Blocker door actuation system

• US 4,275,560 A
• Filed: 12/27/1978
• Issued: 06/30/1981
• Est. Priority Date: 12/27/1978
• Status: Expired due to Term

• Current Assignee: General Electric Company
• Original Assignee: General Electric Company
• Inventors: Snow, Barton H., Wright, Jack D.
• Primary Examiner(s): Garrett, Robert E.
• Assistant Examiner(s): Cronmiller, Rae
• Application Number:
  US05/973,765
• Time in Patent Office: 916 Days
• Field of Search: 60/226 B, 415/148
• US Class Current: 60/226.3
• CPC Class Codes: F02K 3/075 controlling flow ratio between flows
• CPC Class Codes: Y02T 50/60 Efficient propulsion technologies, e.g. for aircraft

Abstract

The angle of the variable blocker door vanes in the bypass duct of a turbofan engine is varied in response to the angle of the variable compressor vanes of the engine. A cam and linkage assembly interconnect the blocker doors with the actuation system of the variable stator vanes such that as the angle of the stator vanes is modulated through a first predetermined range, the angle of the blocker doors is modulated through a second predetermined range.

Claims

1. An improved turbofan engine of the type having a core with variable stators, a fan, a duct for bypassing a portion of the fan flow around the core, and a plurality of blocker doors in the duct for selectively blocking the flow of air in the duct, wherein the improvement comprises:

(a) stator actuator means for selectively varying the angle of the variable stator vanes in response to a predetermined engine parameter, said stator actuator means including at least one linear actuator located radially outside of said duct and at least one rotatable shaft passing through said duct and linked to said linear actuator for transmitting movement therefrom;

(b) blocker door actuator means for selectively varying the angle of the blocking doors as a function of the variable stator vane angle, said blocker door actuator means including an actuator ring and a plurality of lever arms attached at their one end to said actuator ring and at their other ends to the blocker doors;

(c) linkage means interconnecting said stator actuation means and said blocker door actuator means such that when the angle of the variable stator vanes is varied within a first predetermined range, the angle of the blocker doors is varied within a second predetermined range, said linkage means including a cam element which is rotated by said stator actuator means and a cam follower with an attached bellcrank which is rotated during rotation of said cam through a predetermined angle range, said linkage means including a drag link connecting said bellcrank to said actuator ring for transmitting rotation movement by said cam element with said drag link being connected to said bellcrank and to said actuator ring through a pair of uniball connections for accommodating axial movement.

2. An improved turbofan engine, as set forth in claim 1, wherein said first predetermined range is substantially less than said second predetermined range.

3. An improved turbofan engine, as set forth in claim 1, wherein the angle of the variable stator vanes is varied in response to core speed.

4. An improved turbofan engine, as set forth in claim 3, wherein the angle of said variable stator vanes is scheduled such that the vanes are in the most open position when the core speed is substantially 100%.

5. An improved turbofan engine, as set forth in claim 3, wherein said blocker doors are in their most open position when the core speed is substantially 75%.

6. An improved turbofan engine, as set forth in claim 3, wherein said blocker doors are in their most closed position when the core speed is substantially 40%.