IP Library Granted Patent US 12709983
Granted Patent B2
US 12709983 · App. 18/952,066 · Granted Aug 18, 2026

Fretting resistant rotary engine housings

Inventors: Vincent Savaria (Laval, CA); Jean-Philippe Simoneau (Saint-Constant, CA)
Assignee: PRATT & WHITNEY CANADA CORP.
F01C1/22F01C19/005F01C21/10F02B55/08F02B2053/005F05C2253/12
View Patent ↗
Loading inventors, assignments & file history…
Monitor This Case
Get email alerts when status or documents change.
Order Certified Copies
Most orders are placed with the USPTO same day — all within 24 business hours.
Order via The Patent Place →
Pre-filled with this patent's details
Quick Facts
Patent No.
US 12709983
App. No.
18/952,066
Granted
Aug 18, 2026
Kind
B2
Abstract

A rotary internal combustion engine includes a main rotor housing that has a peripheral wall that circumscribes a rotor cavity, a first interface surface and a second interface surface. A rotor is disposed within the rotor cavity. First and second side housings are secured against corresponding first and interface surfaces of the main rotor housing. The main rotor housing, the first side housing and the second side housing are formed from an aluminum alloy and at least one of the first interface surface and the second interface surface include an anti-fretting coating.

Claims (39)

1 . A method of assembling a rotary internal combustion engine comprising:

forming at least a main rotor housing, a first side housing and a second side housing from an aluminum alloy;

forming a first side plate and a second side plate;

selecting interface surfaces between at least the main rotor housing, the first side housing, the second side housing, the first side plate and the second side plate;

masking non-selected surface of the each of the at least the main rotor housing, the first side housing, the second side housing, the first side plate and the second side plate; and

applying an anti-fretting coating to the selected interface surfaces, wherein the rotary internal combustion engine further comprises a first bearing support and a second bearing support that abut against an inner bore surface of a corresponding one of the first side housing and the second side housing, and the method further comprises applying an anti-fretting coating to the inner bore surface of each of the first side housing and the second side housing.

2 . The method as recited in claim 1 , further comprising forming a recess on at least one of the selected interface surfaces prior to application of the anti-fretting coating, wherein the recess is formed to correspond with a final thickness of the anti-fretting coating.

3 . The method as recited in claim 1 , further comprising applying the anti-fretting coating to first thickness and machining the anti-fretting coating to a second thickness that is less than the first thickness.

4 . The method as recited in claim 1 , further comprising selecting a radially outer surface on each of a first transfer housing and a second transfer housing that abuts a corresponding radial face surface of one of the first side housing and the second side housing and applying the anti-fretting coating to the radially outer surface.

5 . The method as recited in claim 4 , wherein each of the first transfer housing and the second transfer housing include a seal surface adjacent to a radially inner surface and the method includes the step of masking the seal surface.

6 . The method as recited in claim 1 , wherein the anti-fretting coating comprises one of a chromium carbide, an aluminum bronze, or a tungsten carbide.

7 . A method of configuring a rotary internal combustion engine comprising:

configuring a main rotor housing to have a peripheral wall circumscribing a rotor cavity, a first interface surface and a second interface surface;

configuring a rotor for operation within the rotor cavity;

configuring a first side housing for securement against the first interface surface of the main rotor housing;

configuring a second side housing for securement against the second interface surface of the main rotor housing, wherein the main rotor housing, the first side housing and the second side housing are formed from an aluminum alloy and at least one of the first interface surface and the second interface surface are configured to includes an anti-fretting coating;

configuring a first side plate to be partially disposed within a clearance space between the first side housing and the main rotor housing;

configuring a second side plate to be partially disposed within a clearance space disposed between the second side housing and the main rotor housing, wherein each of the first side plate and the second side plate are further configured to define a running surface for the rotor; and

configuring a first transfer housing and a second transfer housing to each include a radially outer surface abutting a corresponding inner radial face surface of one of the first side housing and the second side housing; and

configuring each of the corresponding inner face surfaces of the first side housing and the second side housing to receive an anti-fretting coating.

8 . The method of configuring a rotary internal combustion engine as recited in claim 7 , further comprising configuring each of the first side housing and the second side housing to include a plate support surface that abuts a corresponding one of the first side plate and the second side plate and configuring each plate support surface to receive an anti-fretting coating.

9 . The method of configuring a rotary internal combustion engine in claim 8 , further comprising configuring of each of the first side housing and the second side housing to include a peripheral surface abutting a corresponding one of the first side plate and the second side plate and configuring the peripheral surface to include an anti-fretting coating.

10 . The method of configuring a rotary internal combustion engine as recited in claim 9 , further comprising configuring the radial face surface of each of the first side housing and the second side housing to be recessed to accommodate a thickness of the anti-fretting coating.

11 . The method of configuring a rotary internal combustion engine as recited in claim 10 , further comprising configuring each of the first transfer housing and the second transfer housing to include a seal surface adjacent to the radially inner surface that does not include the anti-fretting coating.

12 . The method of configuring a rotary internal combustion engine as recited in claim 7 , further comprising configuring a first bearing support and a second bearing support to abut against an inner bore surface of a corresponding one of the first side housing and the second side housing and configuring the inner bore surface of each of the first side housing and the second side housing to include an anti-fretting coating.

13 . The method of configuring a rotary internal combustion engine as recited in claim 7 , further comprising configuring the anti-fretting coating as a thermal spray coating containing at least one of a chromium carbide, aluminum bronze, or tungsten carbide.

14 . The method of configuring a rotary internal combustion engine a recited in claim 7 , further comprising configuring the anti-fretting coating as one of an anodizing coating, a hard carbon coating, an electro-deposition coating or an aluminum powder coating.

15 . The method of configuring a rotary internal combustion engine as recited in claim 7 , further comprising configuring the anti-fretting coating to be machined to a desired thickness.

16 . A method of assembling a rotary internal combustion engine comprising:

forming at least a main rotor housing, a first side housing and a second side housing from an aluminum alloy;

forming a first side plate and a second side plate;

selecting interface surfaces between at least the main rotor housing, the first side housing, the second side housing, the first side plate and the second side plate;

masking non-selected surface of the each of the at least the main rotor housing, the first side housing, the second side housing, the first side plate and the second side plate;

applying an anti-fretting coating to the selected interface surfaces; and

forming a recess on at least one of the selected interface surfaces prior to application of the anti-fretting coating, wherein the recess is formed to correspond with a final thickness of the anti-fretting coating.

17 . The method as recited in claim 16 , further comprising applying the anti-fretting coating to first thickness and machining the anti-fretting coating to a second thickness that is less than the first thickness.

18 . The method as recited in claim 16 , further comprising selecting a radially outer surface on each of a first transfer housing and a second transfer housing that abuts a corresponding radial face surface of one of the first side housing and the second side housing and applying the anti-fretting coating to the radially outer surface.

19 . The method as recited in claim 18 , wherein each of the first transfer housing and the second transfer housing include a radially inner surface and the method includes the step of applying the anti-fretting coating to the radially inner surface.

20 . The method as recited in claim 16 , wherein the anti-fretting coating comprises one of a chromium carbide, an aluminum bronze, or a tungsten carbide.