Turboprop propulsion apparatus

• US 4,817,382 A
• Filed: 12/31/1985
• Issued: 04/04/1989
• Est. Priority Date: 12/31/1985
• Status: Expired due to Fees

• Current Assignee: The Boeing Co.
• Original Assignee: The Boeing Co.
• Inventors: Ostrom, Grazyna B., Rudolph, Peter K. C.
• Primary Examiner(s): NOT, DEFINED
• Application Number:
  US06/815,447
• Time in Patent Office: 1,190 Days
• Field of Search: 60/226.1, 60/39.162, 60/268, 60/39.31, 60/39.161, 416/171, 416/170 R, 416/129, 416/128, 74/786, 74/785
• US Class Current: 60/268
• CPC Class Codes: B64D 27/026 comprising different types of power plants, e.g. combination of a piston engine and a gas-turbine Hybrid electric aircraft B64D27/33
• CPC Class Codes: F02C 3/067 having counter-rotating rotors F02C3/073 takes precedence
• CPC Class Codes: F02C 3/10 with another turbine driving an output shaft but not driving the compressor
• CPC Class Codes: F02K 3/072 with counter-rotating , e.g. fan rotors
• CPC Class Codes: Y02T 50/60 Efficient propulsion technologies, e.g. for aircraft

Abstract

A turboprop propulsion system where there is a core engine driving a power turbine that is connected through a planetary drive transmission to first and second counterrotating propellers. One of the propellers is connected to the ring gear, while the other propeller is connected to the planetary carrier, the sun gear being driven from the power turbine. The apparatus is provided with a substantially continuous gaseous flow path from the inlet to the exhaust nozzle of the engine, with the planetary drive transmission being spaced radially from the flow path. In some embodiments, the planetary transmission is positioned radially inwardly of the flow path, while in other embodiments, it is positioned radially outwardly of the flow path. The propellers can be in either the pusher configuration or the tractor configuration.

Claims

1. A turboprop propulsion assembly comprising:

a. a nacelle having a support structure;

b. a gas generating and power section mounted in said support structure and having a longitudinally extending operating axis, said gas generating and power section comprising;

1. a compressor means to receive intake air;

2.

3. gear to cause counter-rotation of said propellers. 2. The assembly as recited in claim 1, wherein said planetary drive transmission is positioned radially inwardly of said flow path, and said first and second torque frame means extend from said ring gear means and said planetary carrier means through said flow path to connect to said first and second propellers.

5. The assembly as recited in claim 3, wherein said first and second torque frame means comprise strut means contoured to react to gaseous flow from said turbine means to create a power input to said propellers.

6. The assembly as recited in claim 3, wherein said propellers are mounted to a rear portion of said support structure in a pusher configuration.

8. The assembly as recited in claim 6, wherein said first and second torque frame means comprise strut means contoured to react to gaseous flow into said compressor means to create a supercharging effect to the compressor means.

9. The assembly as recited in claim 6, wherein said propellers are mounted to a forward portion of said support structure in a tractor configuration.

10. The assembly as recited in claim 1, wherein said planetary drive transmission is located radially outwardly of said flow path, and there is connecting means extending through said flow path and operatively connecting said turbine means with said sun gear means.

11. The assembly as recited in claim 9, when there is a path section of said path positioned forwardly of said compressor means, and said connecting means extends through said path section.

12. The assembly as recited in claim 10, wherein said connecting means comprises strut means extending through said path section.

13. The assembly as recited in claim 10, wherein said propellers are mounted to a forward portion of said support structure in a tractor configuration.

14. The assembly as recited in claim 9, wherein there is a path section of said path positioned rearwardly of said turbine means, and said connecting means extends through said path section.

15. The assembly as recited in claim 13, wherein said connecting means comprises strut means contoured to engage gaseous exhaust from said turbine means to provide additional power to said propellers.

16. The assembly as recited in claim 13, wherein said propellers are mounted to a rear portion of said support structure in a pusher configuration.

17. The assembly as recited in claim 9, wherein there is a planetary drive assembly mounted radially inwardly of said flow path, and said planetary assembly is drivingly connected between said turbine means through said connecting means to the sun gear of the planetary drive transmission in a manner to cause speed reduction of said sun gear means relative to said turbine means.

18. The assembly as recited in claim 16, wherein said planetary assembly comprises a second sun gear means operatively connected to said turbine means, a second ring gear means connected through said connecting means to said sun gear means of the planetary transmission, and second planetary means having a planetary carrier mounted so as to be stationary relative to said nacelle support structure.

19. The assembly as recited in claim 16, wherein said planetary assembly is positioned forwardly of said compressor section, and there is a flow section of said flow path positioned forwardly of said compressor means, said connecting means extending through said flow path section.

20. The assembly as recited in claim 16, wherein said planetary assembly is positioned rearwardly of said turbine section, and there is a flow path section of said fluid flow path positioned rearwardly of said turbine means, said connecting means extending through said flow path section.

21. The assembly as recited in claim 9, wherein there is a planetary assembly positioned radially outwardly of said fluid flow path, said planetary assembly being drivingly connected between said planetary transmission and said turbine means.

22. The assembly as recited in claim 20, wherein said connecting means is operatively connected between said turbine means and a sun gear of said planetary assembly, said planetary assembly further comprising a second planetary means comprising a second planetary gear means and a second planetary carrier, said second planetary carrier being connected to the sun gear means of the planetary transmission.

23. The assembly as recited in claim 21, wherein said propellers are mounted at a forward portion of said nacelle support structure, and there is a flow path section of said fluid flow path located forwardly of said compressor means, said connecting means extending through said flow path section to connect to said planetary assembly.

24. The assembly as recited in claim 21, wherein said propellers are mounted to a rear portion of said nacelle support structure, and there is a flow path section of said fluid flow path positioned rearwardly of said turbine means, said connecting means extending through said flow path section to connect to said planetary assembly.

25. The assembly as recited in claim 20, wherein said propellers are mounted at a forward portion of said nacelle support structure, and there is a flow path section of said fluid flow path located forwardly of said compressor means, said connecting means extending through said flow path section to connect to said planetary assembly.

26. The assembly as recited in claim 20, wherein said propellers are mounted to a rear portion of said nacelle structure, and there is a flow path section of said fluid flow path positioned rearwardly of said turbine means, said connecting means extending through said flow path section to connect to said planetary assembly.

27. The assembly as recited in claim 1, wherein said propulsion assembly has a primary mount by which said gas generating and power system, said propellors and said drive transmission are mounted to said nacelle support structure, said primary mount being positioned immediately rearwardly of said turbine means and forwardly of said planetary drive transmission, with loads from said planetary drive transmission being transmitted to said primary mount.

28. The assembly as recited in claim 26, wherein said planetary drive transmission is positioned radially inwardly of said flow path, and said first and second torque frame means extend from said ring gear means and said planetary carrier through said flow path to connect to said first and second propellors, whereby said propellors can be desirably located relative to said planetary drive transmission to provide relatively short load paths to the drive transmission, with the drive transmission having a relatively short load path to said primary mount.

29. The assembly as recited in claim 1, wherein said propulsion assembly has a primary mount by which said gas generating and power system, said propellors and said drive transmission are mounted to said nacelle support structure, said primary mount being positioned immediately forwardly of said compressor means and rearwardly of said planetary drive transmission, with loads from said planetary drive transmission being transmitted to said primary mount.

30. The assembly as recited in claim 28, wherein said planetary drive transmission is positioned radially inwardly of said flow path, and there is first and second torque frame means which extend from said ring gear means and said planetary carrier through said flow path to connect to said first and second propellors, whereby said propellors can be desirably located relative to said planetary drive transmission to provide relatively short load paths to the drive transmission, with the drive transmission having a relatively short load path to said primary mount.

31. The assembly as recited in claim 1, wherein said turbine means comprises a first compressor turbine section having a drive connection to said compressor means, and a separate free turbine section powered independently of said turbine compressor section and operatively connected through said planetary drive transmission to said propellors.

32. The assembly as recited in claim 1, wherein said turbine means comprises at least one shared load turbine section having a drive connection through said planetary drive transmission to said propellors, and also having an operative drive connection to at least a portion of said compressor means.

2. a burner means to receive air from the compressor and burn fuel therein to create a gaseous combustion product;

3. a turbine means having a turbine blade means centered on, and rotatable about, said operating axis;

c. said nacelle having a forward inlet and a rear exhaust nozzle, with said propulsion assembly defining a substantially continuous gaseous fluid flow path from said inlet through said gas generating and power section to said exhaust nozzle;

d. first and second propellers mounted for counter-rotation at a mounting location radially outward of said flow path;

e. a planetary drive transmission comprising;

1. an inner sun gear means of a relatively smaller diameter, mounted for rotation about said operating axis and operatively connected to said turbine means so as to be driven thereby;

2. a ring gear means of a relatively larger diameter, mounted for rotation relative to said support structure about said operating axis and drivingly connected to said first propeller for rotation in a first direction;

3. a planetary means comprising planetary gear means rotatable about axis means generally parallel to said operating axis and drivingly interconnected between the sun gear means and the ring gear means in a manner that rotation of said sun gear means relative to said planetary means in a first direction causes rotation of said ring gear means relative to said planetary gear means in a second direction opposite to the first direction, and further comprising planet carrier means operatively connected to the planetary gear means and rotatable about the operating axis, said planet carrier means being drivingly connected to the second propeller means for rotation in a direction opposite to the direction of rotation of the first propeller;

f. said planetary transmission being positioned at a location spaced radially from said flow path in a manner that gaseous fluid flow through said flow path can be optimized,

g. a gear box enclosing said planetary drive transmission;

h. first torque frame means interconnected between said ring gear means and said first propeller, and second torque frame means interconnected between said planet carrier means and said second propeller, said first and second propellers being axially spaced from said first and second torque frame means, respectively;

i. at least two sets of bearing means positioned at axially spaced locations within said gear box to provide bearing support for said first and second torque frame means;

whereby as said turbine section rotatably drives said sun gear, said sun gear causes relative counter-rotation of said planet carrier and said ring

4. The assembly as recited in claim 2, wherein said flow path has a flow section positioned rearwardly of said turbine means, and said first and second torque frame means extend through said flow section.

7. The assembly as recited in claim 2, wherein said flow path has a flow section positioned forwardly of said compressor means and said first and second torque frame means are connected between said ring gear means and said planetary carrier means through said flow section to connect to said first and second propellers.