Aeronautics and astronautics – Safety lowering devices – Parachutes
Reexamination Certificate
2000-08-25
2002-03-12
Poon, Peter M. (Department: 3643)
Aeronautics and astronautics
Safety lowering devices
Parachutes
C244S142000
Reexamination Certificate
active
06354539
ABSTRACT:
This specification incorporates by reference the disclosure of German priority document 19807.
BACKGROUND OF THE INVENTION
The invention relates to a parachute comprising a parachute canopy having an apex and a base as well as rigging lines attached to the base for retaining the object to be decelerated by the parachute, whereby the parachute is prepared for its use by folding of its parachute canopy as well as its rigging lines into a reefed pack.
Such parachutes are known by virtue of their use in a multitude of situations, whereby the parachute canopy of such a parachute, in the context of its preparation, is prepared for its situational use. The applicable reefed pack is thus typically configured such that the parachute canopy with carry lines is laid out in an extended configuration and, thereafter, is continuously folded in a direction from the apex to the base, whereby, from the beginning of the deployment, the air flow enters into the parachute canopy from the base and the bottleneck pressure resulting therefrom operates to effect deployment of the parachute canopy. As a result of such reefing configurations, the bottleneck pressure is first effective only when the parachute canopy, including the rigging lines which retain the object to be decelerated, have achieved an extended disposition.
The known parachutes bring therewith the disadvantage that, in connection with the extension of the parachute canopy including the rigging lines, there occurs a respective deployment impact or an extension impact which amounts to a considerable loading of the parachute, in dependence upon the instantaneous velocity existing at that moment of deployment. It follows from this that, in connection with high setting out speed and the correspondingly high flow velocity, the phenomenon can occur in which the air mass which is required to expand out the parachute canopy, once the parachute canopy has been pulled from the pack tube and extended, does not follow the flow velocity of the first impact of air which flows from the base to the apex, whereby the base of the parachute canopy closes again onto itself and the deployment is not achieved.
A further disadvantage exists in that, in connection with the intended situational use of the parachute such as, for example, an aircraft braking means, a stabilization parachute, a load parachute, or a personnel rescue parachute, and the resultant setting out speed of the parachute canopy which is correspondingly developed as a result of the particular situational use, it is necessary to use different customized web constructions such as, for example, in the form of banded parachutes or in the form of various parachute canopy materials having differing air through passage characteristics, whereby different parachutes must be kept available for handling different situational uses.
The invention solves the challenge of providing a parachute of the type deployable in a broad range of uses and which ensures a secure deployment in these uses.
SUMMARY OF THE INVENTION
The solution of this challenge, as well as the advantageous configurations and enhancements of the invention, are derivable from the subject matter of the patent claims which follow this description.
The invention provides, as its base concept, that the packing of the parachute canopy is comprised of concentric gathered folds obtained by gathering the parachute canopy fabric, which is laid out in the inflated airborne shape of the parachute, across the entire circumference of the parachute canopy from the base to the apex and across the full height of the parachute canopy.
The invention has the advantage that, as a result of the gathering of the parachute canopy into individual folds across the height of the parachute canopy, the base of the parachute canopy remains open in the respective inflow direction, whereupon a secure deployment results as well in the event of a high air inflow velocity. In such event, the bottleneck pressure which is applied to the apex of the parachute canopy upon the beginning of the deployment ensures a sequential unfolding of the individual folds and, in fact, ensures such a sequential unfolding in correspondence with the blocking pressure being applied against the object to be decelerated. As a consequence of this occurrence, a proportional unfolding of the parachute canopy advantageously occurs with respect to the respectively applied bottleneck pressure, whereby, in the event of a high inflow velocity, only a small parachute surface is respectively unfolded or released via unrolling of the folds while, in the event of a lower inflow velocity, the release of a greater parachute surface is effected. In this manner, the security of the parachute is collectively improved because an immediate complete opening of the parachute without additional unfolding means can be ensured even in the event of a setting out of the parachute at a low height and at a low speed. Another advantage is obtained during the deployment by virtue of the serial unfolding of the concentric gathered folds in that the rigging lines attached to the base of the parachute canopy are by and by lengthened in correspondence with the respective deployment of the parachute canopy whereby a deployment impact or extension impact is substantially avoided or occurs only in a very mitigated form.
A computation can be applied to a respective situational use of a parachute, in accordance with one embodiment of the invention, such that a plurality of concentric gathered folds can be coupled to one another in a predetermined manner via the surrounding control lines to create individual deployment zones. In this regard, it is possible, during the packing of a parachute, to prospectively arrange its opening sequence, whereby the control lines can be configured with differing breaking strengths to effect the creation of the individual deployment zones. In this manner, the sequential deployment of the thus configured deployment zones can be preset to react in correspondence with the occurrence of an anticipated bottleneck pressure during the deployment of the parachute.
The invention offers, in a beneficial manner, the hitherto unavailable possibility to configure different parachute constructions into a single parachute canopy, such that, in accordance with an embodiment of the invention, there is provided a parachute canopy comprised of sections of differing web constructions and each respective section is matched up to a prescribed deployment zone. In this manner, in accordance with the respective situational use of a parachute, a different web construction—such as, for example, in the form of a banded parachute or a web construction having a different porosity—can be configured for each individual deployment zone so that a deployment of the parachute in any given air velocity category can be achieved with the desired spread of the parachute by a targeted time-delayed release or a release corresponding to the respective instantaneous bottleneck pressure of the individual deployment zones.
It is accordingly provided in one embodiment of the invention that the gathered rigging lines are attached to the respective lowermost fold of the individual deployment zone. In this manner, it is ensured that a lengthening of the rigging lines occurs only in that respective spread as the respective fold is released during deployment of the parachute.
In accordance with a preferred embodiment of the invention, the apex of the parachute canopy is arranged on a platform. The configuration of the platform permits further advantageous embodiments of the invention. In this regard, it can be provided that the folds are disposed on the platform and are unrollable from the platform during deployment of the parachute. This results, during packing of the parachute canopy, in a readily deployable packed parachute unit. The deployment of such a packed parachute effects the creation of a bottleneck pressure of a calculable magnitude necessary for a deployment of the parachute against the platform.
Moreover, in accordance with an embodiment
Autoflug GmbH & Co.
Becker R. W.
Jakel Kevin
Poon Peter M.
R.W. Becker & Associates
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