IP Library Granted Patent US 8,973,552
Granted Patent B2
US 8,973,552 · App. 13/169,401 · Granted Mar 10, 2015

Integral oil system

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Quick Facts
Patent No.
US 8,973,552
App. No.
13/169,401
Granted
Mar 10, 2015
Kind
B2
Abstract

An oil management system includes an engine housing assembly which defines a first rotor volume and a second rotor volume. An oil cooler assembly arranged between the first rotor volume and the second rotor volume.

Claims (35)

1. An oil management system comprising:

an engine housing assembly which defines a first rotor housing and a second rotor housing;

the first rotor housing and the second rotor housing which define a first rotor volume and a second rotor volume, respectively;

an oil cooler assembly between said first rotor volume and said second rotor volume, said oil cooler assembly including an oil reservoir;

a coolant circuit in communication with said oil cooler assembly, said coolant circuit including at least one passage through said oil reservoir,

said at least one passage is integral to the first rotor housing and the second rotor housing to fluidly connect the first rotor housing and the second rotor housing; and

wherein water flows through said at least one passage.

2. The system as recited in claim 1 , wherein said oil reservoir includes an oil filter.

3. The system as recited in claim 1 , wherein a plurality of coolant fins are provided in said oil reservoir.

4. An engine comprising:

a compressor housing including a first rotor within a first rotor volume;

a power housing including a second rotor within a second rotor volume;

an oil cooler assembly between said compressor section and said power section, said oil cooler assembly including an oil reservoir;

a coolant circuit in communication with said oil cooler assembly, said coolant circuit including a plurality of passages through said oil reservoir,

said plurality of passages are integral with the compressor housing and the power housing to fluidly connect the compressor housing and the power housing;

wherein said first rotor and said second rotor are mounted to a shaft; and

wherein, in planes normal to an engine axis of rotation, surfaces of said first and second rotor volumes are substantially two-lobed epitrochoids.

5. The engine as recited in claim 4 , wherein said engine is a rotary engine.

6. The engine as recited in claim 4 , wherein said plurality of passages includes a plurality of first passages arranged circumferentially about said shaft.

7. The engine as recited in claim 6 , wherein said plurality of passages includes a plurality of second passages spaced-apart from said plurality of first passages.

8. The engine as recited in claim 4 , wherein first and second eccentric cams are mounted to said shaft, said first and second eccentric cams driving a respective one of said first and second rotors.

9. The engine as recited in claim 4 , wherein water flows through said plurality of passages.

10. A pusher prop propulsion system comprising:

an engine defined along a propeller axis of rotation;

an engine housing assembly including a first rotor housing defining a first rotor volume and including a second rotor housing defining a second rotor volume;

an oil management system integral with said engine,

said oil management system including an oil reservoir located within said engine housing assembly; and

an engine coolant flow circuit in thermal communication with said oil management system, said engine coolant flow circuit including a plurality of passages through said oil reservoir,

said plurality of passages are integral with the first rotor housing and the second rotor housing to fluidly connect the first rotor housing and the second rotor housing;

a first rotor within said first rotor volume and a second rotor within a second rotor volume, wherein said first rotor and said second rotor are mounted to a shaft along said propeller axis of rotation; and

first and second eccentric cams mounted to said shaft, said first and second eccentric cams configured to drive a respective one of said first and second rotors.

11. The system as recited in claim 10 , wherein said engine is a rotary engine.

12. The engine as recited in claim 10 , further comprising a propeller driven by said engine.

13. The engine as recited in claim 10 , wherein said oil reservoir includes an oil filter.

14. The system as recited in claim 10 , wherein water flows through said plurality of passages.

Assignments (10)
TERMINATION AND RELEASE OF SECURITY INTEREST IN PATENTS Recorded Jul 28, 2023
From: BANK OF AMERICA, N.A., AS ADMINISTRATIVE AGENT
To: AEROJET ROCKETDYNE, INC.
Reel/Frame 064424/0109 →
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 →
RELEASE OF SECURITY INTEREST Recorded Aug 5, 2016
From: U.S. BANK NATIONAL ASSOCIATION
To: AEROJET ROCKETDYNE OF DE, INC. (F/K/A PRATT & WHITNEY ROCKETDYNE, INC.)
Reel/Frame 039597/0890 →
LICENSE Recorded Aug 5, 2016
From: UNITED TECHNOLOGIES CORPORATION
To: AEROJET ROCKETDYNE, INC. (F/K/A AEROJET-GENERAL CORPORATION, SUCCESSOR OF RPW ACQUISITION LLC)
Reel/Frame 039595/0315 →
NOTICE OF GRANT OF SECURITY INTEREST IN PATENTS Recorded Jun 17, 2016
From: AEROJET ROCKETDYNE, INC., SUCCESSOR-IN-INTEREST TO RPW ACQUISITION LLC
To: BANK OF AMERICA, N.A., AS ADMINISTRATIVE AGENT
Reel/Frame 039197/0125 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Jul 10, 2013
From: PRATT & WHITNEY ROCKETDYNE, INC.
To: UNITED TECHNOLOGIES CORPORATION
Reel/Frame 030774/0529 →
SECURITY AGREEMENT Recorded Jun 21, 2013
From: PRATT & WHITNEY ROCKETDYNE, INC.
To: U.S. BANK NATIONAL ASSOCIATION
Reel/Frame 030656/0615 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Jun 27, 2011
From: HORN, MARK D.
To: PRATT & WHITNEY ROCKETDYNE, INC.
Reel/Frame 026505/0780 →