What is claimed is:
1. A cryogenic valve device comprising a valve body defining a cryogenic fluid flow duct, a shutter element disposed in the duct and connected to a control rod for moving said shutter element between a closed position in which it closes the duct and an open position in which the cryogenic fluid flows freely along the duct, thereby controlling the flow rate of the cryogenic fluid, the valve device further comprises a pneumatic actuator comprising a chamber defining two cavities and containing a piston in connection with the control rod, the cavities being fed with a control gas for positioning the piston in any position between the closed position and the open position of the shutter element, and an intermediate chamber at positive pressure relative to the surrounding pressure and disposed between the actuator and the valve body in such a manner as to thermally decouple the actuator from the valve body and isolate the actuator from the surrounding environment.
2. A valve device according to claim 1, wherein the intermediate chamber comprises a thermally insulating spacer.
3. A valve device according to claim 1, wherein the control rod further comprises a thermally insulating spacer for thermally decoupling the shutter element from the piston.
4. A device according to claim 1, wherein the actuator, the intermediate chamber, and the valve body include respective casings, said casings being interconnected in leaktight manner so as to confine the control gas and the cryogenic fluid inside the device.
5. A device according to claim 1, wherein the intermediate chamber includes an opening connected to a leak-recovery device.
6. A device according to claim 5, wherein the leak-recovery device is connected to a measuring appliance for detecting malfunction of the valve or of the actuator.
7. A valve device according to claim 1, wherein the intermediate chamber includes first and second openings to enable a sweeping fluid to flow through said chamber.
8. A valve device according to claim 1, wherein the actuator includes means on its outside surface for increasing the inflow of heat thereto.
9. A valve device according to claim 1, wherein the actuator includes insulating material on its outside surface to limit heat exchange between the actuator and the outside.
10. A valve device according to claim 1, wherein the pneumatic actuator is of the linear actuator type for actuating a shutter element in the form of a valve member, the piston of said actuator having a rod connected to the control rod via coupling means for transmitting linear movement to the control rod connected to the valve member so as to move the valve member between the closed position in which the valve member is in contact with a seat provided in the duct, and an open position in which the valve member is raised vertically to a distance from said seat.
11. A valve device according to claim 1, wherein the pneumatic actuator is of the pivoting actuator type for actuating a pivotal shutter element of the butterfly type, the piston being connected to the control rod by a crank for transmitting pivoting movement to the control rod connected to the butterfly so as to position the butterfly in an arbitrary position between the closed position and the open position.
12. A valve device according to claim 11, further comprising an insulating spacer interposed between the control rod and the crank for reducing heat exchange between the actuator and the pivotal shutter element.
13. A valve device according to claim 11, further comprising an insulating spacer interposed between the control rod and the pivotal shutter element to reduce heat exchange between the actuator and the shutter element.
14. A valve device according to claim 11, wherein the piston includes first and second insulating spacers disposed respectively on either side of a connection point between the crank and the piston to reduce heat exchange between the actuator and the shutter element.
15. A valve device according to claim 11, wherein the crank is made of a thermally insulating material.
16. A valve device according to claim 1, wherein the actuator further comprises first and second control gas delivery circuits, said delivery circuits forming heat exchangers with the actuator or the valve body.
17. A valve device according to claim 1, further comprising a pipe for taking cryogenic fluid, the pipe being connected between the duct and a control gas feed opening for the chamber, said pipe including means for vaporizing the cryogenic fluid that has been taken, and a pipe for reinjecting the control gas which is connected between a control gas exhaust opening of the chamber and the duct, said pipe including means for condensing the exhausted gas.
18. A valve device according to claim 1, wherein the control gas has a saturation temperature or a critical temperature that is substantially equal to or greater than the temperature of the cryogenic fluid present in the duct.
19. A valve device according to claim 18, wherein the control gas used in the actuator is dry nitrogen.
20. A valve device according to claim 18, wherein the control gas used in the actuator is dry air.
The claims below are in addition to those above.
All refrences to claim(s) which appear below refer to the numbering after this setence.
1. A method for launching an aircraft having an envelope for receiving a lift gas that is lighter than air, the method comprising:
introducing the lift gas into the envelope of the aircraft so that the aircraft is buoyant and the lift gas is substantially separate from a second gas in the envelope;
releasing the aircraft such that a longitudinal axis of the envelope extending between first and second distal ends thereof is oriented at an angle of at least about 45 degrees relative to horizontal while the aircraft ascends; and
venting gas from the envelope as the aircraft ascends.
2. A method according to claim 1 wherein said introducing step comprises introducing helium into the envelope as the lift gas.
3. A method according to claim 1 wherein said venting step comprises venting air from the envelope such that the envelope maintains a substantially constant volume.
4. A method according to claim 1 further comprising connecting a buoyant balloon to the first end of the envelope such that the balloon lifts the first end of the envelope.
5. A method according to claim 1 further comprising providing a gas bag in the envelope and at least partially filling the gas bag with the lift gas such that the gas bag lifts the first end of the aircraft.
6. A method according to claim 1 further comprising at least partially filling the envelope with the lift gas such that the lift gas raises the first end of the envelope, rotating the longitudinal axis of the envelope from a generally horizontal orientation to an angle of at least about 45 degrees relative to horizontal.
7. A method according to claim 1 wherein said introducing step comprises injecting the lift gas through a tubular channel extending into the envelope and proximate an upper portion of the envelope to minimize mixing of the lift gas in the envelope.
8. A method according to claim 1 further comprising at least partially venting the lift gas from the envelope and receiving air in the envelope such that the aircraft descends with the envelope in a substantially filled configuration.
9. A method according to claim 8 further comprising repeating said introducing, releasing, and first and second venting steps in order to repeat the launching of the aircraft.