FIELD: electrical equipment. SUBSTANCE: method involves fitting of coiled metal Bowden wire onto radiation-modified thermosetting sleeve with one more radiation-modified sleeve placed overall. EFFECT: improved reliability of harness protection against mechanical thrusts on movable sections, reduced weight of protective means as compared to those of harnesses in Bowden cables, eliminated danger of seizure between harness and Bowden cable turns. 1 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| AIRCRAFT AERODYNAMIC SURFACE | 1992 |
|
RU2032278C1 |
| CRYOGENIC PROPELLANT FILLING SYSTEM FOR FLYING VEHICLE | 1991 |
|
RU2034753C1 |
| DETACHABLE DEVICE FOR FILLING WITH CRYOGENIC PROPELLANT | 1991 |
|
RU2042582C1 |
| METHOD FOR FORMATION OF COUNTERSUNK RIVETED JOINT | 1994 |
|
RU2066582C1 |
| FLYING VEHICLE RAMJET ENGINE | 1992 |
|
RU2104227C1 |
| SYSTEM FOR CONTROL OF FREIGHT DROPPING FROM AIRCRAFT CARGO COMPARTMENT | 1990 |
|
RU1795626C |
| SEAT | 1995 |
|
RU2136517C1 |
| AUTOMOBILE SEAT | 1995 |
|
RU2136518C1 |
| ENGINE | 1992 |
|
RU2066777C1 |
| MAIN UNDERCARRIAGE UNIT OF FLYING VEHICLE | 1990 |
|
RU1827993C |
