FIELD: aircraft engineering.
SUBSTANCE: inflight measurements are used to define magnitude Rn.p. of ideal engine thrust as Rn.p.=Rcn.p.-GAVF, where Rcn.p. is conventional thrust of jet nozzle corresponding to full expansion of exhaust jet therein to barometric pressure, GA air flow rate at engine inlet, VF is aircraft flight velocity. In diagnostics, engine thrust is controlled by departure of Rn.p from reference value corresponding to engine thrust prior to engine operation.
EFFECT: higher accuracy of diagnostics.
1 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| METHOD OF DETERMINING THRUST IN FLIGHT OF BYPASS TURBOJET ENGINE WITH MIXING OF FLOWS | 2015 |
|
RU2596413C1 |
| METHOD OF AVIATION BYPASS TURBOJET ENGINE WITH FLOWS MIXING IN-FLIGHT DIAGNOSTICS | 2016 |
|
RU2649715C1 |
| CONTROL METHOD OF TURBOJET TWO-CIRCUIT ENGINE | 2018 |
|
RU2692189C1 |
| METHOD OF FLIGHT DIAGNOSTICS OF UNITS OF TURBOFAN ENGINE WITH FLOW MIXING | 2017 |
|
RU2665142C1 |
| CONTROL METHOD OF JET TURBINE DOUBLE-FLOW ENGINE WITH AFTERBURNER | 2011 |
|
RU2464437C1 |
| TEST BENCH FOR GAS GENERATOR OF TURBOJET BY-PASS ENGINE | 2020 |
|
RU2739168C1 |
| GAS LIQUID JET ENGINE | 2007 |
|
RU2343301C2 |
| DOUBLE-FLOW JET TURBINE ENGINE | 2019 |
|
RU2701034C1 |
| BENCH FOR AUTOMATED TESTING OF THE GAS GENERATOR OF A BY-PASS TURBOJET ENGINE | 2022 |
|
RU2797897C1 |
| BYPASS TURBOJET ENGINE | 2017 |
|
RU2661427C1 |
