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The present application thus provides a retractable seal system for use between a high pressure side and a low pressure side of a turbine engine. The retractable seal system may include a seal positioned in a slot of a stationary component, a pressure balance pocket positioned about the seal, and a

The present application thus provides a retractable seal system for use between a high pressure side and a low pressure side of a turbine engine. The retractable seal system may include a seal positioned in a slot of a stationary component, a pressure balance pocket positioned about the seal, and a conduit in communication with the pressure balance pocket and the high pressure side.

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1. A retractable seal system for use between a high pressure side and a low pressure side of a turbine engine, comprising: a seal positioned in a slot of a stationary component, wherein the seal comprises a neck positioned between a pair of hooks of the slot of the stationary component, an upper fla

1. A retractable seal system for use between a high pressure side and a low pressure side of a turbine engine, comprising: a seal positioned in a slot of a stationary component, wherein the seal comprises a neck positioned between a pair of hooks of the slot of the stationary component, an upper flange positioned on the pair of hooks within a groove of the stationary component, wherein the pair of hooks are formed by the groove, and one or more springs positioned about the stationary component and positioned in between the flange and the pair of hooks;a pressure balance pocket positioned about the seal, wherein the pressure balance pocket is positioned within the neck; anda conduit in communication with the pressure balance pocket and the high pressure side. 2. The retractable seal system of claim 1, wherein the seal faces a rotating component. 3. The retractable seal system of claim 1, wherein the seal comprises a brush seal. 4. The retractable seal system of claim 3, wherein the brush seal comprises a plurality of bristles. 5. The retractable seal system of claim 1, wherein the pressure balance pocket is positioned within one of the pair of hooks. 6. The retractable seal system of claim 1, wherein the conduit comprises a flange conduit through a flange of the seal. 7. The retractable seal system of claim 1, wherein the conduit comprises a flange groove along a flange of the seal. 8. The retractable seal system of claim 1, wherein the conduit comprises a hook grove along a hook of the stationary component. 9. The retractable seal system of claim 1, wherein the seal comprises a labyrinth seal. 10. The retractable seal system of claim 9, wherein the labyrinth seal comprises one or more labyrinth teeth. 11. A retractable seal system for use between a high pressure side and a low pressure side of a turbine engine, comprising: a brush seal positioned in a slot of a stationary component;wherein the brush seal comprises a neck positioned about a pair of hooks of the slot of the stationary component, an upper flange positioned on the pair of hooks within a groove of the stationary component, wherein the pair of hooks are formed by the groove, and one or more springs positioned about the stationary component and positioned in between the flange and the pair of hooks;a pressure balance pocket positioned about the neck and one of the pair of hooks; anda conduit in communication with the pressure balance pocket and the high pressure side,wherein the pressure balance pocket is positioned within the neck and in communication with the high pressure side via the conduit. 12. The retractable seal system of claim 11, wherein the brush seal comprises a plurality of bristles facing a rotating component.