Bias tire for aircraft

Details Bias tire for aircraft Bias tire for aircraft

1989-12-19

1992-04-21

Knable, Geoffrey L.

Resilient tires and wheels

Tires, resilient

Pneumatic tire or inner tube

152454, 152559, B60C 300, B60C 1505

Patent

active

051058650

ABSTRACT:
A bias tire for an aircraft includes a laminate formed by laminating a plurality of plies intersecting with each other and reinforced by organic fiber cords having a large thermal contraction coefficient. Both ends of the plies are turned up around bead cores. A profile curve I of a representative ply corresponding to that number counted from an innermost ply of the laminate plus one, which is one half of a total number of the plies when the tire mounted on a normal rim is filled with 1% of a normal inner pressure is constructed by a smoothly changing crown profile curve J and a smoothly changing side profile curves K. The crown profile curve J intersects a natural equilibrium profile curve H and is positioned between natural equilibrium profile curves E and H between both shoulder ends. The side profile curves K contact both the natural equilibrium profile curves E and H at rim points and smoothly connecting with the crown profile curve J and are positioned outwardly of the natural equilibrium profile curves E and H between the shoulder ends and rim points.

REFERENCES:
patent: 4349062 (1982-09-01), Tsurunaga et al.
patent: 4481994 (1984-11-01), Pommier
patent: 4513802 (1985-04-01), Togashi et al.
patent: 4867218 (1989-09-01), Asano et al.

Affiliated with

Also associated with

Rating

Bias tire for aircraft does not yet have a rating. At this time, there are no reviews or comments for this patent.

If you have personal experience with Bias tire for aircraft, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Bias tire for aircraft will most certainly appreciate the feedback.

Rate now

Comments { 0 }

Profile ID: LFUS-PAI-O-1579212