Self-locking threaded fastener

Claim 2

A temperature responsive self-locking fastener for use in a gas turbine engine whose operating temperature is different than its installation temperature comprising; a threaded shank having a first coefficient of thermal expansion, TC1, and an opening for receiving a locking member; a threaded mating element for receiving said shank and having a second coefficient of thermal expansion, TC2, that is approximately equal to said first coefficient of thermal expansion; a temperature responsive locking member disposed in said shank opening and having a third coefficient of thermal expansion, TC3, wherein TC3 is not equal to either said first or said second coefficient of thermal expansion; wherein at said installation temperature, said locking member is unlocked, thereby minimizing wear and tear on said locking member during installation or removal, and at said operating temperature said locking member prevents disengagement of said threaded shank and said mating element.

Claim 3

A temperature responsive self-locking fastener as described in claim 1 wherein said threaded shank is disposed along an axis and having a first cross-sectional area, a first and a second end and a head with a second cross-sectional area that is perpendicular to said axis and integrally attached to said first end, wherein said second cross-sectional area is larger than said first cross-sectional area.

Claim 4

A temperature responsive self-locking fastener as described in claim 1 wherein said threaded shank is axially divided into an unthreaded upper half and a threaded lower half and said locking member is axially located along said unthreaded upper half.

Claim 5

A temperature responsive self-locking fastener, as described in claim 1, including a plurality of locking members, each having a different coefficient of thermal expansion.

Claim 6

A temperature responsive self-locking fastener as described in claim 1, wherein said threaded shank has a diameter, D, and said locking member has a diameter or thickness, X, wherein the ratio of X to D is less than 0.5.

Claim 7

A temperature responsive self-locking fastener as described in claim 1, wherein said first, said second and said third coefficients of thermal expansion are between 2.0×10**-6/°F. and 30.0×10**-6/°F.

Claim 8

A temperature responsive self-locking fastener as described in claim 1, wherein said difference between said first or said second coefficient of thermal expansion and said third coefficient of thermal expansion is larger than 3.0×10**-6/°F.

Claim 9

A temperature responsive self-locking fastener as described in claim 1, wherein said locking member and said mating element form removable engagement at a temperature below 110° F. and form locked, substantially vibration resistant engagement, at a temperature above 160° F.

Claim 10

A temperature responsive self-locking fastener as described in claim 1, wherein said locking member and said mating element form removable engagement at a temperature above 30° F. and form locked, substantially vibration resistant engagement, at a temperature below 10° F.

Claim 11

A temperature responsive self-locking fastener as described in claim 1, wherein said locking member develops a locking force between said locking member and said mating element that exceeds 50 pounds.

Claim 12

A temperature responsive self-locking fastener as described in claim 10 wherein said locking force is developed by friction between said locking member and said mating element.

Claim 13

A temperature responsive self-locking fastener for use in a gas turbine engine whose operating temperature is different than its installation temperature comprising: a) a threaded shank having a first coefficient of thermal expansion, TC1, and an opening for receiving a locking member; b) a threaded mating element for receiving said shank, having a second coefficient of thermal expansion, TC2, that is approximately equal to said first coefficient of thermal expansion and having a notch or a hole; and c) a temperature responsive locking member disposed in said shank opening and having a third coefficient of thermal expansion, TC3, wherein TC3 is not equal to either said first or said second coefficient of thermal expansion wherein said locking member engages said notch or said hole when said self-locking fastener is at said operating temperature.

Claim 14

A temperature responsive self-locking fastener for use in a gas turbine engine whose operating temperature is different than its installation temperature comprising: a) a threaded shank having a first coefficient of thermal expansion, TC1, and an opening for receiving a locking member; b) a threaded mating element for receiving said shank, having a second coefficient of thermal expansion, TC2, that is approximately equal to said first coefficient of thermal expansion and having a notch or a hole; and c) a temperature responsive locking member disposed in said shank opening and having a third coefficient of thermal expansion, TC3, wherein TC3 is not equal to either said first or said second coefficient of thermal expansion wherein said locking member engages said notch or said hole when said self-locking fastener is at said operating temperature.

Claim 15

A temperature responsive self-locking fastener as described in claim 12, wherein said engagement prevents rotational movement of said threaded shank relative to said mating element.

Claim 16

A temperature responsive self-locking fastener as described in claim 12, wherein said engagement prevents axial movement of said threaded shank relative to said mating element.

Claim 17

A temperature responsive self-locking fastener as described in claim 12, wherein said engagement prevents axial and rotational movement of said threaded shank relative to said mating element.

Claim 18

A temperature responsive self-locking fastener as described in claim 12, wherein said threaded shank includes a plurality of openings each for receiving a locking member; wherein said threaded mating element includes a plurality of notches or holes; and a plurality of temperature responsive locking members each having a coefficient of thermal expansion different from each other and different from TC1 and TC2 and being disposed in said plurality of shank openings wherein at least one of said temperature responsive locking members engages one of said notches or said holes when said self-locking fastener is at said operating temperature.

Claim 19

A temperature responsive self-locking fastener as described in claim 1, wherein said locking member is situated in an axially located and circumferentially disposed groove.

Claim 20

A temperature responsive self-locking fastener as described in claim 1, wherein said locking member is axially located and circumferentially disposed in a groove around said threaded shank.

Claim 21

A temperature responsive self-locking fastener as described in claim 1, wherein said locking member is axially located and circumferentially disposed in a groove that is less than 360° around said threaded shank.

Claim 22

A temperature responsive self-locking fastener as described in claim 1, wherein said locking member is situated in an axially located and radially disposed hole in said threaded shank.

Claim 23

A temperature responsive self-locking fastener as described in claim 1, wherein said locking member is bimetallic.

Claim 24

A temperature responsive self-locking fastener as described in claim 1, wherein the material for said locking member is metallic.

Claim 25

A temperature responsive self-locking fastener as described in claim 1, wherein the material for said threaded shank and said mating element is metallic.

Claim 26

A temperature responsive self-locking fastener as described in claim 1, including means for coupling said threaded shank and said locking member.

Claim 27

A temperature responsive self-locking fastener for use in a gas turbine engine whose operating temperature is different than its installation temperature comprising: a threaded shank having a first coefficient of thermal expansion, TC1, and an axially located and radially disposed hole; a threaded mating element for receiving said shank and having a second coefficient of thermal expansion, TC2, that is approximately equal to said first coefficient of thermal expansion; a temperature responsive locking member disposed in said shank hole and having a set of threads that, at an installation temperature, are continuous with said threads formed on said shank and, at an operating temperature, said locking member expands relative to said threaded shank and said mating element and develops a frictional force between said locking member and said mating element, thereby preventing disengagement of said threaded shank and said mating element; wherein at said installation temperature, said locking member is unlocked thereby minimizing wear and tear on said locking member and thereby maximizing the number of installation and removal cycles of said self-locking fastener.

Claim 28

A temperature responsive self-locking fastener for use in a gas turbine engine whose operating temperature is different than its installation temperature comprising: a threaded shank having a first coefficient of thermal expansion, TC1, and an axially located and radially disposed hole; a threaded mating element for receiving said shank and having a second coefficient of thermal expansion, TC2, that is approximately equal to said first coefficient of thermal expansion; a temperature responsive locking member disposed in said shank hole and having a set of threads that, at an installation temperature, are continuous with said threads formed on said shank and, at an operating temperature, said locking member expands relative to said threaded shank and said mating element and develops a frictional force between said locking member and said mating element, thereby preventing disengagement of said threaded shank and said mating element; wherein at said installation temperature, said locking member is unlocked thereby minimizing wear and tear on said locking member and thereby maximizing the number of installation and removal cycles of said self-locking fastener.

Claim 29

A temperature responsive self-locking fastener as described in claim 25 including a plurality of locking members, each having a different coefficient of thermal expansion.

Claim 30

A temperature responsive self-locking fastener for use in a gas turbine engine whose operating temperature is different from its installation temperature comprising: a) a threaded shank having a first coefficient of thermal expansion, TC1, and a plurality of axially located and radially disposed holes; b) a threaded mating element for receiving said shank, having a second coefficient of thermal expansion, TC2, that is approximately equal to said first coefficient of thermal expansion; and c) a plurality of temperature responsive locking members each having a coefficient of thermal expansion that is different from each other and different from TC1 and TC2 and being disposed in said plurality of shank holes and each having a set of threads that, at an installation temperature, are continuous with said threads formed on said shank and, at an operating temperature, at least one of said locking members expands relative to said threaded shank and said mating element and develops a frictional force between said locking member and said mating element, thereby preventing disengagement of said threaded shank and said mating element.

Claim 31

A temperature responsive self-locking fastener for use in a gas turbine engine whose operating temperature is different from its installation temperature comprising: a) a threaded shank having a first coefficient of thermal expansion, TC1, and a plurality of axially located and radially disposed holes; b) a threaded mating element for receiving said shank, having a second coefficient of thermal expansion, TC2, that is approximately equal to said first coefficient of thermal expansion; and c) a plurality of temperature responsive locking members each having a coefficient of thermal expansion that is different from each other and different from TC1 and TC2 and being disposed in said plurality of shank holes and each having a set of threads that, at an installation temperature, are continuous with said threads formed on said shank and, at an operating temperature, at least one of said locking members expands relative to said threaded shank and said mating element and develops a frictional force between said locking member and said mating element, thereby preventing disengagement of said threaded shank and said mating element.