Parachute with canopy slits or openings for preventing canopy inversion
Parachutes which have a generally circular skirt or hem, such as semi-hemispherical, extended gore, or any variant of axisymmetric parachutes and cruciform parachutes with arms attached are disclosed with a plurality of vertical slits located in a circumferential band adjacent the skirt or hem of the parachute to prevent canopy inversion. During deployment, when the outer portion of the canopy is exposed to air flow, the slits open up and the drag of the skirt of the canopy is reduced, thus limiting the potential for hem migration. The slits are positioned to allow airflow therethrough in order for the pressure on the outside of the canopy to be transferred through the slit openings and released or transferred to inside of the lower section of the canopy. Instead of slits, elongated narrow openings can be utilized.
1 . A parachute comprising:
a canopy including multiple gores having a gore length and a generally circular skirt or hem around a lower edge of said canopy, said skirt or hem having a skirt band;
suspension lines attached to said skirt band and configured to support a load;
a plurality of generally vertical reinforced slits spaced around said canopy and extending upwardly from said skirt band to a vertical slit top end; and
a corresponding plurality of generally horizontal reinforced slits positioned at each said vertical slit top end.
2 . The parachute in accordance with claim 1 , wherein the parachute is a semi-hemispherical, extended gore or any variant of axisymmetric parachute.
3 . The parachute in accordance with claim 1 , wherein the parachute is a cruciform parachute with arms attached forming corner air openings.
4 . The parachute in accordance with claim 1 , wherein said vertical slits are positioned mid-center of each gore and each of said horizontal slits is positioned adjacent a lower edge of each gore, preferably 5% to 10% of the gore length from the lower edge of the gore, and having a mid-point at said vertical slit top end.
5 . The parachute in accordance with claim 1 , wherein said generally vertical slits and said generally horizontal slits allow airflow through openings formed by said generally vertical slits and said generally horizontal slits during deployment in order for air pressure on an outside of the canopy to be transferred through the openings and released to a lower inside of the canopy.
6 . The parachute in accordance with claim 1 , wherein said generally vertical slits and said generally horizontal slits are equally spaced around a continuous anti-inversion band extending around a lower portion of said gores with a bottom of said continuous anti-inversion band defined by a reinforcement of said skirt or hem with said continuous anti-inversion band and an upper edge of said continuous anti-inversion band defined by a reinforcement extending around said multiple gores, said generally horizontal slits being formed in said upper edge continuous anti-inversion band reinforcement.
7 . A parachute comprising:
a canopy including multiple gores in a generally circular skirt or hem around a lower edge thereof, said skirt or hem having a skirt band;
suspension lines attached to said skirt band and configured to support a load;
a plurality of generally vertical reinforced slits or elongated narrow openings spaced around said canopy and extending upwardly from an area adjacent said skirt band to a vertical slit or narrow opening top end; and
a corresponding plurality of generally horizontal reinforced slits or elongated narrow openings positioned at each said vertical slit or narrow opening top end, said generally vertical slits or elongated narrow openings and said generally horizontal slits or elongated narrow openings being configured to enable airflow therethrough so as to prevent canopy inversion during deployment.
8 . The parachute in accordance with claim 7 , wherein said generally vertical slits or elongated narrow openings are contained within a continuous anti-inversion band extending around a lower portion of said gores with a bottom of said continuous anti-inversion band defined by a reinforcement of said skirt or hem, and an upper edge of said continuous anti-inversion band defined by a reinforcement extending around said multiple gores, said generally horizontal slits or elongated narrow openings formed in said continuous anti-inversion band upper edge reinforcement.
9 . The parachute in accordance with claim 8 , wherein a total area of the generally vertical slits or narrow openings and the generally horizontal slits or elongated narrow openings constitutes no more than 2.5% of a total area of the circular anti-inversion band.
10 . The parachute in accordance with claim 7 , wherein the parachute is a semi-hemispherical, extended gore or any variant of axisymmetric parachute.
11 . The parachute in accordance with claim 7 , wherein the parachute is a cruciform parachute with arms attached forming corner air openings.
12 . The parachute in accordance with claim 7 , wherein said generally vertical slits or elongated narrow openings and said generally horizontal slits or elongated narrow openings are spaced equally around said canopy.
13 . The parachute in accordance with claim 7 , wherein a number of said generally vertical slits or elongated narrow openings and said generally horizontal slits or elongated narrow openings is no less than fifty percent (50%) of a number of said gores.
14 . The parachute in accordance with claim 7 , wherein opening of said generally vertical slits or elongated narrow openings and said generally horizontal slits or elongated narrow openings during deployment reduces drag of the skirt or hem of the canopy, thus limiting potential for skirt or hem migration.
15 . The parachute in accordance with claim 7 , wherein air flow through said generally vertical slits or elongated narrow openings and said generally horizontal slits or elongated narrow openings transfers air pressure on an outside the canopy through said slits or openings to a lower inside of the canopy during deployment.
16 . The parachute in accordance with claim 7 , wherein each of the generally vertical slits or elongated narrow openings and the corresponding generally horizontal slits or elongated narrow openings has a T-shaped configuration.
17 . A method of providing anti-inversion capability to a parachute having a canopy with a generally circular skirt or hem around a lower edge thereof, the skirt or hem having a skirt band, said method comprising providing a plurality of generally vertical reinforced single slits or elongated narrow openings spaced around the lower edge of said canopy, and extending upwardly from said skirt band, said slits or openings being configured to enable air flow during deployment such that air pressure on an outside of the canopy is transferred through the slits or openings and released to a lower inside of the canopy so as to prevent canopy inversion during the deployment.
18 . The method in accordance with claim 17 , wherein the parachute is selected from the group consisting of semi-hemispherical, extended gore and any variant of axisymmetric parachutes and cruciform parachutes with arms attached to form corner openings.
19 . The method in accordance with claim 17 , wherein said slits or openings are also configured to reduces drag of the skirt or hem of the canopy during deployment.
20 . The method in accordance with claim 17 , wherein said generally vertical reinforced slits or elongated narrow openings extend upwardly to a vertical slit or narrow opening top end, and a corresponding plurality of generally horizontal reinforced slits or elongated narrow openings are positioned at said vertical slit or narrow opening top end.
21 . The method in accordance with claim 20 , wherein said generally vertical slits or elongated narrow openings are contained within a continuous anti-inversion band around a lower portion of said gores with a bottom of said continuous anti-inversion band defined by a reinforcement of said skirt or hem and an upper edge of said continuous anti-inversion band defined by a reinforcement extending around said multiple gores, said generally horizontal slits or elongated narrow openings formed in said continuous anti-inversion band upper edge reinforcement.
22 . The method in accordance with claim 17 , wherein a bottom end of each of the single slits or elongated narrow openings is located adjacent to the skirt band.
23 . The method in accordance with claim 17 , wherein one of the plurality of generally vertical reinforced single slits or elongated narrow openings spaced around said canopy and extending upwardly from said skirt band is positioned midway between each radial of the canopy.
24 . The method in accordance with claim 17 , wherein one or more of the plurality of generally vertical reinforced single slits or elongated narrow openings spaced around said canopy and extending upwardly from said skirt band are positioned between each radial of the canopy.
25 . The method in accordance with claim 17 , wherein the plurality of generally vertical reinforced single slits or elongated narrow openings extend upwardly from the skirt, and have a vertical height of between about five percent (5%) and about fifteen percent (15%) of a gore length.
26 . A method of providing anti-inversion capability to a parachute having a canopy with a generally circular skirt or hem around a lower portion thereof, the skirt or hem having a skirt band, said method comprising providing a plurality of generally vertical reinforced slits spaced around said canopy and extending upwardly from said skirt band to a vertical slit top end, and a corresponding plurality of generally horizontal reinforced slits positioned at each vertical slit top end, said generally vertical slits and said generally horizontal slits enabling air flow therethrough during deployment such that air pressure on an outside of the canopy in transferred through said generally vertical and said generally horizontal slits and released to a lower inside of the canopy so as to prevent canopy inversion during the deployment.
27 . The method in accordance with claim 26 , wherein the parachute is selected from the group consisting of semi-hemispherical, extended gore and any variant of axisymmetric parachutes and cruciform parachutes with arms attached to form corner openings.