Thermal restraint system for a circular heat exchanger

Claim 2

A heat exchanger including a core having a plurality of heat recipient passages and a plurality of heat donor passages therein, comprising: said core including a plurality of cells each defining one of the passages therein, the cells being secured together forming a generally circular core, adjacent cells forming the other of the passages and the core further including an inner portion and an outer portion; each of said heat donor passages having a donor fluid therein during operation and each of said heat recipient passages having a recipient fluid therein during operation, said donor fluid exerting a first working pressure and force and said recipient fluid exerting a second working pressure and force in the passages when in operation, said working pressures and forces attempting to separate the passages; and means for resisting the forces attempting to separate the passages, at least a portion of said means being positioned externally around the outer portion of the core and the entire means being totally in heat transferring relationship with the donor fluid.

Claim 3

The heat exchanger of claim 1 wherein said means for resisting includes one tension ring being positioned around the outer portion of the core and in contact therewith.

Claim 4

The heat exchanger of claim 2 wherein said core has a preestablished rate of thermal expansion and said tension rings each have a rate of thermal expansion which closely matches the rate of thermal expansion of the core.

Claim 5

The heat exchanger of claim 3 wherein each of said tension rings is permanently attached in a continuous ring configuration.

Claim 6

The heat exchanger of claim 3 wherein each of said tension rings is removably attached in a continuous ring configuration.

Claim 7

The heat exchanger of claim 1 wherein said means for resisting includes a plurality of evenly spaced individual tension rings positioned around the outer portion of the core and in contact therewith.

Claim 8

The heat exchanger of claim 6 wherein said core has a preestablished rate of expansion and said individual tension rings have a rate of thermal expansion which closely matches the rate of thermal expansion of the core.

Claim 9

The heat exchanger of claim 6 wherein each of said individual tension rings has a constant cross-sectional area along the entire length of the ring and the cross-sectional area of each individual tension ring is equal to each other.

Claim 10

The heat exchanger of claim 8 wherein said cross-sectional area is circular and has a predetermined thickness.

Claim 11

The heat exchanger of claim 9 wherein said individual tension rings are made from Inconel 718 steel.

Claim 12

The heat exchanger of claim 10 wherein said predetermined thickness of each ring is about 6 millimeters.

Claim 13

The heat exchanger of claim 1 wherein said means for resisting includes a compressive hoop positioned at the inner portion of the core.

Claim 14

The heat exchanger of claim 12 wherein said compressive hoop is formed by each of the cells being in contacting relationship to each other at the inner portion of the core.

Claim 15

The heat exchanger of claim 12 wherein said compressive hoop further includes one weld radially connecting each of the cells at the inner portion of the core.

Claim 16

A gas turbine engine including an exhaust system having a donor fluid therein, an air intake system having a recipient fluid therein, a heat exchanger including a core having a heat recipient passage and a heat donor passage therein, a housing surrounding the core, said exhaust system being connected to the heat donor passage and said air intake system being connected to the heat recovery passage, comprising: said core including a plurality of stacked cells each defining one of the passages therein, the cells being secured together, forming a generally circular core and being centered about an axis, adjacent cells forming the other of the passages therebetween and said core further including an outer portion and an inner portion; said donor fluid in each of said heat donor passages during the operation of the engine exerting a first working pressure and force within the passage resulting in a force attempting to separate the passages; said recipient fluid in each of said heat recipient passages during operation of the engine exerting a second working pressure and force within the passages resulting in a force attempting to separate the passages; and means for resisting the forces attempting to separate the passages, at least a portion of said means being positioned externally around the outer portion of the core and the entire means being totally in heat transferring relationship with the donor fluid.

Claim 17

A gas turbine engine including an exhaust system having a donor fluid therein, an air intake system having a recipient fluid therein, a heat exchanger including a core having a heat recipient passage and a heat donor passage therein, a housing surrounding the core, said exhaust system being connected to the heat donor passage and said air intake system being connected to the heat recovery passage, comprising: said core including a plurality of stacked cells each defining one of the passages therein, the cells being secured together, forming a generally circular core and being centered about an axis, adjacent cells forming the other of the passages therebetween and said core further including an outer portion and an inner portion; said donor fluid in each of said heat donor passages during the operation of the engine exerting a first working pressure and force within the passage resulting in a force attempting to separate the passages; said recipient fluid in each of said heat recipient passages during operation of the engine exerting a second working pressure and force within the passages resulting in a force attempting to separate the passages; and means for resisting the forces attempting to separate the passages, at least a portion of said means being positioned externally around the outer portion of the core and the entire means being totally in heat transferring relationship with the donor fluid.

Claim 18

The heat exchanger of claim 15 wherein said means for resisting includes tension ring being positioned around the outer portion of the core and in contact therewith.

Claim 19

The heat exchanger of claim 16 wherein said core has a preestablished rate of expansion and the tension rings each have a rate of thermal expansion which closely matches the rate of thermal expansion of the core.

Claim 20

The heat exchanger of claim 17 wherein each of said tension rings is permanently attached in a continuous ring configuration.

Claim 21

The heat exchanger of claim 17 wherein each of said tension rings is removably attached in a continuous ring configuration.

Claim 22

The heat exchanger of claim 15 wherein said means for resisting includes a plurality of evenly spaced individual tension rings positioned around the outer portion of the core and in contact therewith.

Claim 23

The heat exchanger of claim 20 wherein said core has a preestablished rate of expansion and the individual tension rings each have a rate of thermal expansion which closely matches the rate of thermal expansion of the core.

Claim 24

The heat exchanger of claim 21 wherein each of said individual tension rings has a constant cross-sectional area along the entire length of the ring and the cross-sectional area of each individual tension ring is equal to each other.

Claim 25

The heat exchanger of claim 22 wherein said cross-sectional area is circular and has a predetermined thickness.

Claim 26

The heat exchanger of claim 21 wherein said individual tension rings are made from Inconel 718 steel.

Claim 27

The heat exchanger of claim 23 wherein said predetermined thickness of each ring is about 6 millimeters.

Claim 28

The heat exchanger of claim 15 wherein said means for resisting includes a compressive hoop positioned at the inner portion of the core.

Claim 29

The heat exchanger of claim 26 wherein said compressive hoop is formed by the cells being in force transferring relationship to each other at the inner portion of the core.

Claim 30

The heat exchanger of claim 26 wherein said compressive hoop further includes one weld radially connecting each of the cells at the inner portion of the core.

Claim 31

A heat exchanger, comprising: a core being made of many pieces and having a plurality of first and second passages adapted to receive fluids of different temperatures, said core further having a generally circular configuration and including an outer portion, said fluids exerting different pressures on said heat exchanger pieces; and means for expanding and contracting in response to the temperature of only one of the fluids, and maintaining a preestablished force on said heat exchanger pieces, and means for expanding and contraction including at least a portion of said means being positioned externally around the outer portion of the core and the entire means being totally in heat transferring relationship with one of the fluids.

Claim 32

A heat exchanger, comprising: a core being made of many pieces and having a plurality of first and second passages adapted to receive fluids of different temperatures, said core further having a generally circular configuration and including an outer portion, said fluids exerting different pressures on said heat exchanger pieces; and means for expanding and contracting in response to the temperature of only one of the fluids, and maintaining a preestablished force on said heat exchanger pieces, and means for expanding and contraction including at least a portion of said means being positioned externally around the outer portion of the core and the entire means being totally in heat transferring relationship with one of the fluids.

Claim 33

The heat exchanger of claim 29 wherein said preestablished force has a range of between about 1500 N and 19,000 N.

Claim 34

The heat exchanger of claim 29 wherein said core includes an inner portion.

Claim 35

The heat exchanger of claim 31 wherein said means for expanding and contracting includes one tension ring being positioned around the outer portion of the core and in contact therewith.

Claim 36

The heat exchanger of claim 32 wherein said core has a preestablished rate of thermal expansion and the one tension ring has a rate of thermal expansion which closely matches the rate of thermal expansion of the core.

Claim 37

The heat exchanger of claim 32 wherein each of said tension rings is permanently attached in a continuous ring configuration.

Claim 38

The heat exchanger of claim 32 wherein each of said tension rings is removably attached in a continuous ring configuration.

Claim 39

The heat exchanger of claim 29 wherein said means for expanding and contracting includes a plurality of evenly spaced individual tension rings positioned around the outer portion of the core and in contact therewith.

Claim 40

The heat exchanger of claim 36 wherein said core has a preestablished rate of expansion and said individual tension rings have a rate of thermal expansion which closely matches the rate of thermal expansion of the core.

Claim 41

The heat exchanger of claim 37 wherein each of said individual tension rings has a constant cross-sectional area along the entire length of the ring, and the cross-sectional area of each individual tension ring is equal to each other.

Claim 42

The heat exchanger of claim 38 wherein said cross-sectional area is circular and has a predetermined thickness.

Claim 43

The heat exchanger of claim 39 wherein said individual tension rings are made from Inconel 718 steel.

Claim 44

The heat exchanger of claim 39 wherein said predetermined thickness of each ring is about 6 millimeters.