FIELD: transport.
SUBSTANCE: invention relates to controlled in-flight aircraft fuelling units. When taper is stabilised in its three perpendicular axes of symmetry the jets are blown out the intensity of which is set as linear function of speed and taper displacement in corresponding direction. To determine these parameters accelerometers in two mutually perpendicular planes and microprocessor are installed. The microprocessor calculates from measured by accelerometers accelerations the time-dependent taper speed and displacement from which it determines reactive forces of jets in two mutually perpendicular planes, which forces are needed to correct taper position. According to values of these forces the microprocessor gives signal to change jet parameters.
EFFECT: fuelling unit taper stabilisation.
| Title | Year | Author | Number |
|---|---|---|---|
| IN-FLIGHT FUELING UNIT TAPER GAGE | 2012 |
|
RU2490179C1 |
| DEVICE TO DETECT FORCE ACTING ON TIRE | 2008 |
|
RU2423246C1 |
| AIR SPEED VECTOR TRANSDUCER | 0 |
|
SU1693554A1 |
| METHOD FOR SYNCHRONISATION OF RADIO COMMUNICATION SYSTEM DISTRIBUTED IN RADIO COMMUNICATION CELLS | 2004 |
|
RU2368102C2 |
| METHOD OF DETERMINING COORDINATES OF RADIO-FREQUENCY RADIATION SOURCE ONBOARD AIRCRAFT | 2012 |
|
RU2510618C2 |
| METHOD FOR SYNCHRONISATION OF RADIO COMMUNICATION SYSTEM DISTRIBUTED IN RADIO COMMUNICATION CELLS | 2009 |
|
RU2447617C2 |
| DEVICE FOR CONTROL OVER VEHICLE, VEHICLE AND METHOD FOR ITS CONTROL | 2012 |
|
RU2570996C1 |
| DEFINITION METHOD OF CONTENT OF EFFECTIVE COMPONENT IN IMPLODED MOUNTAIN MASS AT ITS EXCAVATION AT MOTIONS | 2008 |
|
RU2386032C1 |
| METHOD OF GROUND OR WATER SURFACE LAUNCH OF ROCKET WITH CONTROL SYSTEM AND DEVICE FOR ITS REALIZATION | 1996 |
|
RU2096721C1 |
| ACTIVE VIBROPROTECTION PANEL (BOX) WITH ACCELEROMETRE TILT SIGNAL COMPENSATION IN STATIONARY CONDITIONS AND VEHICLES | 2006 |
|
RU2337390C2 |
