Hollow nozzle-actuating ring

Hollow nozzle-actuating ring

  • CN 1,234,850 A
  • Filed: 11/04/1996
  • Published: 11/10/1999
  • Est. Priority Date: 11/04/1996
  • Status: Abandoned Application
First Claim
Patent Images

1. hollow actuating ring (86) that is used for rotating synchronously aircraft combustion gas turbine jet pipe (14), this actuating ring (86) comprising:

  • A general toroidal hollow unit, it has axially spaced antetheca (110) and rear wall (114);

    Between above-mentioned front and rear wall (110 and

         114), axially extend and be connected support (118) what they structurally coupled together;

    An actuating ring intensifier (124), be used for reducing described connection support in the front and rear wall (110 and

         114) between (118) actuating ring of at least one effectively crooked with reverse length L.

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