Gas turbine engine powerplant with flow control devices

• US 4,716,724 A
• Filed: 02/03/1987
• Issued: 01/05/1988
• Est. Priority Date: 04/25/1986
• Status: Expired due to Fees

• Current Assignee: Rolls-Royce PLC (Rolls-Royce Holdings Plc)
• Original Assignee: Rolls-Royce PLC (Rolls-Royce Holdings Plc)
• Inventors: Newton, Arnold C.
• Primary Examiner(s): Casaregola, Louis J.
• Assistant Examiner(s): Stout, Donald E.
• Application Number:
  US07/010,493
• Time in Patent Office: 336 Days
• Field of Search: 60/226.2, 60/229, 60/230, 60/232, 60/262, 60/242, 60/271, 239/265.31, 239/265.29, 239/265.33, 244/110 B
• US Class Current: 60/226.2
• CPC Class Codes: F02K 1/1261 of one series of flaps hinged at their upstream ends on a substantially axially movable structure
• CPC Class Codes: F02K 1/72 the aft end of the fan housing being movable to uncover openings in the fan housing for the reversed flow

Abstract

In a gas turbine engine powerplant which has a requirement for both nozzle outlet area variation and thrust reversal, there is provided a common actuating means in the form of rams which firstly move a cowl portion so as to open a radial gap and thereby effectively increase the nozzle outlet area, and secondly move reverser cascades in a downstream direction into the gap created by moving the cowl portion. A lost motion device is fitted so as to enable achieving of the former movement without affecting the latter movement until such time as the latter movement is also required.

Claims

1. A gas turbine engine powerplant including a streamlined casing, a portion of which is translatable axially of the powerplant and the fixed remainder of which contains translatable reverser cascade means and common means for moving both the translatable portion through a first predetermined distance to open a gap of a selected axial dimension in the streamlined casing without moving said translatable reverser cascades and for moving both said portion and said translatable cascades through a second selected distance so as to enlarge said gap, said common means comprising ram mechanisms which are equi-angularly spaced around the interior of said streamlined casing, and connected via rods in series with said translatable cascades and said translatable portion and including lost motion means so as to initially enable translation of said portion without translating said cascades as said portion is moved through said first distance to open said gap, said lost motion means comprising ram rods passing through said cascades in close sliding relationship, said ram rods having free ends fixed to the upstream end of said translatable portion, each said ram rod having a fixed collar thereon in spaced relationship with and upstream of a respective cascade a distance equal to said selected first distance.

2. A gas turbine engine powerplant as claimed in claim 1 wherein said collars are fixed on said ram rods so as to engage said respective reverser cascades to move said reverser cascades through said selected second distance into said gap.

3. A gas turbine engine powerplant as claimed in claim 1 comprising a core gas generator and a fan stage which is driven by the said core gas generator and projects radially outwardly thereof, and wherein the streamlined casing comprises a fan cowl which surrounds the fan stage.