingly, it is an object of the present invention to provide an entrapped air flotation device from air-tosea launched stores in which retardation is provided during air descent, and in which a relatively high inflation pressure is maintained after reaching its normal floating position.
Another object of the invention is to provide an entrapped air flotation device which is capable of positively erecting an antenna therewithin for operation of radio apparatus associated therewith under various sea-state conditions.
Still another object of the invention is to provide an entrapped air flotation device which is relatively simple in construction and inexpensive to manufacture, which is compact and easy to package, and which is rugged and reliable in the most severe of operating environments.
Various other objects and advantages will appear from the following description of one embodiment of the invention, and the most novel features will be particularly pointed out hereinafter in connection with the appended claims.
Briefly, the invention to be described hereinbelow contemplates an inflatable bag connected by shroud lines at its open end to an air-to-sea launchable store such as a transducer and radio combination. After being launched from an aircraft, the bag pays out and scoops in air causing it to inflate and retard the store. An auxiliary parachute about the periphery of the bag assists in these functions, but may be omitted as conditions dictate. The bag is internally divided along its length into an upper compartment and lower compartment which communicate through a one-way valve that permits air to flow in one direction only from lower to the upper compartment. During water entry, where maximum entrapped air pressure occurs, the upper compartment becomes fully inflated and retains this pressure level irrespective of any subsequent reduction of pressure in the lower compartment as the store and bag assume their normal floating positions relative to each other in the water. The amount of entrapped air in the upper compartment is suflicient to maintain full inflation of the upper portion of the bag, and complete erection of any antenna supported therewithin.
In the drawings:
FIG. 1 is a pictorial representation in elevation of one embodiment of the invention as applied to an air-to-sea launched sonobuoy resting in water at its normal floating position;
FIG. 2 represents a longitudinal cross section of the upper portion of the inventive embodiment shown in FIG. 1; and
FIG. 3 represents a transverse cross section of the inventive embodiment taken along the line 33 of FIG.
In the illustrated embodiment of the invention, FIG. 1 shows a sonobuoy floating in water in its normal operating position wherein a transducer or hydrophone 10' depends by a cable 11 from a housing 12. The housing 12 contains radio equipment for electronically coupling the hydrophone 10 to an antenna 13. As is explained hereinbelow, the antenna 13 is erected by means of an entrapped air flotation bag 15 which is attached to the housing 12 by a plurality of shroud lines 6.
Referring now to FIGS. 2 and 3 the inflation bag 15 comprises a generally elongated cylindrical configuration of air-impermeable, flexible material closed at the socalled upper or free end and open at the so-called lower or shroud-connected end. The diameter of the bag 15 varies along its length: beginning at its open end, the bag tapers inward slightly, then tapers outward to a diameter greater than at the open end, and finally tapers inward again at any convenient angle or angles until it reaches the closed end. The precise taper profile of the bag for achieving optimum retardation and air entrapment is a matter of design and is not critical except to the extent that the bag functions in the manner contemplated by the invention as described and claimed herein.
At the point of maximum diameter along the length of the bag 15, there is a check valve comprised of two adjacent circular diaphragms 18 and 19 each sealingly secured at their circumference to the inner surface of the bag 15 forming thereby two compartments: a lower compartment between the bag opening and the diaphragm 18, and an upper compartment between the closed end of the bag and the diaphragm 19. The diaphragm 19 includes a plurality of through 'holes 21 arranged in a circular array about its center, and the diaphragm 18 includes a single through hole 22 at its center. Thus, when the two diaphragms are contiguous to each other, there is no communication between the upper and lower compartments of the bag due to the offset between holes 21 and 22. However, when the diaphragms are non-contiguous, such as shown by the dotted outline of diaphragm 19 in FIG.
2, communication is established. The diaphragm 19 is constructed in a manner and material so that it can deflect away from the diaphragm 18 into the dotted outline position whenever the pressure in the lower compartment is greater than in the upper compartment. Under this pressure differential condition, communication is established to permit air to flow upward through the openings 22 and 21, respectively. No air is permitted to flow from the upper compartment to the lower compartment whenever the pressure in the upper compartment exceeds the pressure in the lower compartment by virtue of the contiguous relationship established by the diaphragms 18 and 19. The antenna 13 is also flexible and passes from the lower to the upper compartment through a seal 23. It is secured by any convenient means to the closed end of the bag 15. Of course the antenna length in the upper compartment must be sutficient to permit the diaphragm 19 to move to its contiguous position while the upper compartment remains fully inflated.
Depending upon conditions, it may be necessary to provide auxiliary retardation and inflation augmentation of the bag. It is, therefore, contemplated that an annular parachute 26 be placed about the bag 15 near the point of maximum diameter, such as by a plurality of straps 27 each secured at its ends to the bag in any convenient manner. When the bag 15 is initially deployed during descent, the parachute'26 will assist inflation by tending to pull the bag 15 radially outward near the point of maximum diameter. concomitantly, the parachute 26 will augment the retardation produced by the open end. of the bag in the same Way as an ordinary parachute.
To appreciate the inventions operation it should be understood that the time of maximum entrapped air pressure in the bag 15 occurs during entry into the water. The level of the water within the bag is, at this instant, illustrated by the dotted line A in FIG. 2. As the bag comes to rest in its normal floating position, the water level within the bag drops to the level shown at line B. Since there is an increase in volume in the lower compartment, the pressure drops but the diaphragms 18 and 19 prevent the high pressure entrapped air in the upper compartment from escaping, thereby sustaining complete inflation of the upper portion of the bag 15 and full erection of the antenna 13.
It will be understood that various changes in the details, materials, steps and arrangement of parts, which have been herein described and illustrated in order to explain the nature of the invention, may be made by those skilled in the art within the principle and scope of the invention as expressed in the appended claims.
What is claimed is:
1. An entrapped air flotation device for air-to-sea launched stores, comprising:
an elongated inflatable bag open at one end for admitting air therein, said bag generally tapering toward the ends from an annular surface of the bag lying in the plane normal to and intermediate of the ends;
a pair of normally contiguous circular diaphragms sealingly secured at their circumferences to said bag in said plane forming thereby an open end compartment and a closed end compartment for permitting air flow only from said open end compartment to said closed end compartment, each diaphragm having a hole oflset from the other for establishing communication between the compartments when said diaphragms are noncontiguous, and the diaphragm nearest said closed compartment being constructed to deflect away from the other diaphragm whenever the pressure in the open end compartment is greater than in the closed end compartment;
whereby the maximum air pressure attained in said closed end compartment is maintained irrespective of any reduction in the maximum pressure in the open end compartment.
2. An entrapped air flotation device as set forth in claim 1 further comprising shroud lines secured at the open end of said bag and adapted to be connected to the store.
3. An entrapped air flotation device as set forth in claim 2 further comprising:
a flexible antenna secured at one end to the closed end of said bag and adapted to be connected at the other end to the store.
4. An entrapped air flotation device as set forth in claim 3 further comprising:
an annular parachute secured about the periphery of said bag at said plane.
References Cited UNITED STATES PATENTS 2,384,721 9/1946 Bingham 244-142 3,061,249 10/1962 Chipperfield 244-138 3,154,268 10/1964 Strubble 24432 3,161,896 12/1964 Holt et al. 9-8 3,234,503 2/1966 Wojciechowski et a1. 3402 RODNEY D. BENNETT, Primary Examiner.
RICHARD A. FARLEY, Examin r.
Claims (1)
1. AN ENTRAPPED AIR FLOTATION DEVICE FOR AIR-TO-SEA LAUNCHED STORES, COMPRISING: AN ELONGATED INFLATABLE BAG OPEN AT ONE END FOR ADMITTING AIR THEREIN, SAID BAG GENERALLY TAPERING TOWARD THE ENDS FROM AN ANNULAR SURFACE OF THE BAG LYING IN THE PLANE NORMAL TO AND INTERMEDIATE OF THE ENDS; A PAIR OF NORMALLY CONTIGUOUS CIRCULAR DIAPHRAGMS SEALINGLY SECURED AT THEIR CIRCUMFERENCES TO SAID BAG IN SAID PLANE FORMING THEREBY AN OPEN END COMPARTMENT AND A CLOSED END COMPARTMENT FOR PERMITTING AIR FLOW ONLY FROM SAID OPEN END COMPARTMENT TO SAID CLOSED END COMPARTMENT, EACH DIAPHRAGM HAVING A HOLE OFFSET FROM THE OTHER FOR ESTABLISHING COMMUNICATION BETWEEN THE COMPARTMENTS WHEN SAID DIAPHRAGMS ARE NONCONTIGUOUS, AND THE DIAPHRAGM NEAREST SAID CLOSED COMPARTMENT BEING CONSTRUCTED TO DEFLECT AWAY FROM THE OTHER DIAPHRAGM WHENEVER THE PRESSURE IN THE OPEN END COMPARTMENT IS GREATER THAN IN THE CLOSED END COMPARTMENT; WHEREBY THE MAXIMUM AIR PRESSURE ATTAINED IN SAID CLOSED END COMPARTMENT IS MAINTAINED IRRESPECTIVE OF ANY REDUCTION IN THE MAXIMUM PRESSURE IN THE OPEN END COMPARTMENT.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
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US484135A US3328750A (en) | 1965-08-31 | 1965-08-31 | Entrapped air flotation device |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US484135A US3328750A (en) | 1965-08-31 | 1965-08-31 | Entrapped air flotation device |
Publications (1)
Publication Number | Publication Date |
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US3328750A true US3328750A (en) | 1967-06-27 |
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Application Number | Title | Priority Date | Filing Date |
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US484135A Expired - Lifetime US3328750A (en) | 1965-08-31 | 1965-08-31 | Entrapped air flotation device |
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Cited By (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3377615A (en) * | 1966-04-25 | 1968-04-09 | Sparton Corp | Compliant suspension system |
US3514058A (en) * | 1968-05-03 | 1970-05-26 | Us Navy | Self-inflating retardation and floatation device |
US3561705A (en) * | 1969-02-24 | 1971-02-09 | Raymond S Daughenbaugh | Self-inflating target deployment container |
US3755836A (en) * | 1970-09-28 | 1973-09-04 | Itt | Stabilization arrangement for communication buoys |
US3889224A (en) * | 1974-03-08 | 1975-06-10 | Us Navy | Crown float/decelerator |
FR2438587A1 (en) * | 1974-11-28 | 1980-05-09 | France Etat | LOADING AND FLOATING DEVICE FOR A SUSPENDED LOAD |
US4298963A (en) * | 1974-11-28 | 1981-11-03 | Etat Francais Represente Par Le Delegue Ministeriel Pour L'armement | Jettisoning and flotation device for a suspended load, particularly an underwater listening body |
US4407607A (en) * | 1982-02-05 | 1983-10-04 | Mccambridge Joseph | Fluid dynamic erosion control unit |
US5406294A (en) * | 1993-05-13 | 1995-04-11 | Spears Associates, Inc. | Floating antenna system |
US20040185727A1 (en) * | 2003-03-17 | 2004-09-23 | Japan Aircraft Manufacturing Co., Ltd. | Airdrop type buoy apparatus |
US20050093754A1 (en) * | 2003-10-30 | 2005-05-05 | Lyons Alan M. | Light-weight signal transmission lines and radio frequency antenna system |
Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2384721A (en) * | 1943-10-02 | 1945-09-11 | Cambridge Rubber Co | Life preserving apparatus |
US3061249A (en) * | 1959-05-22 | 1962-10-30 | Ultra Electronics Ltd | Floating means |
US3154268A (en) * | 1962-09-19 | 1964-10-27 | Jr Arthur D Struble | Balloon and parachute combination |
US3161896A (en) * | 1963-11-20 | 1964-12-22 | Ira T Holt | Ram air inflated flotation bag |
US3234503A (en) * | 1963-03-27 | 1966-02-08 | Hoffman Electronics Corp | Drag chute and flotation device |
-
1965
- 1965-08-31 US US484135A patent/US3328750A/en not_active Expired - Lifetime
Patent Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2384721A (en) * | 1943-10-02 | 1945-09-11 | Cambridge Rubber Co | Life preserving apparatus |
US3061249A (en) * | 1959-05-22 | 1962-10-30 | Ultra Electronics Ltd | Floating means |
US3154268A (en) * | 1962-09-19 | 1964-10-27 | Jr Arthur D Struble | Balloon and parachute combination |
US3234503A (en) * | 1963-03-27 | 1966-02-08 | Hoffman Electronics Corp | Drag chute and flotation device |
US3161896A (en) * | 1963-11-20 | 1964-12-22 | Ira T Holt | Ram air inflated flotation bag |
Cited By (13)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3377615A (en) * | 1966-04-25 | 1968-04-09 | Sparton Corp | Compliant suspension system |
US3514058A (en) * | 1968-05-03 | 1970-05-26 | Us Navy | Self-inflating retardation and floatation device |
US3561705A (en) * | 1969-02-24 | 1971-02-09 | Raymond S Daughenbaugh | Self-inflating target deployment container |
US3755836A (en) * | 1970-09-28 | 1973-09-04 | Itt | Stabilization arrangement for communication buoys |
US3889224A (en) * | 1974-03-08 | 1975-06-10 | Us Navy | Crown float/decelerator |
FR2438587A1 (en) * | 1974-11-28 | 1980-05-09 | France Etat | LOADING AND FLOATING DEVICE FOR A SUSPENDED LOAD |
US4298963A (en) * | 1974-11-28 | 1981-11-03 | Etat Francais Represente Par Le Delegue Ministeriel Pour L'armement | Jettisoning and flotation device for a suspended load, particularly an underwater listening body |
US4407607A (en) * | 1982-02-05 | 1983-10-04 | Mccambridge Joseph | Fluid dynamic erosion control unit |
US5406294A (en) * | 1993-05-13 | 1995-04-11 | Spears Associates, Inc. | Floating antenna system |
US20040185727A1 (en) * | 2003-03-17 | 2004-09-23 | Japan Aircraft Manufacturing Co., Ltd. | Airdrop type buoy apparatus |
US6814638B2 (en) * | 2003-03-17 | 2004-11-09 | Japan Aircraft Manufacturing Co., Ltd. | Airdrop type buoy apparatus |
US20050093754A1 (en) * | 2003-10-30 | 2005-05-05 | Lyons Alan M. | Light-weight signal transmission lines and radio frequency antenna system |
US7095377B2 (en) * | 2003-10-30 | 2006-08-22 | Lucent Technologies Inc. | Light-weight signal transmission lines and radio frequency antenna system |
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