IP Library › Granted Patent US 7,908,840
Granted Patent B2
US 7,908,840 · App. 11/605,671 · Granted Mar 22, 2011

Turbine engine with integrated generator having shared lubrication system

Assignee: United Technologies Corporation
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Quick Facts
Patent No.
US 7,908,840
App. No.
11/605,671
Granted
Mar 22, 2011
Kind
B2
Abstract

A heat exchange system for use in operating equipment having a plurality of subsystems in each of which a common working fluid is utilized to provide selected operations in that subsystem with a reservoir containing at least some of the common working fluid and has both a supply system and a return system connected between the reservoir and each of the plurality of subsystems through which any common working fluid in the reservoir can be conveyed. An airstream heat exchanger is provided connected in one of the supply and return systems so as to have the common working fluid conveyed therethrough cooled at selectively variable rates in the airstreams passing thereby during at least some such uses of the operating equipment.

Claims (23)

1. A heat exchange system for use in operating equipment having a plurality of subsystems in each of which a common lubricant is utilized to provide selected operations in that subsystem, the heat exchange system providing air and lubricant heat exchanges to cool that common lubricant at selectively variable rates in airstreams occurring with at least some uses of the operating equipment, the system comprising:

a reservoir containing at least some of the common lubricant;

a supply system connected between the reservoir and each of the plurality of subsystems through which common lubricant in the reservoir is conveyed from the reservoir to each of those subsystems;

a return system connected between each of the plurality of subsystems and the reservoir through which the common lubricant passing through each of the plurality of subsystems can be conveyed to the reservoir; and

a first airstream heat exchanger connected in one of the supply and return systems, the first air stream heat exchanger being mounted in a first duct in the operating equipment having a first moveable flap cover at least a portion of one end of the first duct as selected by a control system such that the common lubricant conveyed through the first heat exchanger is cooled at selectively variable rates in the airstreams passing thereby during at least some such uses of the operating equipment; and

a second airstream heat exchanger connected in one of the supply system and return systems so as to have the common lubricant conveyed therethrough cooled at selectively variable rates in the airstreams passing thereby during at least some such uses of the operating equipment.

2. The system of claim 1 wherein the first airstream heat exchanger is connected in the supply system between the reservoir and at least one of the plurality of subsystems.

3. The system of claim 2 wherein the first airstream heat exchanger is connected in the supply system between the reservoir and at least two of the plurality of subsystems.

4. The system of claim 3 wherein the first airstream heat exchanger is connected in the supply system between the reservoir and all of the plurality of subsystems.

5. The system of claim 3 wherein the first airstream heat exchanger is connected in the supply system between the reservoir and just one of the plurality of subsystems, and the second airstream heat exchanger is connected in the supply system between the first airstream heat exchanger and one of the two of the plurality of subsystems so as to have the common lubricant conveyed therethrough cooled at selectively variable rates in the airstreams passing thereby during at least some such uses of the operating equipment.

6. The system of claim 5 further comprising portions of the airstreams being forced into the first duct during at least some such uses of the operating equipment, and the second airstream heat exchanger being mounted in a second duct in the operating equipment with portions of the airstreams being forced into this second duct during at least some such uses of the operating equipment.

7. The system of claim 6 further comprising a second moveable flap and a flap actuator which can force the flap to at least in part cover a portion of one end of the second duct as selected by the control system.

8. The system of claim 2 wherein the first airstream heat exchanger is connected in the supply system between the reservoir and just one of the plurality of subsystems, and the second airstream heat exchanger is connected in the supply system between the reservoir and another one of the plurality of subsystems.

9. The system of claim 8 further comprising portions of the airstreams being forced into the first duct during at least some such uses of the operating equipment, and the second airstream heat exchanger being mounted in a second duct in the operating equipment with portions of the airstreams being forced into this second duct during at least some such uses of the operating equipment.

10. The system of claim 9 further comprising a second moveable flap and a flap actuator which can force the flap to at least in part, as selected by the control system, cover a portion of one end of the second duct.

11. The system of claim 1 further comprising portions of the airstreams being forced into the first duct during at least some such uses of the operating equipment.

12. The system of claim 1 further comprising an operating equipment fuel and common lubricant heat exchanger connected to the operating equipment so as to allow operating equipment fuel to pass along a first passageway therethrough and connected to the supply system so as to allow the common lubricant received from the reservoir to pass along a second passageway therethrough before reaching the first airstream cooled heat exchanger such that the common lubricant can transfer heat to the operating equipment fuel in this operating equipment fuel and common lubricant heat exchanger.

13. A common lubrication system for use with a turbofan engine and an integrated direct drive electrical generator powered by the turbofan engine in which systems a common lubricating oil is utilized for lubricating moving components with the common lubrication system providing air and lubricating oil heat exchanges to thereby cool the common lubricating oil at selectively variable rates in airstreams provided by the fan of the turbofan engine occurring during at least some operations of the turbofan engine, the system comprising:

a reservoir containing at least some of the common lubricating oil;

a supply system connected between the reservoir and both the turbofan engine and the electrical generator through which the common passing through the turbofan engine and the electrical generator can be conveyed to the reservoir; and

a pair of airstream heat exchangers each mounted in a corresponding duct adjacent the turbofan engine with a moveable flap covering at least a portion of one end thereof as selected by a control system and each connected in one of the supply and return systems so as to each have the common working fluid conveyed therethrough cooled at selectively variable rates in the airstreams passing thereby during at least some such operations of the turbofan engine.

14. The system of claim 13 wherein one of the airstream heat exchangers is connected in the supply system between the reservoir and at least one of the turbofan engine and the electrical generator.

15. The system of claim 13 further comprising an operating equipment fuel and common lubricating oil heat exchanger connected to the turbofan engine so as to allow turbofan engine fuel to pass along a first passageway therethrough and connected to the supply system so as to allow common lubricating oil received from the reservoir to pass along a second passageway therethrough before reaching the airstream cooled heat exchanger such that the common lubricating oil can transfer heat to the turbofan engine fuel in this turbofan engine fuel and common lubricating oil heat exchanger.

Assignments (4)
CHANGE OF NAME Recorded Jul 27, 2023
From: RAYTHEON TECHNOLOGIES CORPORATION
To: RTX CORPORATION
Reel/Frame 064714/0001 →
CORRECTIVE ASSIGNMENT TO CORRECT THE AND REMOVE PATENT APPLICATION NUMBER 11886281 AND ADD PATENT APPLICATION NUMBER 14846874. TO CORRECT THE RECEIVING PARTY ADDRESS PREVIOUSLY RECORDED AT REEL: 054062 FRAME: 0001. ASSIGNOR(S) HEREBY CONFIRMS THE CHANGE OF ADDRESS. Recorded Mar 4, 2021
From: UNITED TECHNOLOGIES CORPORATION
To: RAYTHEON TECHNOLOGIES CORPORATION
Reel/Frame 055659/0001 →
CHANGE OF NAME Recorded Sep 4, 2020
From: UNITED TECHNOLOGIES CORPORATION
To: RAYTHEON TECHNOLOGIES CORPORATION
Reel/Frame 054062/0001 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Nov 29, 2006
From: SCHWARZ, FREDERICK M.; GLAHN, JORN A.
To: UNITED TECHNOLOGIES CORPORATION
Reel/Frame 018632/0425 →
Continuity (1)
Related Publication 20080121376A1 · May 29, 2008