US20010005000A1

US20010005000A1 - Opening reinforcement for aerostat envelope

Info

Publication number: US20010005000A1
Application number: US09/742,543
Authority: US
Inventors: Casteras Christophe
Original assignee: Individual
Current assignee: Centre National dEtudes Spatiales CNES
Priority date: 1998-06-26
Filing date: 2000-12-22
Publication date: 2001-06-28
Anticipated expiration: 2019-06-24
Also published as: EP1087886B1; WO2000000386A1; DE69912603D1; EP1087886A1; US6394388B2; FR2780379B1; FR2780379A1

Abstract

An aperture-reinforcing device for flexible envelopes which are intended to be tensioned, and in particular for aerostat envelopes, includes adjacent first and second annular members. The envelope is passed successively over the inside parts of the surfaces of the first and second annular members, then the outside part of the surface of the second annular member, and then again over the inside part of the surface of the first annular member, between itself and that part.

Description

This application is a continuation of International PCT Application PCT/FR/99/01521 filed on Jan. 24, 1999, which designated the United States of America.

BACKGROUND OF THE INVENTION

1. Field of the Invention

The present invention relates to an aperture-reinforcing device for flexible envelopes intended to be tensioned, and in particular to an aperture-reinforcing device for aerostat envelopes.

2. Description of the Prior Art

FIG. 1 of the accompanying drawings is a general view of a conventional experimental aerostat also known as a “sonde balloon”.

As can be seen in FIG. 1, an aerostat of this kind typically includes a

flexible envelope

1 filled with a gas lighter than air, such as hydrogen or helium.

The envelope comprises a plurality of plastics

material film panels

2 welded together in the meridian direction and converging toward a top part 3 of the aerostat referred to as the “North Pole” and toward a bottom part 4 of the aerostat referred to as the “South Pole”.

The

panels

2 forming the envelope 1 are conventionally made of polyethylene reinforced with polyester fibers and the polar zones 3, 4 of the envelope 1 include aperture-reinforcing

devices

5, 6 consisting either of circular flanges fixed by nuts and bolts or of components glued to the envelope.

The aperture-

reinforcing device

6 of the South Pole of the balloon includes a ring 7 adapted to support a flight system 8, typically comprising a basket 9 that can carry scientific instruments, a radar reflector 10 and a parachute 11.

New composite envelope materials have recently been used to improve the strength-to-weight ratio of experimental aerostat envelopes, so that larger payloads can be carried.

For example, new generation envelope open stratosphere balloons have envelopes comprising very thin polyester panels reinforced with carbon fibers or oriented polyethylene fibers.

These extremely light materials unfortunately have the disadvantage of being prone to tearing by shear forces, i.e. forces applied in the direction transverse to the plane of the envelope.

For this reason, conventional aperture-reinforcing devices at the poles are not suitable for the new generation envelopes, because they apply high shear forces to the panels.

An object of the present invention is to provide a pole aperture-reinforcing device suitable for this new type of envelope.

SUMMARY OF THE INVENTION

The above object of the invention, and others that will become apparent on reading the following description, are met by an aperture-reinforcing device for flexible envelopes intended to be tensioned, and in particular for aerostat envelopes, the device including adjacent first and second annular members such that the envelope can pass successively over inside parts of surfaces of the first and second annular members, then over an outside part of a surface of the second annular member, and then again over the inside part of the surface of the first annular member, between itself and the part.

According to one feature of the invention the aperture-reinforcing device further includes means for urging the first and second annular members together to immobilize the envelope when it is not tensioned.

According to another feature of the invention a first flange is fixed to the periphery of the first annular member, a second flange is placed over the second annular member, and a plurality of springs is tensioned between the first and second flanges.

According to another feature of the invention a seal is disposed between the second flange and the second annular member to enable sealed closure of the aperture-reinforcing device.

According to another feature of the invention the first and second annular members are toroidal.

Because of the above features, the aperture-reinforcing device according to the invention applies low shear forces to the panels of the envelope in the polar zones.

What is more, an aperture-reinforcing device according to the invention can be made from a small number of components, reducing its mass and its manufacturing cost.

Other features and advantages of the present invention will become apparent on reading the following description and examining the accompanying drawings.

BRIEF DESCRIPTION OF THE DRAWINGS

FIG. 1 is a general view of an experimental aerostat described in the preamble of this description. [0023]
FIG. 2 is a top view of an aperture-reinforcing device according to the invention for reinforcing the North Pole of the envelope of an experimental aerostat. [0024]
FIG. 3 is a view of the same aperture-reinforcing device in section taken along the line III-III in FIG. 2. [0025]
FIG. 4 is a bottom view of an aperture-reinforcing device according to the invention for reinforcing the South Pole of the envelope of an experimental aerostat. [0026]
FIG. 5 is a view of the same aperture-reinforcing device in section taken along the line V-V in FIG. 4. [0027]

DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENT

In the figures, identical reference numerals designate identical or similar units. [0028]
The aperture-reinforcing device according to the invention is described hereinafter when incorporated into an experimental aerostat, because this is a particularly suitable application of the invention. [0029]
Nevertheless, it must be borne in mind that the aperture-reinforcing device could be equally suitable for any other application in which it is necessary to immobilize a flexible envelope that is intended to be tensioned. [0030]
FIGS. 2 and 3 show a first aperture-reinforcing [0031] device 5 for reinforcing the North Pole of the envelope 1 of an experimental balloon.
As shown in FIGS. 2 and 3, the first aperture-reinforcing device includes first and second adjacent [0032] annular members 12 and 13 at its periphery, which members are preferably tubular and toroidal and preferably have the same radius.
A first [0033] annular flange 14 is fixed to the outside periphery of the first annular member 12.
An [0034] annular seal 15 is shaped to fit over the second annular member 13.
A second [0035] annular flange 16 is placed over the seal 15.
A plurality of [0036] springs 17 under tension between the first and second flanges 14 and 16 pull them toward each other.
A [0037] cover 18 fixed and sealed to the second flange 16 closes the aperture-reinforcing device.
A system (not shown) can be provided for opening the cover under remote control in order to release progressively the gas contained in the [0038] envelope 1.
For example, the first and second [0039] annular members 12 and 13 and the first and second flanges 14 and 16 can be made of aluminum or light alloy. The seal 15 can be made from a closed-cell elastomer material.
The aperture-[0040] reinforcing device 5 is fitted to the North Pole of the envelope 1 of the aerostat in the following manner (the envelope is shown in chain-dotted line in FIG. 3).
With the [0041] envelope 1 of the aerostat empty of gas, the first annular member 12 with the first flange 14 fixed to it is placed around the polar orifice of the envelope.
The second [0042] annular member 13 is then superposed on the first annular member 12.
The [0043] free edge 1 a of the envelope 1 is seized and passed over the interior parts of the surfaces of the first and second annular members 12 and 13 (i.e. over the parts of those surfaces which face toward the axis A of the aperture-reinforcing device).
The [0044] envelope 1 is then folded around the second annular member 13 so that it passes over the outside portion of its surface.
The [0045] envelope 1 is then passed again over the inside part of the surface of the first annular member 12, between itself and that part, and its free edge 1 a is brought out as far as the outside part of the surface of that member.
The [0046] seal 15 is then nested over the second annular member 13, after which the second flange 16 is placed over the seal 15.
The [0047] springs 17 are then tensioned between the first and second flanges 14 and 16, after which the cover 18 is fixed to the second flange 16.
When the aerostat is inflated, the [0048] envelope 1 is tensioned. The portion of the envelope under tension that extends around the aperture-reinforcing device 5 is designated by the reference numeral 1 b in FIG. 3.
Tensioning the [0049] envelope 1 immobilizes it against the first and second annular members 12 and 13, as is clear from the description of how the envelope 1 is wrapped around those members.
The [0050] envelope 1 presses the second annular member 13 against the first annular member 12, thereby jamming the envelope portion that passes between the two members.
The [0051] tensioned envelope 1 also jams the envelope portion that passes between itself and the inside part of the surface of the first annular member 12.
The [0052] springs 17 pull the first and second annular members 12 and 13 against each other and immobilize the envelope 1, even when it is not tensioned.
The springs also press the [0053] seal 15 against the second annular member 13 to seal the aperture-reinforcing device.
It should now be clear that the aperture-reinforcing [0054] device 5 eliminates the risk of shearing the envelope 1: all that is required to ensure this is to choose sufficiently large radii for the substantially circular sections of the first and second annular members 12 and 13.
It is also clear that the aperture-reinforcing [0055] device 5 can be made from a small number of components: very few screws are needed, in contrast to conventional pole-reinforcing devices.
It is finally clear that the aperture-reinforcing [0056] device 5 can be demounted very easily, whereas this is difficult with the conventional reinforcing devices.
FIGS. 4 and 5 show a second aperture-reinforcing [0057] device 6 for reinforcing the South Pole of the envelope 1 of an experimental aerostat.
Most components of the second aperture-reinforcing device are analogous to those of the first aperture-reinforcing [0058] device 5. They are therefore described very briefly, without expanding on their functions.
As can be seen in FIGS. 4 and 5, the second aperture-reinforcing [0059] device 6 includes adjacent first and second annular members 12′ and 13′ at its periphery. Those members are preferably tubular and toroidal.
The radius of the first [0060] annular member 12′ is preferably slightly less than that of the second annular member 13′.
This difference in their radii holds the [0061] envelope 1 in contact with the first annular member 12′ regardless of the inclination of the envelope relative to that member. This feature guarantees immobilization of the envelope during the inflation phase in particular.
An [0062] annular flange 14′ defining a substantially frustoconical volume is fixed to the outside periphery of the first annular member 12′.
An [0063] annular seal 15′ is shaped to fit over the second annular member 13′.
A [0064] circular flange 16′ forming a cover is placed over the seal 15′.
A plurality of [0065] springs 17′ in tension between the flange 14′ and brackets 20 fastened to the flange 16′ pull the flanges toward each other.
Unlike the first aperture-reinforcing [0066] device 5, the second aperture-reinforcing device 6 also includes a ring 21 fixed to the periphery of the flange 14′ and supporting a ring assembly 22.
The ring assembly can include a [0067] tripod 23, for example, fixed by screws 24 to the ring 21 and supporting the ring 7 previously mentioned.
Of course, the invention is not limited to the embodiment and the application described and shown, which are included merely by way of example. [0068]
For example, without limiting the scope of the invention, the aperture-reinforcing device according to the invention could equally well be used for the inflation orifices of “ZODIAC” (registered trademark) class inflatable boats. [0069]
The annular members described above could have a non-circular contour, for example an elliptical contour, although it is preferable for the contour to be looped and without discontinuities. [0070]

Claims

There is claimed:

1. An aperture-reinforcing device for flexible envelopes intended to be tensioned, and in particular for aerostat envelopes, said device including adjacent first and second annular members such that said envelope can pass successively over inside parts of surfaces of said first and second annular members, then over an outside part of a surface of said second annular member, and then again over said inside part of said surface of said first annular member, between itself and said part.

2. The aperture-reinforcing device claimed in

claim 1

further including means for urging said first and second annular members together to immobilize said envelope when it is not tensioned.

3. The aperture-reinforcing device claimed in

claim 2

wherein a first flange is fixed to the periphery of said first annular member, a second flange is placed over said second annular member, and a plurality of springs is tensioned between said first and second flanges.

4. The aperture-reinforcing device claimed in

claim 3

wherein a seal is disposed between said second flange and said second annular member to enable sealed closure of said aperture-reinforcing device.

5. The aperture-reinforcing device claimed in

claim 3

further including a load-support ring fixed to said first flange.

6. The aperture-reinforcing device claimed in

claim 1

wherein said first and second annular members are tubular and toroidal.

7. The aperture-reinforcing device claimed in

claim 1

wherein said first and second annular members have the same radius.

8. The aperture-reinforcing device claimed in

claim 1

wherein said first annular member has a radius slightly less than that of said second annular member.

9. An aerostat envelope including at least one aperture-reinforcing device at its North Pole or at its South Pole and wherein said device includes adjacent first and second annular members such that said envelope can pass successively over inside parts of surfaces of said first and second annular members, then over an outside part of a surface of said second annular member, and then again over said inside part of said surface of said first annular member, between itself and said part.

10. The envelope claimed in

claim 9

11. The envelope claimed in

claim 10

12. The envelope claimed in

claim 11

13. The envelope claimed in

claim 11

further including a load-support ring fixed to said first flange.

14. The envelope claimed in

claim 9

wherein said first and second annular members are tubular and toroidal.

15. The envelope claimed in

claim 9

wherein said first and second annular members have the same radius.

16. The envelope claimed in

claim 9