IP Library Granted Patent US 9,435,204
Granted Patent B2
US 9,435,204 · App. 13/052,859 · Granted Sep 6, 2016

Structurally efficient cooled engine housing for rotary engines

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Quick Facts
Patent No.
US 9,435,204
App. No.
13/052,859
Granted
Sep 6, 2016
Kind
B2
Abstract

An engine includes a housing having a single wall, where the wall has a rib and a flange, and the wall provides a primary structure and cooling for the engine. A closeout is attached to an outer surface of the wall, and the closeout and the wall form a cavity. The closeout provides a secondary structure for containing a coolant fluid flow within the cavity. The closeout may be corrugated, and the ribs may be exposed to the cavity.

Claims (37)

1. An apparatus for an engine, comprising:

a tubular housing structure extending along a centerline and comprising:

an inner wall portion extending about and axially along the centerline;

a first flange projecting radially out from the inner wall portion;

a second flange projecting radially out from the inner wall portion;

a first rib projecting radially out from the inner wall portion, and extending axially between the first flange and the second flange; and

a second rib projecting radially out from the inner wall portion, and extending axially between the first flange and the second flange; and

a closeout radially recessed into a side of and forming a cavity with the tubular housing structure, and the closeout attached to the tubular housing structure;

wherein the cavity extends axially between the first flange and the second flange, laterally between the first rib and the second rib, and radially outward from the inner wall portion to the closeout.

2. The apparatus of claim 1 , wherein the closeout is welded to the tubular housing structure.

3. The apparatus of claim 1 , where the closeout carries a load from coolant within the cavity and the closeout is free of engine loads.

4. The apparatus of claim 1 , wherein the closeout is one of a plurality of closeouts distributed about the centerline and attached to the tubular housing structure.

5. The apparatus of claim 1 , further comprising:

a third rib projecting radially out from the inner wall portion, and extending axially between the first flange and the second flange; and

a second closeout radially recessed into the side of and forming a second cavity with the tubular housing structure, wherein the second closeout is attached to the tubular housing structure;

wherein the second cavity extends axially between the first flange and the second flange, laterally between the first rib and the third rib, and radially outward from the inner wall portion to the second closeout.

6. The apparatus of claim 1 , further comprising:

a third rib projecting radially out from the inner wall portion, and extending axially between the first flange and the second flange;

a fourth rib projecting radially out from the inner wall portion, and extending axially between the first flange and the second flange; and

a second closeout radially recessed into the side of and forming a second cavity with the tubular housing structure, wherein the second closeout is attached to the tubular housing structure;

wherein the second cavity extends axially between the first flange and the second flange, laterally between the third rib and the fourth rib, and radially outward from the inner wall portion to the second closeout.

7. The apparatus of claim 1 , wherein the closeout comprises sheet metal.

8. The apparatus of claim 1 , wherein the closeout comprises a corrugated sheet of material.

9. The apparatus of claim 1 , further comprising a fin projecting radially out from the inner wall portion and partially into the cavity.

10. The apparatus of claim 9 , wherein the fin extends axially between the first flange and the second flange.

11. The apparatus of claim 1 , further comprising a plurality of fins projecting radially out from the inner wall portion and partially into the cavity.

12. The apparatus of claim 1 , wherein the inner wall portion has a trochoidal inner surface.

13. A rotary engine, comprising:

a tubular housing structure extending along a centerline and comprising:

an inner wall portion extending about and axially along the centerline;

a first flange projecting radially out from the inner wall portion;

a second flange projecting radially out from the inner wall portion;

a first rib projecting radially out from the inner wall portion, and extending axially between the first flange and the second flange; and

a second rib projecting radially out from the inner wall portion, and extending axially between the first flange and the second flange;

a closeout radially recessed into a side of and forming a cavity with the tubular housing structure, and the closeout attached to the tubular housing structure; and

a rotor arranged within an inner volume formed by and radially within the inner wall portion;

wherein the cavity extends axially between the first flange and the second flange, laterally between the first rib and the second rib, and radially outward from the inner wall portion to the closeout.

Assignments (9)
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 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Mar 22, 2011
From: HORN, MARK DAVID
To: PRATT & WHITNEY ROCKETDYNE, INC.
Reel/Frame 025994/0657 →