GB2218950A - An air descent control and flotation device - Google Patents

An air descent control and flotation device Download PDF

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Publication number
GB2218950A
GB2218950A GB8907452A GB8907452A GB2218950A GB 2218950 A GB2218950 A GB 2218950A GB 8907452 A GB8907452 A GB 8907452A GB 8907452 A GB8907452 A GB 8907452A GB 2218950 A GB2218950 A GB 2218950A
Authority
GB
United Kingdom
Prior art keywords
bag
inflated
bottom end
air
dropped
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Granted
Application number
GB8907452A
Other versions
GB8907452D0 (en
GB2218950B (en
Inventor
Murray O Hill
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Minister of National Defence of Canada
UK Secretary of State for Defence
Original Assignee
Minister of National Defence of Canada
UK Secretary of State for Defence
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Minister of National Defence of Canada, UK Secretary of State for Defence filed Critical Minister of National Defence of Canada
Publication of GB8907452D0 publication Critical patent/GB8907452D0/en
Publication of GB2218950A publication Critical patent/GB2218950A/en
Application granted granted Critical
Publication of GB2218950B publication Critical patent/GB2218950B/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B63SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
    • B63BSHIPS OR OTHER WATERBORNE VESSELS; EQUIPMENT FOR SHIPPING 
    • B63B22/00Buoys
    • B63B22/003Buoys adapted for being launched from an aircraft or water vehicle;, e.g. with brakes deployed in the water
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42AMMUNITION; BLASTING
    • F42BEXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B10/00Means for influencing, e.g. improving, the aerodynamic properties of projectiles or missiles; Arrangements on projectiles or missiles for stabilising, steering, range-reducing, range-increasing or fall-retarding
    • F42B10/32Range-reducing or range-increasing arrangements; Fall-retarding means
    • F42B10/48Range-reducing, destabilising or braking arrangements, e.g. impact-braking arrangements; Fall-retarding means, e.g. balloons, rockets for braking or fall-retarding
    • F42B10/50Brake flaps, e.g. inflatable

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  • Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • General Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • Ocean & Marine Engineering (AREA)
  • Details Of Aerials (AREA)

Abstract

An air descent control and flotation device comprising a collapsible, inflatable bag having a bottom end adapted for connection to an object to be dropped into a body of water from a height, the bag being configured to produce substantial aerodynamic drag when inflated and passing through air bottom end first, so as to slow descent of the object when dropped, the bag having an inflated volume sufficient to float the object at the surface of the body of water. Various shapes are disclosed. The bag may incorporate a directional discontinuity ring radiator antenna 18 including an upper open wire loop 20 with an impedance match section 22 connected at 24 to core 26 of a coaxial line 28, and connected at 30 to a braided wire 32 forming a second loop, which is connected at 34 to the shield of the coaxial line 28. <IMAGE>

Description

AN AIR DESCENT CONTROL AND FLOTATION DEVICE The present invention relates to a combined air descent control and flotation device for use with an object to be dropped into a body of water from a height.
Conventionally, bodies that are dropped into water from a height, for example from an aircraft, carry separate air descent control and flotation devices. The air descent control device may be, for example, a parachute or a rotochute. The flotation device is usually inflated upon water entry and may be in the form of a bag, ring or the like. In some circumstances, as when dealing with large numberS of small objects to be dropped into a body of water, it is desirable to limit the size and complexity of the complete package to be air dropped. The present invention proposes a device that combines the function of the air descent control apparatus and the flotation device.
According to the present invention there is provided an air descent control and flotation device comprising a collapsible, inflatable bag having a bottom end adapted for connection to an object to be dropped into a body of water from a height, the bag being configured to produce substantial aerodynamic drag when inflated and passing through air bottom end first, so as to slow descent of the object when dropped, the bag having an inflated volume sufficient to float the object at the surface of the body of water.
Where the object to be dropped into water contains a telecommunications apparatus, an antenna may be integrated with the wall of the inflatible bag so that the antenna is deployed by inflation of the bag.
In the accompanying drawings, which illustrate exemplary embodiments of the present invention: Figure 1 is a perspective view of one embodiment of the descent control and flotation device; Figure 2 is an elevational view, partially broken away of the device of Figure 1; Figure 3 is an elevational view of an alternative form of the device; and Figure 4 is an elevational view of a third embodiment of the device.
Referring to the drawinys, and particularly to Figures 1 and 2, there is illustrated a combined descent control and flotation device 10. This device is in the form of an inflatable bag with a right cylindrical side wall 12 and a frustoconical bottom end 14 with a central neck 16. The frustoconical send 14 acts as a braking panel when the neck of the inflated bag is secured to an object that is falling through the air.
The device illustrated in Figures 1 and 2 also incorporates a directional discontinuity ring radiator antenna 18.
This device includes an upper open wire loop 20 that is spaced slightly below the top of the side wall. One end of this loop is an impedance match section 22 that is connected at a position 24 spaced from its end to the core 26 of a co-axial feed line 28.
The end of the impedance match section 22 is connected at 30 to a braided wire 32 that forms another loop spaced below and parallel to the loop of wire 20. The shield of the co-axial feed line 28 is connected to the braided wire 32 at 34.
The directional discontinuity ring radiator antenna thus constructed is attached internally to the float material. The antenna requires a significantly smaller float to house it than the conventionally used quarter wave ground plane antenna, while providing a vertically polarized radiation pattern.
Turning to Figure 3, there is illustrated an air descent control and flotation device 40 that is generally similar to the device 10 of Figures 1 and 2. In this case however, the side wall 42 of the device is frustoconical, tapering from bottom to top.
The top panel 44 of the device is flat.
Figure 4 illustrates a third embodiment of the device where the side wall 52 is conical.
The embodiments of Figures 3 and 4 may include helically wound antennas that are deployed with the inflation of the bag.
While certain embodiments of the present invention have been described in the foregoing, it is to be understood that other embodiments are possible within the scope of the invention. In particular, it is to be understood that different shapes of inflatable bag and different antenna configurations can be employed.

Claims (9)

1. An air descent control and flotation device comprising a collapsible, inflatable bag having a bottom end adapted for connection to an object to be dropped into a body of water from a height, the bag being configured to produce substantial aerodynamic drag when inflated and passing through air bottom end first, so as to slow descent of the object when dropped, the bag having an inflated volume sufficient to float the object at the surface of the body water.
2. A device according to claim 1 and including a neck at the centre of the bottom end of the bag.
3. A device according to claim I or claim 2 wherein the bottom end of the bag is of frustoconical configuration.
4. A device according to any one of the preceding claims wherein the inflated bag has a right circular cylindrical side.
5. A device according to any one of the preceding claims wherein the inflated bag has a conical top surface.
6. A device according to any one of claims I to 3 wherein the inflated bag has a flat top surface and a frusto conical side.
7. A device according to any one of the preceding claims and including ahEicaly wound antenna inside the bag.
8. A device according to any one of claims 1 to 6 and including a directional discontinuity ring radiator antenna attached to the wall of the bag.
9. An air descent control and flotation device substantially as herein described with reference to Figures 1 and 2, Figure 3 or Figure 4 of the accompanying drawings.
GB8907452A 1988-05-26 1989-04-03 An air descent control and flotation device Expired - Lifetime GB2218950B (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CA567753 1988-05-26

Publications (3)

Publication Number Publication Date
GB8907452D0 GB8907452D0 (en) 1989-05-17
GB2218950A true GB2218950A (en) 1989-11-29
GB2218950B GB2218950B (en) 1992-09-30

Family

ID=4138080

Family Applications (1)

Application Number Title Priority Date Filing Date
GB8907452A Expired - Lifetime GB2218950B (en) 1988-05-26 1989-04-03 An air descent control and flotation device

Country Status (1)

Country Link
GB (1) GB2218950B (en)

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3514058A (en) * 1968-05-03 1970-05-26 Us Navy Self-inflating retardation and floatation device
US3889224A (en) * 1974-03-08 1975-06-10 Us Navy Crown float/decelerator
EP0007830A1 (en) * 1978-07-18 1980-02-06 Thomson-Csf Air-dropped buoy
EP0015177A1 (en) * 1979-02-27 1980-09-03 Thomson-Csf Air-dropped buoy with aerodynamic and inertial releases
EP0024988A1 (en) * 1979-08-28 1981-03-11 Thomson-Csf Air-dropped buoy
GB1588917A (en) * 1974-11-28 1981-04-29 France Armed Forces Parachute load-laying device

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3514058A (en) * 1968-05-03 1970-05-26 Us Navy Self-inflating retardation and floatation device
US3889224A (en) * 1974-03-08 1975-06-10 Us Navy Crown float/decelerator
GB1588917A (en) * 1974-11-28 1981-04-29 France Armed Forces Parachute load-laying device
EP0007830A1 (en) * 1978-07-18 1980-02-06 Thomson-Csf Air-dropped buoy
EP0015177A1 (en) * 1979-02-27 1980-09-03 Thomson-Csf Air-dropped buoy with aerodynamic and inertial releases
EP0024988A1 (en) * 1979-08-28 1981-03-11 Thomson-Csf Air-dropped buoy

Also Published As

Publication number Publication date
GB8907452D0 (en) 1989-05-17
GB2218950B (en) 1992-09-30

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Legal Events

Date Code Title Description
PCNP Patent ceased through non-payment of renewal fee

Effective date: 19960403