Claims
- 1. A flap-type two-dimensional plug nozzle having a rectangular inlet, fixed sides extending rearwardly from each side of said inlet, a pivotally mounted top flap, said pivotally mounted top flap being pivotally mounted between its ends about a first fixed pivotal axis extending between said fixed sides, a pivotally mounted bottom flap, said pivotally mounted bottom flap being pivotally mounted between its ends about a second fixed pivotal axis extending between said fixed sides, the rear ends of said top and bottom flaps along with said fixed sides forming the exit area, plug means centered between said pivotally mounted top flap and said pivotally mounted bottom flap, a first throat plane being formed between said plug means and said top flap, a second throat plane being formed between said plug means and said bottom flap, said top flap forming a convergent-divergent passage with said plug means, said bottom flap forming a convergent-divergent passage with said plug means, said first and second throat planes being located downstream of said first and second pivotal axes, respectively, to provide an increase in nozzle area ratio as throat area at the throat plane increases.
- 2. A nozzle as set forth in claim 1 wherein the rear part of the plug means is pivoted to deflect the exhaust gases away from the nozzle centerline.
- 3. A nozzle as set forth in claim 1 wherein a balance flap is hinged to each flap upstream of the flap pivot to offset pressure forces on the portion of the flap downstream of its pivot, thereby minimizing the actuation force required to move the flap system to control throat area.
- 4. A nozzle as set forth in claim 1 wherein the plug means is pivoted about its upstream end to deflect the exhaust gases away from the nozzle centerline.
- 5. A two dimensional plug nozzle as in claim 1 wherein the flaps can be rotated past their normal minimum throat area position such that the downstream ends of said flaps come in contact with the plug means thereby blocking flow through the nozzle.
- 6. A nozzle as set forth in claim 1 wherein side walls extend from the ends of said fixed sides along each end of the plug means to channel flow thereover.
- 7. A nozzle as set forth in claim 6 wherein the rear part of the plug means is pivoted to deflect the exhaust gases away from the nozzle centerline, the side walls on the rear part of the plug means being pivoted to move therewith.
- 8. A nozzle as set forth in claim 3 wherein said rectangular inlet has a short upper wall member extending rearwardly from the top thereof and a short lower wall extending rearwardly from the bottom thereof, the forward end of the balance flap hinged to the top flap is slideably mounted adjacent the short upper wall member, the forward end of the balance flap hinged to the bottom flap is slideably mounted adjacent the short lower wall member.
- 9. A flap-type two-dimensional plug nozzle having a rectangular inlet, fixed sides extending rearwardly from each side of said inlet, a pivotally mounted single top flap, said top flap having a continuous inner surface, said top flap being pivotally mounted between its ends about a first fixed pivotal axis extending between said fixed sides, a pivotally mounted bottom flap, said bottom flap having a continuous solid inner surface, said flap being pivotally mounted between its ends about a second fixed pivotal axis extending between said fixed sides, the rear ends of said top and bottom flaps along with said fixed sides forming the exit area, plug means centered between said inner surface of said top flap and said inner surface of said bottom flap, a first throat plane being formed between said plug means and the surface of said top flap, a second throat plane being formed between said plug means and the surface of said bottom flap, the surface of said top flap forming a convergent-divergent passage with said plug means, the surface of said bottom flap forming a convergent-divergent passage with said plug means, said first and second throat planes being located downstream of said first and second pivotal axes.
Government Interests
The invention herein described was made in the course of or under a contract or subcontract with the Department of the Air Force.
US Referenced Citations (6)