Cooling system for tail cone mounted generator
US-11821370-B2 · Nov 21, 2023 · US
US12372010B1 · US · B1
| Field | Value |
|---|---|
| Publication number | US-12372010-B1 |
| Application number | US-202418423446-A |
| Country | US |
| Kind code | B1 |
| Filing date | Jan 26, 2024 |
| Priority date | Jan 26, 2024 |
| Publication date | Jul 29, 2025 |
| Grant date | Jul 29, 2025 |
A practical reading order for non-experts. Skip the full description unless you need deep technical detail.
What the patent document calls the invention.
A short plain-language summary of the technical disclosure.
Who owns or filed the patent and who is credited as inventor.
Filing, priority, publication, and grant dates set the timeline.
The legal scope of protection — read this for what is actually claimed.
Technology tags used to group this patent with similar filings.
Prior art links and similar publications in this corpus.
Official abstract text for this publication.
A tail cone ventilation system including a tail cone case defining a tail cone interior and a tail cone exterior, the tail cone having a forward portion and an aft portion separated axially along a tail cone axis; a distribution manifold located within the tail cone interior proximate the forward portion, wherein the distribution manifold comprises nozzles arranged radially around the axis, the nozzles configured to direct a cooling air over at least one electronic component within the tail cone interior and along an inner surface of the tail cone case; an air inlet fluidly coupled with the distribution manifold through ducting, the air inlet located externally from the tail cone interior; and a tail cone discharge located proximate the tail cone aft portion, the tail cone discharge being fluidly coupled with the distribution manifold.
Opening claim text (preview).
What is claimed is: 1. A tail cone ventilation system comprising: a tail cone case defining a tail cone interior and a tail cone exterior, the tail cone having a forward portion and an aft portion separated axially along a tail cone axis; a distribution manifold located within the tail cone interior proximate the forward portion, wherein the distribution manifold comprises nozzles arranged radially around the axis, the nozzles configured to direct a cooling air over at least one electronic component within the tail cone interior and along an inner surface of the tail cone case; an air inlet fluidly coupled with the distribution manifold through ducting, the air inlet located externally from the tail cone interior; and a tail cone discharge located proximate the tail cone aft portion, the tail cone discharge being fluidly coupled with the distribution manifold. 2. The tail cone ventilation system according to claim 1 , wherein the distribution manifold comprises a circular torus located concentric around the tail cone axis. 3. The tail cone ventilation system according to claim 1 , wherein the distribution manifold comprises more than one torus of varying circumferences, located at various distances from the tail cone forward portion along the tail cone axis. 4. The tail cone ventilation system according to claim 1 , wherein the air inlet comprises an air scoop design configured to receive air flowing past an outer surface. 5. The tail cone ventilation system according to claim 1 , further comprising: a conduit attached to the tail cone case at the tail cone exterior and to a pylon at an opposite end, the conduit comprising a cable chase having cable, the cable being in operative communication with the at least one electronic component within the tail cone interior, the cable chase being isolated from the tail cone interior by a firewall, a cooling supply fluidly coupled with the cable chase, the cooling supply configured to cool the cable within the cable chase. 6. The tail cone ventilation system according to claim 5 , further comprising: a pylon air scoop fluidly coupled to the cable chase, wherein the pylon air scoop is configured to direct the cooling air to the cable chase through internal flow passages. 7. The tail cone ventilation system according to claim 1 , wherein the nozzles are configured to direct the cooling air along an inner surface of the tail cone case forming a cooling film layer. 8. A tail cone ventilation system comprising: a gas turbine engine aft portion; a tail cone case attached to the gas turbine aft portion; the tail cone case defining a tail cone interior and a tail cone exterior, the tail cone having a forward portion and an aft portion separated axially along a tail cone axis; a distribution manifold located within the tail cone interior proximate the forward portion, wherein the distribution manifold comprises nozzles arranged radially around the axis, the nozzles configured to direct a cooling air over at least one electronic component and along an inner surface of the tail cone case; an air inlet fluidly coupled with the distribution manifold through ducting, the air inlet located externally from the tail cone interior; and a tail cone discharge located proximate the tail cone aft portion, the tail cone discharge being fluidly coupled with the distribution manifold. 9. The tail cone ventilation system according to claim 8 , further comprising: insulation attached to the tail cone case between the tail cone interior and the tail cone exterior. 10. The tail cone ventilation system according to claim 8 , wherein the distribution manifold comprises a circular torus located concentric around the tail cone axis. 11. The tail cone ventilation system according to claim 8 , wherein the distribution manifold comprises more than one torus of varying circumferences, located at various distances from the tail cone forward portion along the tail cone axis. 12. The tail cone ventilation system according to claim 8 , further comprising: a conduit attached to the tail cone case at the tail cone exterior and to a pylon at an opposite end, the conduit comprising a cable chase having cable, the cable being in operative communication with the at least one electronic component within the tail cone interior, the cable chase being isolated from the tail cone interior by a firewall, a cooling supply fluidly coupled with the cable chase, the cooling supply configured to cool the cable within the cable chase. 13. The tail cone ventilation system according to claim 8 , wherein the nozzles are configured to direct the cooling air along an inner surface of the tail cone case forming a cooling film layer. 14. A process for cooling a tail cone interior comprising: attaching a tail cone case to a gas turbine engine aft portion, the tail cone case defining a tail cone interior and a tail cone exterior, the tail cone having a forward portion and an aft portion separated axially along a tail cone axis; locating a distribution manifold within the tail cone interior proximate the forward portion; forming nozzles on the distribution manifold, the nozzles arranged radially around the tail cone axis; configuring the nozzles to direct a cooling air over at least one electronic component within the tail cone case; configuring the nozzles to direct a cooling air along an inner surface of the tail cone case; fluidly coupling an air inlet with the distribution manifold through ducting, the air inlet located externally from the tail cone interior; locating a tail cone discharge proximate the tail cone aft portion; and fluidly coupling the tail cone discharge with the distribution manifold. 15. The process of claim 14 , wherein the distribution manifold comprises a circular torus located concentric around the tail cone axis. 16. The process of claim 14 , wherein the distribution manifold comprises more than one torus of varying circumferences, located at various distances from the tail cone forward portion along the tail cone axis. 17. The process of claim 14 , further comprising: attaching a conduit to the tail cone case at the tail cone exterior and to a pylon at an opposite end, the conduit comprising a cable chase having cable, the cable being in operative communication with the at least one electronic component within the tail cone interior, the cable chase being isolated from the tail cone interior by a firewall, a cooling supply fluidly coupled with the cable chase, the cooling supply configured to cool the cable within the cable chase. 18. The process of claim 14 , further comprising: attaching insulation to the tail cone case between the tail cone interior and the tail cone exterior. 19. The process of claim 14 , further comprising: configuring the nozzles to direct the cooling air along an inner surface of the tail cone case forming a cooling film layer. 20. The process of claim 14 , further comprising: fluidly coupling a pylon air scoop to the cable chase; and configuring the pylon air scoop to direct the cooling air to the cable chase through internal flow passages.
characterized by the cooling medium · CPC title
the medium being gaseous, e.g. air {(F02C7/125 takes precedence)} · CPC title
Cooling · CPC title
the elongated body being a closed loop · CPC title
Nozzles or other outlets specially adapted for discharging one or more gases · CPC title
Related publications grouped by family.
Answers are generated from the same data shown on this page.