Air-oil heat exchanger

• US 20070215326A1
• Filed: 03/17/2006
• Published: 09/20/2007
• Est. Priority Date: 03/17/2006
• Status: Active Grant

• Current Assignee: Raytheon Technologies Corporation d/b/a RTX (Rtx Corporation)
• Original Assignee: United Technologies Corporation (Rtx Corporation)
• Inventors: Schwarz, Frederick, Elsaesser, Frederick
• Granted Patent: US 8,127,828 B2
• Time in Patent Office: Days
• US Class Current: 165/96
• CPC Class Codes: F01D 25/08 Cooling of machines or engines in general F01P; Heating; Heat-insulation of blade-carrying members, of blades F01D5/00
• CPC Class Codes: F01D 25/12 Cooling
• CPC Class Codes: F01D 25/18 Lubricating arrangements of machines or engines in general F01M
• CPC Class Codes: F01D 25/24 Casings modified for heating or cooling F01D25/14; Casing parts, e.g. diaphragms, casing fastenings casings for rotary machines or engines in general F16M ; special arrangements in stators dealing with breaking-off of part of rotor F01D21/045
• CPC Class Codes: F01D 5/046 Heating, heat insulation or cooling means
• CPC Class Codes: F02C 7/06 Arrangements of bearings bearings F16C; Lubricating of turbo machines F01D25/18; of machines or engines in general F01M
• CPC Class Codes: F02C 7/12 Cooling of plants of component parts, see the relevant subclasses, e.g. F01D; cooling of engines in general F01P
• CPC Class Codes: F02C 7/14 of fluids in the plant , e.g. lubricant or fuel F02C7/185 takes precedence
• CPC Class Codes: F02C 7/16 characterised by cooling medium
• CPC Class Codes: F05D 2260/20 Heat transfer, e.g. cooling
• CPC Class Codes: F05D 2260/211 by intercooling, e.g. during a compression cycle
• CPC Class Codes: F05D 2260/232 characterized by the cooling medium
• CPC Class Codes: F28D 2021/0026 for combustion engines, e.g. for gas turbines or for Stirling engines
• CPC Class Codes: F28D 2021/0049 for lubricants, e.g. oil coolers
• CPC Class Codes: F28F 2280/10 Movable elements, e.g. being pivotable
• CPC Class Codes: F28F 9/0246 Arrangements for connecting header boxes with flow lines
• CPC Class Codes: Y02T 50/60 Efficient propulsion technologies, e.g. for aircraft

Abstract

A heat exchange system for use in fluid operated equipment to provide air and working fluid heat exchanges to cool the working fluid in airstreams on a stream side of a wall. An actuator is mounted to be substantially located on a side of the wall opposite the stream side thereof having a positionable motion effector. A heat exchanger core having a plurality of passageway structures therein to enable providing the working fluid to, and removal therefrom. The heat exchanger core is mounted on the motion effector so as to be extendable and retractable thereby through the opening for selected distances into that region to be occupied by the airstreams.

Claims

1. A heat exchange system for use in operating equipment in which a working fluid is utilized in providing selected operations thereof, the heat exchange system for providing air and working fluid heat exchanges to cool the working fluid at selectively variable rates in airstreams occurring on a stream side of a wall provided with the equipment, the system comprising:

an actuator mounted to be substantially located on a side of the wall opposite the stream side and having a positionable motion effector therein that can be moved to selected positions with respect to an opening in the wall; and

a heat exchanger core having a plurality of passageway structures therein about which air can pass in flowing therethrough with the passageway structures being coupled to an input conduit at one end thereof and coupled to an output conduit at an opposite end thereof to enable the working fluid to be provided, and removed from, interiors of the passageway structures through interiors of the input and output conduits, the heat exchanger core being mounted on the motion effector so as to be extendable thereby through the opening for selected distances into that region to be occupied by the airstreams on the stream side of the wall, and selectively retractable from those distances.

2. The system of claim 1 further comprising the heat exchanger core having a closing structure thereon, the heat exchanger core being out of the region to be occupied by the airstreams if the heat exchanger core is in an unextended position and with the closing structure then substantially blocking the opening, and in the region to be occupied by the airstreams at least in part if the heat exchanger core is in an extended position.

3. The system of claim 1 wherein the actuator comprises a motor rotating a jackscrew within a threaded nut affixed to a side of the heat exchanger core.

4. The system of claim 1 wherein an input portion of the plurality of passageway structures are coupled to an input conduit at one end thereof and an output portion of the plurality of passageway structures are coupled to an output conduit at one end thereof, the input portions and the output portions of the plurality of passageway structures being coupled to corresponding ones of each other at opposite ends thereof.

5. The system of claim 2 further comprising a container having an interior within which the actuator and the heat exchanger core are provided at least in part, the interior of the container being substantially closed from the region to be occupied by the airstreams if the heat exchanger core is in an unextended position by the closing structure on the heat exchanger core substantially blocking the opening so as to have an outer surface thereof flush with, and following contours of, adjacent portions of that surface of the wall on the stream side thereof.

6. The system of claim 2 further comprising a pair of sidewalls provided substantially perpendicular to the wall and extending along opposite sides of the heat exchanger core substantially parallel to that direction primarily followed by the airstreams in the region to be occupied thereby.

7. The system of claim 2 further comprising a baffle coupled to the heat exchanger core on a side thereof opposite the closing structure and extending in a direction opposite that direction primarily followed by the airstreams in the region to be occupied thereby such that the baffle substantially seals that portion of the interior on one side of the heat exchanger core from that portion of the interior on an opposite side of the baffle.

8. The system of claim 5 further comprising an container inlet and container outlet provided through a side of the container, and a core inlet and a core outlet provided on the heat exchanger core having the open interior passageways in the heat exchanger core connected therebetween, the container inlet and the core inlet being coupled by a flexible conduit with the container outlet and the core outlet also being coupled by a another flexible conduit such that the working fluid can be caused to enter the container inlet and to pass through the core inlet, the open interior passageways, the core outlet and the container outlet, the flexible conduits flexing sufficiently to remain so coupled following extensions and retractions of the heat exchange core.

9. The system of claim 5 further comprising a pair of sidewalls mounted in the container provided substantially perpendicular to the wall and extending along opposite sides of the heat exchanger core substantially parallel to that direction primarily followed by the airstreams in the region to be occupied thereby.

10. The system of claim 5 further comprising a baffle in the interior of the container coupled to the heat exchanger core on a side thereof opposite the closing structure and extending nearly to a side of the container in a direction opposite that direction primarily followed by the airstreams in said region to be occupied thereby such that the baffle substantially seals that portion of the interior on one side of the heat exchanger core from that portion of the interior on an opposite side of the baffle.

11. The system of claim 5 wherein the closing structure has an end facing a direction opposite that direction primarily followed by the airstreams in the region to be occupied thereby having a surface beginning thereat substantially parallel to the wall with sufficient convexity inwardly from the end to become oriented substantially perpendicular to the wall.

12. The system of claim 9 further comprising a baffle in the interior of the container coupled to the heat exchanger core on a side thereof opposite the closing structure and extending nearly to a side of the container in a direction opposite that direction primarily followed by the airstreams in the region to be occupied thereby such that the baffle substantially seals that portion of the interior on one side of the heat exchanger core from that portion of the interior on an opposite side of the baffle.

13. A heat exchange system for use in lubricating systems for aircraft turbofan engine equipment in which a lubricant is provided under pressure to spaces bounded at least in part by surfaces moving relative to one another, the heat exchange system for providing air and lubricant heat exchanges to cool the lubricant at selectively variable rates in airstreams occurring on a stream side of an engine fan duct wall, the system comprising:

a controllable motor having a shaft with a selectable angular position with the motor being mounted to be substantially located on a side of the wall opposite the stream side and having a positionable motion effector coupled to the shaft that can be moved to selected positions with respect to an opening in the wall by selected rotations of the shaft; and

a heat exchanger core having a closing structure thereon and having a plurality of passageway structures therein about which air can pass in flowing therethrough with the passageway structures being coupled to an input conduit at one end thereof and coupled to an output conduit at an opposite end thereof to enable the lubricant to be provided, and removed from, interiors of the passageway structures through interiors of the input and output conduits, the heat exchanger core being mounted on the motion effector so as to be extendable thereby through the opening for selected distances into that region to be occupied by the airstreams on the stream side of the wall in an extended position, and selectively retractable from those distances including retracted sufficiently to be out of the region to be occupied by the airstreams if the heat exchanger core is in an unextended position such that the closing structure on the heat exchanger core substantially blocks the opening.

14. The system of claim 13 wherein the closing structure on the heat exchanger core substantially blocks the opening so as to have an outer surface thereof flush with, and following contours of, adjacent portions of that surface of the wall on the stream side thereof.

15. The system of claim 13 further comprising a container having an interior within which the motor and the heat exchanger core are provided at least in part, and in which a pair of sidewalls mounted in the container are provided substantially perpendicular to the wall and which extend along opposite sides of the heat exchanger core substantially parallel to that direction primarily followed by the airstreams in the region to be occupied thereby.

16. The system of claim 13 further comprising a container having an interior within which the motor and the heat exchanger core are provided at least in part, and in which a baffle is provided in the interior of the container coupled to the heat exchanger core on a side thereof opposite the closing structure and extending nearly to a side of the container in a direction opposite that direction primarily followed by the airstreams in said region to be occupied thereby such that the baffle substantially seals that portion of the interior on one side of the heat exchanger core from that portion of the interior on an opposite side of the baffle.

17. The system of claim 13 wherein the closing structure has an end facing a direction opposite that direction primarily followed by the airstreams in the region to be occupied thereby having a surface beginning thereat substantially parallel to the wall with sufficient convexity inwardly from the end to become oriented substantially perpendicular to the wall.

18. A heat exchange system for use in lubricating systems for aircraft turbofan engine equipment in which a lubricant is provided under pressure to spaces bounded at least in part by surfaces moving relative to one another, the heat exchange system for providing air and lubricant heat exchanges to cool the lubricant at selectively variable rates in airstreams occurring on a stream side of an engine fan duct wall, the system comprising:

a controllable motor having a shaft with a selectable angular position with the motor being mounted to be substantially located on a side of the wall opposite the stream side and having a positionable motion effector coupled to the shaft that can be moved to selected positions with respect to an opening in the wall by selected rotations of the shaft;

a heat exchanger core having a plurality of passageway structures therein about which air can pass in flowing therethrough with the passageway structures being coupled to an input conduit at one end thereof and coupled to an output conduit at an opposite end thereof to enable the lubricant to be provided, and removed from, interiors of the passageway structures through interiors of the input and output conduits, the heat exchanger core being mounted on the motion effector so as to be extendable thereby through the opening for selected distances into that region to be occupied by the airstreams on the stream side of the wall in an extended position, and selectively retractable from those distances; and

a container mounted to the wall about the opening having an interior within which the motor and the heat exchanger core are provided at least in part.

19. The system of claim 18 further comprising the heat exchanger core having a closing structure thereon wherein the interior of the container is substantially closed from the region to be occupied by the airstreams if the heat exchanger core is in an unextended position by the closing structure on the heat exchanger core substantially blocking the opening so as to have an outer surface thereof flush with, and following contours of, adjacent portions of that surface of the wall on the stream side thereof.

20. The system of claim 18 further comprising an container inlet and container outlet provided through a side of the container, and a core inlet and a core outlet provided on the heat exchanger core having the open interior passageways in the heat exchanger core connected therebetween, the container inlet and the core inlet being coupled by a flexible conduit with the container outlet and the core outlet also being coupled by a another flexible conduit such that the lubricant can be caused to enter the container inlet and to pass through the core inlet, the open interior passageways, the core outlet and the container outlet, the flexible conduits flexing sufficiently to remain so coupled following extensions and retractions of the heat exchange core.