Claims
- 1. In a 2-D nozzle of a gas-turbine engine having a C/D flap said hinge terminating in hinge ends and joining a convergent flap and a divergent flap, a varying gap seal from each of said hinge ends to proximately spaced surfaces comprising, a plurality of cups resiliently mounted to each of said hinge ends, which cups move axially on resilient means to contact said spaced surfaces across variable gaps to seal same and maintain such seal at varying flap positions and varying operating conditions of said 2-D nozzle.
- 2. The gap seal of claim 1 wherein said cup seals move axially independently to contact said spaced surfaces.
- 3. The gap seal of claim 1 wherein said cups are mounted on helical springs which in turn are mounted to each side edge of said divergent flap.
- 4. The gap seal of claim 3 wherein said cups are constrained in an enclosure mounted to a side edge of said divergent flap.
- 5. The gap seal of claim 1 wherein said convergent flap is mounted between a pair of discs and a pair of sidewalls and a pair of cup seals are independently and resiliently mounted at each end of such hinge to seal the gaps between each hinge end and one of said discs and one of said sidewalls.
- 6. The gap seal of claim 5 wherein a first cup seal engages one of said discs across a first gap and a second cup seal engages one of said sidewalls across a second gap, said second cup seal overlapping one of said discs in spaced proximity at a plurality of said flap positions.
STATEMENT OF GOVERNMENT INTEREST
The invention described herein may be manufactured and used by or for the Government for governmental purposes without the payment of any royalty thereon.
US Referenced Citations (16)
Foreign Referenced Citations (1)
Number |
Date |
Country |
722616 |
Jan 1955 |
GBX |