|
| GAS TURBINE ENGINE BOOSTING METHOD |
| FIELD: aviation.
EFFECT: increased thrust of gas turbine engine. 1 dwg |
| Publishing date: January 21, 2003 |
|
| PLASMA-JET ENGINE WITH CLOSED-CIRCUIT ELECTRON DRIFT |
| FIELD: space engineering; stationary plasma jet engines and anode-layer engines of electric rocket engine units.
EFFECT: enhanced reliability and service life of engine. 2 cl, 2 dwg |
| Publishing date: October 8, 2002 |
|
| METHOD FOR TREATING THE PATIENTS SUFFERING FROM INVETERATE AND RECURRENT CARCINOMA OF THE RECTUM |
| FIELD: meteorology, civil aviation.
EFFECT: increased range and diminished coarse errors in location of thunderstorms. 1 dwg |
| Publishing date: August 27, 2002 |
|
| DEVICE FOR PREVENTION OF HELICOPTER COLLISIONS WITH HIGH-VOLTAGE POWER LINES |
| FIELD: radar equipment, applicable for insurance of safety of helicopter flight at low altitudes, in particular, for warning of helicopter pilots on the danger of collisions with high-voltage power lines.
EFFECT: prevented collisions of helicopter with obstacles in the form of electric power lines. 1 dwg |
| Publishing date: March 5, 2002 |
|
| METHOD OF EMERGENCY EVACUATION OF PASSENGERS FROM AIRCRAFT |
| FIELD: rescue aids.
EFFECT: enhanced safety of passengers. 4 dwg |
| Publishing date: February 5, 2002 |
|
| ANTICORROSIVE COMPOSITION AND METHOD OF ITS APPLICATION TO METAL SURFACE |
| FIELD: metal corrosion, particularly, protection of metals from atmospheric and biological corrosion; applicable in mechanical and instrumentation engineering, and in other industries.
EFFECT: higher protective properties of coatings, simplified and low-cost process. 2 cl, 3 tbl, 1 ex |
| Publishing date: November 21, 2001 |
|
| PASSIVE TRANSCEIVER |
| FIELD: radar detection and ranging, applicable for transmission of friend-or-foe signals and identification of radar surveillance objects, applicable in air traffic control systems, systems of identification of remote objects and in other fields.
EFFECT: enhanced noise immunity of identification information due to transmission of reply signals at the carrier frequency differing from the interrogation signal frequency. 4 dwg |
| Publishing date: November 14, 2001 |
|
| COATING ON METAL AND METHOD OF FORMING THEREOF |
| FIELD: chemical industry.
EFFECT: improved service characteristics of compositions for coating having better consumer properties of said compositions and shorter duration and lower power intensiveness for forming thereof. 4 cl, 1 tbl |
| Publishing date: October 17, 2001 |
|
| COMPOSITION FOR PROTECTING CORRODED METALLIC SURFACES |
| FIELD: composition for anticorrosion coatings for protection of corroded surface of products and structures made of ferrous metals operating in atmospheric conditions of various climatic zones, in atmosphere containing aggressive gases and vapors under conditions of increased humidity.
EFFECT: improved properties of the composition. 2 cl, 6 ex, 3 tbl |
| Publishing date: October 17, 2001 |
|
| DETERGENT COMPOSITION FOR REMOVING SCALE |
| FIELD: domestic chemistry, more particularly removing scale from metallic surfaces of heat-exchange devices, coiled pipes and other structural members of heat and power engineering systems, e.g. removing scale from internal walls of radiators of cooling system of internal combustion engines.
EFFECT: improved properties of the detergent composition. 2 cl, 1 tbl |
| Publishing date: September 19, 2001 |
|
| HERMETICALLY SEALED CONNECTOR |
| FIELD: radio and electronic engineering; aerospace equipment.
EFFECT: enlarged operating temperature range, enhanced strength, improved reliability of sealing. 2 dwg, 1 tbl, 2 ex |
| Publishing date: August 29, 2001 |
|
| HELMET TARGET INDICATION SYSTEM |
| FIELD: optoelectron instrumentation.
EFFECT: enhanced accuracy characteristics of video signal and quick response of system. 3 cl, 3 dwg
|
| Publishing date: June 26, 2001 |
|
| A METHOD OF AND INSTALLATION FOR TRAINING FLIGHTS |
| The newly-patented training flight installation consists of: an actual aircraft with its controls, aggregates and systems; simulators of the controls activation of which might cause equipment breaks and system failure and accidentally start-up the engine; aircraft automatic control system with a device to actuate power installation controls they are connected with. |
| Publishing date: October 23, 2000 |
|
Aircraft
