Multi-grommet retained slider for parachutes

1. In combination with a ram air parachute canopy having a wingspan with upper and lower airfoil surfaces separated by chordwise-extending ribs to form cells inflated by inflow of air at an open leading edge, and suspension lines connecting the lower surface of the canopy to a load, the improvement comprising:

a reefing slider with a spanwise length and a chordwise width having reinforced openings through which the suspension lines extend, said slider further having a plurality of separate retaining devices spaced along said spanwise length and secured to said canopy for retarding descent of the slider relative to the canopy from an upper reefing position in which inflation of the canopy is restricted, said slider being releasable from said canopy to descend along said suspension lines in response to release of said retaining devices due to force created by said inflow of air to said cells, a number of said retaining devices at a central area along said slider spanwise length and secured to a central part of said canopy wingspan being stronger than a number of said retaining devices at outer edges of said slider spanwise length and secured to wing tip portions of said canopy.

2. The combination as set forth in claim 1 , wherein each of said retaining devices includes a slider retaining element secured to said slider, and a canopy retaining element secured to said canopy, said slider retaining elements and said canopy retaining elements being releasably secured to one another and calibrated so that the force needed to separate the slider retaining elements from the canopy retaining elements is greater at said central part of said canopy wingspan than at said canopy wing tips.

3. The combination as set forth in claim 2 , wherein said slider retaining elements and said canopy retaining elements are mating magnetic elements.

4. The combination as set forth in claim 2 , wherein said slider retaining elements and said canopy retaining elements are mating snap fastener elements.

5. The combination as set forth in claim 2 , wherein each slider retaining element is secured to said slider adjacent a reinforced opening and said canopy retaining elements are secured to said canopy in spaced relationship corresponding to a spacing of said slider retaining elements so that said slider retaining elements and said canopy retaining elements are releasably secured to one another in corresponding pairs.

6. The combination as set forth in claim 5 , wherein said corresponding pairs of slider retaining elements and said canopy retaining elements are releasably secured to one another tie elements.

7. The combination as set forth in claim 6 , wherein said tie elements are cable-tie type fasteners.

8. The combination as set forth in claim 6 , wherein said tie elements include cord or string.

9. The combination as set forth in claim 8 , wherein each of said slider retaining elements includes a slider retaining loop and each canopy retaining element includes a canopy retaining loop, a tie element being passed through the paired loops on said slider and canopy and tied to join each corresponding pair.

10. The combination as set forth in claim 9 , wherein a tie strength of said tie elements incrementally increases from loop pairs adjacent said wing tips to loop pairs at the center area of the canopy.

11. The combination as set forth in claim 9 , wherein said tie element is passed through the loops of a corresponding pair of retaining elements more than once before being tied.

12. The combination as set forth in claim 11 , wherein tie elements of corresponding pairs at the central part of the canopy are passed through their associated loops a greater number of times than are tie elements of corresponding pairs at said wing tips so that a tie strength at the central part of the canopy is greater than a tie strength at the wing tips.

13. The combination as set forth in claim 12 , wherein a tie strength of tie elements connecting loops of corresponding pairs along the canopy wingspan between the central part and the wing tips is intermediate between said central part tie strength and said wing tip tie strength, said intermediate strength being determined by a number of times the tie elements pass through their associated pairs of loops before being tied.

14. A ram air parachute comprising:

a canopy having a wingspan and upper and lower airfoil surfaces separated by chordwise-extending ribs to form cells inflated by inflow of air at an open leading edge;

suspension lines connecting the lower surface of the canopy to a load; and

a reefing slider with a spanwise length and a chordwise width having reinforced openings through which the suspension lines extend, said slider further having a plurality of separate retaining devices spaced along said spanwise length and secured to said canopy for retarding descent of the slider relative to the canopy from an upper reefing position in which inflation of the canopy is restricted, said slider being releasable from said canopy to descend along said suspension lines in response to release of said retaining devices due to force created by said inflow of air to said cells, a number of said retaining devices at a center along said slider spanwise length and secured to a central part of said canopy wingspan being stronger than a number of said retaining devices at outer edges of said slider spanwise length and secured to wing tip portions of said canopy.

15. The ram air parachute as set forth in claim 14 , wherein each of said retaining devices includes a slider retaining element secured to said slider and a canopy retaining element secured to said canopy, said slider retaining elements and said canopy retaining elements being aligned in corresponding pairs and calibrated so that the force needed to separate the slider retaining elements from the canopy retaining elements is greater at said central part of said canopy wingspan than at said canopy wing tips.

16. The ram air parachute as set forth in claim 15 , wherein said slider retaining elements and said canopy retaining elements are mating magnetic elements.

17. The ram air parachute as set forth in claim 15 , wherein said slider retaining elements and said canopy retaining elements are mating snap fastener elements.

18. The ram air parachute as set forth in claim 15 , wherein said corresponding pairs of slider retaining elements and said canopy retaining elements are releasably secured to one another by tie elements including cable-tie type fasteners, cord or string.

19. The ram air parachute as set forth in claim 18 , wherein each of said slider retaining elements includes a slider retaining loop and each canopy retaining element includes a canopy retaining loop, a tie element being passed through the pair loops on said slider and canopy at least once and tied to join each corresponding pair.

20. The ram air parachute as set forth in claim 19 , wherein said tie elements are cords, the tie element cords of corresponding pairs at the central part of the canopy being passed through their associated loops a greater number of times than are tie element cords of corresponding pairs at said wing tips so that a tie strength at the central part of the canopy is greater than a tie strength at the wing tips.

21. A method of securing a reefing slider to a ram air parachute canopy having a wingspan and upper and lower airfoil surfaces separated by chordwise-extending ribs to form cells inflated by inflow of air at an open leading edge, and suspension lines connecting the lower surface of the canopy to a load, said reefing slider having a plurality of reinforced openings spaced from one another through which the suspension lines extend, said slider further having slider retaining elements adjacent at least some of said reinforced openings and said canopy having canopy retaining elements in spaced relationship corresponding to a spacing of said slider retaining elements, the method comprising the steps of:

aligning the canopy retaining elements with said slider retaining elements to form a plurality of retaining element pairs; and

releasably securing the slider retaining elements and the canopy retaining elements of each respective retaining element pair to one another along the wingspan of said canopy, said step of securing including securing retaining element pairs near a central area of said canopy with a mechanical connection having a first connection strength and securing retaining element pairs near the wing tips of the canopy with a mechanical connection having a second connection strength, said first connection strength being greater than said second connection strength, said releasably secured pairs of retaining elements securing said slider to said canopy to retard descent of the slider relative to the canopy from an upper reefing position in which inflation of the canopy is restricted, said slider being released from said canopy to descend along said suspension lines to a lowered position in response to release of said retaining elements from one another due to force created by said inflow of air to said cells.

22. The method as set forth in claim 21 , wherein each of said slider retaining elements includes a slider retaining loop and each canopy retaining element includes a canopy retaining loop, said step of releasably securing including passing a tie element through the canopy retaining loop and the slider retaining loop of each retaining element pair and tying the tie element, tie elements that secure retaining element pairs near a central area of said canopy being passed through the respective loop pairs more than once before tying to obtain said first connection strength, and tie elements that secure retaining element pairs near the wing tips of said canopy being passed through the respective loop pairs a fewer number of times before tying as compared with said central area pairs to obtain said second connection strength.