Inflatable structure paraglider

• US 5,244,169 A
• Filed: 05/15/1992
• Issued: 09/14/1993
• Est. Priority Date: 05/15/1992
• Status: Expired due to Fees

• Current Assignee: Vertigo, Inc. (HDT Global, Inc.)
• Original Assignee: Vertigo, Inc. (HDT Global, Inc.)
• Inventors: Haggard, Roy, Brown, Glen J.
• Primary Examiner(s): PETERS JR, JOSEPH F
• Application Number:
  US07/883,341
• Time in Patent Office: 487 Days
• Field of Search: 244/142, 244/149, 244/146, 244/900, 244/902, 244/123, 244/117 R
• US Class Current: 244/146
• CPC Class Codes: B64D 17/025 for gliding chutes

Abstract

A paraglider having ram-air inflated left and right wings and supported above a pilot by suspension lines, the wings consisting of foldable and flexible sheet material and defining front openings to receive ram-air to inflate the wings in flight, the combination comprising; fluid inflated spar tube means extending spanwise in stiffening relation to the wings, to assist in supporting and shaping the wings in flight; spar tube means extending in such proximity to the front openings as to resist tuck under and collapse of the wings, at low angles of attack; spar tube means consisting of material which is flexible and foldable when the spar tube means is not inflated.

Claims

1. In a paraglider having ram-air inflated left and right wings and supported above a pilot by suspension lines, the wings consisting of foldable and flexible sheet material and defining front openings to receive ram-air to inflate the wings in flight, the combination comprising

a) fluid inflated spar tube mean extending spanwise in stiffening relation to the wings, to assist in supporting and shaping the wings in flight,

b) said spar tube means extending in such proximity to said front openings as to resist tuck-under and collapse of the wings, at low angles of attack,

c) said spar tube means consisting of material which is flexible and foldable when the spar tube means is not inflated,

d) said spar tube means including

i) a forward spanwise extending inflated tube proximate leading edges defined by the wings, and

ii) a rearward spanwise extending tube located within the wings,

e) said wings having spanwise arching configuration, said forward and rearward spar tubes being inflated into arching configuration corresponding to said arching configuration,

f) each of said wings including

i) a top fabric panel,

ii) a bottom fabric panel,

iii) chordwise extending panels which are spaced apart spanwise of the wings, and which have upper and lower edges connected to said top and bottom panels,

iv) said forward and rearward tubes extending through said chordwise extending panels,

g) said forward and rearward spar tubes being urged toward one another by said chordwise extending panels, whereby the spacing between said forward and rearward spar tubes tapers toward tips defined by said wings,

h) and including at least one chordwise extending spar tube connected with said forward and rearward tubes, medially of their spanwise lengths.

2. The combination of claim 1 wherein said wings have leading edges above and forwardly of said front openings, and said forward spar tube extends spanwise of the wings above and forwardly of said front openings, and proximate said wing leading edges.

3. The combination of claim 1 wherein each spar tube comprises

x₁) an inner inflatable tube to contain inflating fluid pressure,

x₂) an outer protective sheath extending about said inflatable tube to be expanded into stiff form.

4. The combination of claim 3 wherein said outer protective sheath consists of synthetic yarn, which is one of the following:

braided

woven

wound.

5. The combination of claim 1 wherein there are three of said chordwise extending tubes, one medially of said forward and rearward tubes, and the other two respectively located near opposite ends of said forward and rearward tubes.

6. The combination of claim 1 including an additional tube in the form of an air pressure containing vessel extending chordwise between said forward and rearward tubes.

7. The combination of claim 6 including a pressure line extending between said additional tube and at least one of said forward and rearward tubes, and a regulator in said line.

8. The combination of claim 6 including two pressure lines extending between said additional tube and said forward and rearward tubes respectively, pressure regulator in said lines, and pressure relief valves connected with said forward and rearward tubes.

9. In a paraglider having ram-air inflated left and right wings and supported above a pilot by suspension lines, the wings consisting of foldable and flexible sheet material and defining front openings to receive ram-air to inflate the wings in flight, the combination comprising

a) fluid inflated spar tube means extending spanwise in stiffening relation to the wings, to assist in supporting and shaping the wings in flight,

b) said spar tube means extending in such proximity to said front openings as to resist tuck under and collapse of the wings, at low angles of attack,

c) said wings have arching configuration, said spar tubes means including forward and rearward spar tubes which are inflated into arching configuration corresponding to said wing arching configuration,

d) each of said wings including

i) a top fabric panel,

ii) a bottom fabric panel,

iii) chordwise extending panels which are spaced apart spanwise of the wings, and which have upper and lower edges connected to said top and bottom panels,

iv) said spar tube means extending through said chordwise extending panels.