Harness assembly for aircraft pilot crew mask

1. An aircraft inflatable harness assembly for an aircraft oxygen crew mask operating between 50 and 125 psi for providing regulated flow of oxygen on board an aircraft for an aircraft crew, comprising:

at least one inner inflatable tube having a normally deflated configuration and an inflated configuration, said at least one inner inflatable tube having a first end and a second end, said at least one inner inflatable tube being configured to be inflated to cause expansion of the harness assembly to allow the harness assembly to be placed over a user's head, the at least one inner inflatable tube having an internal diameter greater than or equal to 0.250 inches and less than or equal to 0.375 inches and a wall thickness greater than or equal to 0.0625 inches and less than or equal to 0.095 inches, said at least one inner inflatable tube including a braided outer sleeve of elastic material, the outer sleeve made of polyethylene terephthalate, wherein the inner inflatable tube includes a silicone tube;

wherein said outer sleeve of elastic material is configured to have a first length when said at least one inner inflatable tube is in the normally deflated configuration, and wherein said outer sleeve of elastic material is configured to longitudinally expand to a second length greater than the first length when said at least one inner inflatable tube is in the inflated configuration, wherein the first length is greater than or equal to a third length of the at least one inner inflatable tube in the normally deflated configuration, the outer sleeve having a longitudinal stretch ratio of two to one or less;

wherein inflation of said at least one inner inflatable tube causes said outer sleeve of elastic material to expand in a longitudinal direction to the second length to allow the aircraft inflatable harness assembly to be placed over the user's head, and wherein deflation of said at least one inner inflatable tube causes said outer sleeve of elastic material to retract in a reverse longitudinal direction back to the first length to allow the aircraft inflatable harness assembly to grip the user's head with a desired head tension.

2. The aircraft inflatable harness assembly of claim 1 , wherein the at least one inner inflatable tube is a continuous inner inflatable tube.

3. The aircraft inflatable harness assembly of claim 1 , further comprising at least one mask attachment fitting having a barbed end secured to the first end of said at least one inner inflatable tube, said mask attachment fitting being configured to be connected to a crew mask for control of inflation and deflation of said at least one inner inflatable tube.

4. The aircraft inflatable harness assembly of claim 3 , wherein the at least one mask attachment fitting is secured to the first end of the inner inflatable tube by a crimped ferrule.

5. The aircraft inflatable harness assembly of claim 1 , further comprising a mask attachment tube secured to the second end of said at least one inner inflatable tube.

6. The aircraft inflatable harness assembly of claim 5 , wherein the mask attachment tube is secured to the second end of the inner inflatable tube by a crimped ferrule.

7. The aircraft inflatable harness assembly of claim 1 , wherein the at least one inner inflatable tube comprises a plurality of inner inflatable tubes.

8. The aircraft inflatable harness assembly of claim 7 , further comprising an elastic head strap for adjustment of positioning of the harness assembly on the user's head.

9. The aircraft inflatable harness assembly of claim 7 , further comprising a back pad connected between said plurality of inner inflatable tubes to form a contour of the harness assembly for positioning of the harness assembly on the user's head.

10. The aircraft inflatable harness assembly of claim 1 , wherein the second length of the outer sleeve of elastic material in the inflated configuration is at most twice the first length of the outer sleeve of elastic material in the deflated configuration.

11. The aircraft inflatable harness assembly of claim 1 , wherein the outer sleeve has the longitudinal stretch ratio of two to one or less when between 50 psi and 125 psi of air pressure is applied to the outer sleeve.

12. An aircraft inflatable harness assembly for an aircraft oxygen crew mask operating between 50 and 125 psi for providing regulated flow of oxygen on board an aircraft for an aircraft crew, comprising:

a plurality of inner inflatable tubes having a normally deflated configuration and an inflated configuration, said plurality of inner inflatable tubes each having a first end and a second end, said plurality of inner inflatable tubes being configured to be inflated to cause expansion of the harness assembly to allow the harness assembly to be placed over a user's head, at least one of the inner inflatable tubes having an internal diameter greater than or equal to 0.250 inches and less than or equal to 0.375 inches and a wall thickness greater than or equal to 0.0625 inches and less than or equal to 0.095 inches, said plurality of inner inflatable tubes including a braided outer sleeve of elastic material, the outer sleeve made of polyethylene terephthalate, wherein each of the plurality of inner inflatable tubes includes a silicone tube;

at least one mask attachment fitting having a barbed end secured to the first ends of said plurality of inner inflatable tubes, said mask attachment fitting being configured to be connected to a crew mask for control of inflation and deflation of said plurality of inner inflatable tubes; a mask attachment tube secured to the second ends of said plurality of inner inflatable tubes; an elastic head strap for adjustment of positioning of the harness assembly on the user's head;

a back pad connected between said plurality of inner inflatable tubes to form a contour of the harness assembly for positioning of the harness assembly on the user's head;

wherein said outer sleeve of elastic material is configured to have a first length when said plurality of inner inflatable tubes is in the normally deflated configuration, wherein said outer sleeve of elastic material is configured to longitudinally expand to a second length greater than the first length when said plurality of inner inflatable tubes is in the inflated configuration, wherein the first length is greater than or equal to a third length of each of the plurality of inner inflatable tubes in the normally deflated configuration, the outer sleeve having a longitudinal stretch ratio of two to one or less;

wherein inflation of said plurality of inner inflatable tubes causes said outer sleeve of elastic material to expand in a longitudinal direction to the second length to allow the aircraft inflatable harness assembly to be placed over the user's head; and wherein deflation of said plurality of inner inflatable tubes causes said outer sleeve of elastic material to retract in a reverse longitudinal direction back to the first length to allow the aircraft inflatable harness assembly to grip the user's head with a desired head tension.

13. The aircraft inflatable harness assembly of claim 12 , wherein the plurality of inner inflatable tubes are continuous inner inflatable tubes.

14. The aircraft inflatable harness assembly of claim 12 , wherein the second length of the outer sleeve of elastic material in the inflated configuration is at most twice the first length of the outer sleeve of elastic material in the deflated configuration.