Hybrid aircraft propulsion system with electric motor alignment
A hybrid aircraft propulsion system includes a first motor operatively connected to a propulsor via a first motor driveshaft and is mounted to an engine static structure through engine mounts operable to adjust a position of the first motor and the first motor driveshaft. A second motor is an electric motor having a second motor driveshaft which is coaxial to the first motor driveshaft. The second motor is operatively connected to the propulsor via the second motor driveshaft to selectively drive the propulsor. A height compensation structure is operatively connected to the second motor and structured to adjust axial alignment of the second motor driveshaft relative to the first motor driveshaft to make the first motor driveshaft more coaxial to the second motor driveshaft.
1 . A hybrid aircraft propulsion system, comprising:
a first motor operatively connected to a propulsor via a first motor driveshaft and being mounted to an engine static structure through engine mounts operable to adjust a position of the first motor and the first motor driveshaft;
a second motor, being an electric motor having a second motor driveshaft which is coaxial to the first motor driveshaft, the second motor being operatively connected to the propulsor via the second motor driveshaft to selectively drive the propulsor; and
a height compensation structure operatively connected to the second motor and structured to adjust axial alignment of the second motor driveshaft relative to the first motor driveshaft to make the first motor driveshaft more coaxial to the second motor driveshaft.
2 . The hybrid system as set forth in claim 1 , wherein the first motor is one or more of a gas turbine engine, a rotary engine, a reciprocating engine, and an electric motor.
3 . The hybrid system as set forth in claim 2 , wherein the second motor is mounted through a second motor mount such that it can slide within a guide, and is provided with a spring bias to control the amount of movement of the second motor, the second motor mount being part of the height compensation system.
4 . The hybrid system as set forth in claim 3 , wherein a hydraulic connection between the first motor and the height compensation structure communicates movement of the first motor to the height compensation to provide adjustment of the height of the second motor in response to adjustment of the height of the first motor.
5 . The hybrid system as set forth in claim 4 , wherein the hydraulic connection provides feedback of both an attitude change and a height change of the first motor to the height compensation structure.
6 . The hybrid system as set forth in claim 5 , wherein there is the second motor mount has a pivot connection between the second motor and second motor static structure such that the second motor can pivot and move vertically with the first motor.
7 . The hybrid system as set forth in claim 6 , wherein the second motor mount includes a gimbal member which is pivotally mounted to the second motor to allow pivoting movement about a first axis, and the gimbal structure is pivotally mounted to the second motor static structure such that second motor may also pivot about a second axis.
8 . The hybrid system as set forth in claim 5 , wherein there are elastomeric mounting blocks as part of the second motor mount and the second motor static structure that allow the adjustment of the second motor in response to movement of the first motor.
9 . The hybrid system as set forth in claim 5 , wherein there are a pair of front mount hydraulic cylinders associated with port and starboard sides of the first motor, and a pair of rear port and starboard mounts associated with the first motor, each having fluid cylinders and fluid pistons, and communicating hydraulic fluid between opposed chambers on each side of the respective fluid pistons to each of the front starboard and port mounts and rear starboard and port mounts, and to a second motor adjustment cylinder having a second motor piston that is part of the height compensation structure.
10 . The hybrid system as set forth in claim 2 , wherein the second motor driveshaft is connected to the first motor driveshaft and to the second motor through flexible diaphragms.
11 . The hybrid system as set forth in claim 1 , wherein a hydraulic connection between the first motor and the height compensation structure communicates movement of the first motor to the height compensation structure to provide adjustment of the height of the second motor in response to adjustment of the height of the first motor.
12 . The hybrid system as set forth in claim 11 , wherein there is a second motor mount as part of the height compensation system, with an element on the second motor is guided within a guide on the second motor mount to allow height adjustment.
13 . The hybrid system as set forth in claim 12 , wherein the hydraulic connection provides feedback of both an attitude change and a height change of the first motor to the height compensation structure.
14 . The hybrid system as set forth in claim 3 , wherein the second motor mount also includes a pivot connection between the second motor and second motor static structure such that the second motor can pivot and move vertically with the first motor.
15 . The hybrid system as set forth in claim 14 , wherein a control for the first motor and the second motor operates the second motor selectively under high power conditions to supplement the drive from the first motor.
16 . The hybrid system as set forth in claim 14 , wherein there are a pair of front mount hydraulic cylinders associated with port and starboard sides of the first motor, and a pair of rear port and starboard mounts associated with the first motor, each having fluid cylinders and fluid pistons, and communicating hydraulic fluid between opposed chambers on each side of the respective fluid pistons to each of the front starboard and port mounts and rear starboard and port mounts, and to a first second motor adjustment cylinder having a second motor piston that is part of the height compensation structure.
17 . The hybrid system as set forth in claim 14 , wherein the second motor mount includes a gimbal member which is pivotally mounted to the second motor to allow pivoting movement about a first axis, and the gimbal structure is pivotally mounted to the second motor static structure such that second motor may also pivot about a second axis.
18 . The hybrid system as set forth in claim 1 , wherein there are elastomeric mounting blocks as part of a second motor mount that is part of the height compensation structure and second motor static structure that allow adjustment of the second motor in response to movement of the first motor.
19 . The hybrid system as set forth in claim 1 , wherein the second motor driveshaft is connected to the first motor driveshaft and to the second motor through flexible diaphragms.
20 . The hybrid system as set forth in claim 1 , wherein a control for the second motor and the first motor operates the second motor selectively under high power conditions to supplement the drive from the first motor.