초록 ▼

An exemplary cone brake device includes a brake drum and a thermal sprayed coating deposited and bonded to the outer surface. The thermal sprayed coating is configured to engage a friction lining when one of the brake drum and the friction element is moved toward the other of the brake drum and the

An exemplary cone brake device includes a brake drum and a thermal sprayed coating deposited and bonded to the outer surface. The thermal sprayed coating is configured to engage a friction lining when one of the brake drum and the friction element is moved toward the other of the brake drum and the friction element, so as to decrease the speed of an aerospace propeller.

대표청구항 ▼

1. A cone brake device, comprising: an outer member having an annular inner surface;a friction element attached to the annular inner surface of the outer member;a brake drum having an outer surface and configured to move toward the friction element; anda thermal sprayed high velocity oxygen fuel coa

1. A cone brake device, comprising: an outer member having an annular inner surface;a friction element attached to the annular inner surface of the outer member;a brake drum having an outer surface and configured to move toward the friction element; anda thermal sprayed high velocity oxygen fuel coating including molten or semi-molten material attached to the outer surface of the brake drum and having a thickness greater than 1.5 mm, and the thermal sprayed coating is configured to engage the friction element when one of the brake drum and the friction element is moved toward the other of the brake drum and the friction element. 2. The cone brake device of claim 1, wherein the thermal sprayed coating is a tungsten carbide—17% cobalt hard material. 3. The cone brake device of claim 1, wherein the friction element is a sintered bronze material. 4. The cone brake device of claim 1, wherein the outer surface is a frustoconical surface. 5. The cone brake device of claim 1, wherein the brake drum is a ring having a first end and a second end, and the ring has an outside diameter that tapers from the first end to the second end. 6. The cone brake device of claim 1, wherein one of the outer member and the brake drum is connected to an aerospace propeller. 7. A gear box, comprising: a gear set; anda cone brake device including an outer member, a friction element, a brake drum and a thermal sprayed high velocity oxygen fuel coating including molten or semi-molten material and having a thickness greater than 1.5 mm;wherein the outer member has an annular inner surface;wherein the friction element is attached to the annular inner surface of the outer member;wherein the brake drum has an outer surface and is configured to move toward the friction element; andwherein the thermal sprayed high velocity oxygen fuel coating is attached to the outer surface of the brake drum, and the thermal sprayed coating is configured to engage the friction element when one of the brake drum and the friction element is moved toward the other of the brake drum and the friction element. 8. The gear box of claim 7, wherein the thermal sprayed coating is a tungsten carbide—17% cobalt hard material. 9. The gear box of claim 7, wherein the friction element is a sintered bronze material. 10. The gear box of claim 7, wherein the outer surface is a frustoconical surface. 11. The gear box of claim 7, wherein the brake drum is a ring having a first end and a second end, and the ring has an outside diameter that tapers from the first end to the second end. 12. The gear box of claim 7, wherein one of the outer member and the brake drum is connected to an aerospace propeller. 13. An aircraft propeller system, comprising: an aerospace propeller; anda gear box including a gear set and a cone brake device;wherein the gear set is configured to rotate the aerospace propeller;wherein the cone brake device includes an outer member, a friction element, a brake drum and a thermal sprayed high velocity oxygen fuel coating including molten or semi-molten material and having a thickness greater than 1.5 mm;wherein the outer member has an annular inner surface;wherein the friction element is attached to the annular inner surface of the outer member;wherein the brake drum has an outer surface and is configured to move toward the friction element; andwherein the thermal sprayed high velocity oxygen fuel coating is attached to the outer surface of the brake drum, and the thermal sprayed coating is configured to engage the friction element when one of the brake drum and the friction element is moved toward the other of the brake drum and the friction element, so as to decrease a speed of the aerospace propeller. 14. The aircraft propeller system of claim 13, wherein the thermal sprayed coating is a tungsten carbide—17% cobalt hard material. 15. The aircraft propeller system of claim 13, wherein the friction element is a sintered bronze material. 16. The aircraft propeller system of claim 13, wherein the outer surface is a frustoconical surface. 17. The aircraft propeller system of claim 13, wherein the brake drum is a ring having a first end and a second end, and the ring has an outside diameter that tapers from the first end to the second end.