초록 ▼

A piston assembly for use in a brake assembly has a piston sleeve having a first end, a second end, an external radius, an internal radius, and a cap on the piston sleeve second end. The cap has a first end, a middle portion, and a second end. The cap first end has an external radius and the cap sec

A piston assembly for use in a brake assembly has a piston sleeve having a first end, a second end, an external radius, an internal radius, and a cap on the piston sleeve second end. The cap has a first end, a middle portion, and a second end. The cap first end has an external radius and the cap second end has an external radius, wherein the cap first end external radius is smaller than the cap second end external radius. The middle portion is stepped to transition from the cap first end external radius to the cap second end external radius. The cap first end external radius is such that the cap first end slides into the piston sleeve. The cap middle portion has a conical mating surface, and the piston sleeve second end has a corresponding conical mating surface. Further, the cap second end external radius is larger than the piston sleeve external radius.

대표청구항 ▼

I claim: 1. In a piston assembly for use in a brake assembly having a brake stack wherein the piston assembly has a one piece piston sleeve having a first end, a second end, an external radius, and an internal radius, and a one piece cap on said piston sleeve second end, the improvement comprising;

I claim: 1. In a piston assembly for use in a brake assembly having a brake stack wherein the piston assembly has a one piece piston sleeve having a first end, a second end, an external radius, and an internal radius, and a one piece cap on said piston sleeve second end, the improvement comprising; said cap having a first end, a middle portion and a second end, wherein said cap first end has an external radius and said cap second end has an external radius, and wherein said cap first end external radius is smaller than said cap second end external radius, and wherein the middle portion is stepped to transition from the cap first end external radius to the cap second end external radius, wherein said cap first end external radius is such that said cap first end slides into said piston sleeve, and wherein said cap middle portion has a conical mating surface, hereinafter referred to as the cap conical mating surface, for mating with said piston sleeve second end, and wherein said piston sleeve second end has a corresponding conical mating surface, hereinafter referred to as the piston sleeve conical mating surface, for mating with said cap conical mating surface, wherein said cap conical mating surface and said piston sleeve conical mating surface each have a frustoconical shape which opens away from the brake stack, and wherein said cap second end external radius is larger than said piston sleeve external radius, and wherein said cap second end further comprises a disc portion, operative to engage the brake stack. 2. The piston assembly for use in a brake assembly of claim 1 wherein said cap is a heat insulator. 3. The piston assembly for use In a brake assembly of claim 2 wherein the heat insulator is a stainless steel. 4. The piston assembly for use in a brake assembly of claim 2 wherein the heat insulator is a 304L or 316L stainless steel. 5. The piston assembly for use in a brake assembly of claim 1 wherein said cap conical mating surface and/or said piston sleeve conical mating surface have a dry film lubricant thereon. 6. The piston assembly for use in a brake assembly of claim 5 wherein said dry film lubricant is a tungsten disulfide coating. 7. The piston assembly for use in a brake assembly of claim 1 wherein said cap conical mating surface and said corresponding piston sleeve conical mating surface are each a 15 degree taper. 8. The piston assembly for use in a brake assembly of claim 1 wherein there is a radial clearance between said piston sleeve internal radius and said cap first end external radius. 9. The piston assembly for use in a brake assembly of claim 8 wherein said radial clearance between said piston sleeve internal radius and said cap first end external radius is approximately 0.025 inches. 10. In an aircraft disc brake assembly having an axle means, a piston support member mounted on the axle means, wherein said piston support member has a radially extending flange portion, an inner rim portion, and a plurality of circumferentially spaced cylinders or cylinder housings, wherein said radially extending flange portion is secured to a stationary torque tube hub means of a stationary torque tube; wherein said torque tube has a plurality of axially extending ribs, a plurality of stator discs with circumferentially spaced slots engaging said ribs for axial movement of said stator discs, wherein there is an end stator disc called a pressure plate; interspaced between said stator discs are rotor discs, said rotor discs interleaved between said stator discs define a brake stack, each said circumferentially spaced cylinder has a piston cylinder with an elongated one piece piston sleeve slidably mounted therein, wherein said piston sleeve has a first end and a second end, an external radius and an internal radius, said first end of said piston sleeve has an end wall that is cooperative with said cylinder to define a piston chamber which is selectively pressurized, the improvement comprising; wherein said second end of said piston sleeve has a one piece cap having a first end, a middle portion and a second end, wherein said cap first end has an external radius and said cap second end has an external radius, wherein said cap first end external radius is smaller than said cap second end external radius, and wherein the middle portion is stepped to transition from the cap first end external radius to the cap second end external radius, wherein said cap first end external radius is such that said cap first end slides into said piston sleeve, and wherein said cap middle portion has a conical mating surface, hereinafter referred to as the cap conical mating surface, for mating with said piston sleeve second end and wherein said piston sleeve second end has a corresponding conical mating surface, hereinafter referred to as the piston sleeve conical mating surface, for mating with said cap conical mating surface, and wherein said cap second end external radius is larger than said piston sleeve external radius, further, wherein said cap second end has a disc portion operative to engage said brake stack. 11. The aircraft disc brake assembly of claim 10 wherein said cap is a heat insulator. 12. The aircraft disc brake assembly of claim 11 wherein the heat insulator is a stainless steel. 13. The aircraft disc brake assembly of claim 11 wherein the heat insulator is a 304L or 316L stainless steel. 14. The aircraft disc brake assembly of claim 10 wherein said cap conical mating surface and/or said piston sleeve conical mating surface have a dry film lubricant thereon. 15. The aircraft disc brake assembly of claim 14 wherein said dry film lubricant is a tungsten disulfide coating. 16. The aircraft disc brake assembly of claim 10 wherein said cap conical mating surface and said corresponding piston sleeve conical mating surface are each a 15 degree taper. 17. The aircraft disc brake assembly of claim 10 wherein there is a radial clearance between said piston sleeve internal radius and said cap first end external radius. 18. The aircraft disc brake assembly of claim 17 wherein said radial clearance between said piston sleeve internal radius and said cap first end external radius is approximately 0.025 inches.