SU1034303A1 - POWER LOCK FOR FASTENING OF AIRCRAFT HATS - Google Patents

POWER LOCK FOR FASTENING OF AIRCRAFT HATS

Info

Publication number
SU1034303A1
SU1034303A1 SU3389822/23A SU3389822A SU1034303A1 SU 1034303 A1 SU1034303 A1 SU 1034303A1 SU 3389822/23 A SU3389822/23 A SU 3389822/23A SU 3389822 A SU3389822 A SU 3389822A SU 1034303 A1 SU1034303 A1 SU 1034303A1
Authority
SU
USSR - Soviet Union
Prior art keywords
aircraft
stops
hats
fastening
bushing
Prior art date
Application number
SU3389822/23A
Other languages
Russian (ru)
Inventor
Н.В. Банделовский
Original Assignee
Н.В. Банделовский
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Н.В. Банделовский filed Critical Н.В. Банделовский
Priority to SU3389822/23A priority Critical patent/SU1034303A1/en
Application granted granted Critical
Publication of SU1034303A1 publication Critical patent/SU1034303A1/en

Links

Landscapes

  • Clamps And Clips (AREA)

Abstract

Силовой замок для крепления люков летательного аппарата, содержащий корпус, внутри которого размещены резьбовая втулка с упорами и подпружиненный запирающий штырь с головкой, взаимодействующей с упорами, выполненными на дне стакана, установленного внутри резьбовой втулки, отличающийся тем, что, с целью повышения надежности его контровки, резьбовая втулка выполнена с продольной прорезью, упоры втулки размещены на ее внутренней поверхности, а в стакане выполнены пазы для размещения упоров втулки.Power lock for fixing the hatches of the aircraft, comprising a housing inside which a threaded bushing with stops and a spring-loaded locking pin with a head cooperating with stops at the bottom of the glass installed inside the threaded bushing, are installed, in order to increase the reliability of its lock , the threaded bushing is made with a longitudinal slit, the bushing stops are placed on its inner surface, and the grooves are made in the glass to accommodate the bushing stops.

SU3389822/23A 1982-01-25 1982-01-25 POWER LOCK FOR FASTENING OF AIRCRAFT HATS SU1034303A1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
SU3389822/23A SU1034303A1 (en) 1982-01-25 1982-01-25 POWER LOCK FOR FASTENING OF AIRCRAFT HATS

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
SU3389822/23A SU1034303A1 (en) 1982-01-25 1982-01-25 POWER LOCK FOR FASTENING OF AIRCRAFT HATS

Publications (1)

Publication Number Publication Date
SU1034303A1 true SU1034303A1 (en) 2005-05-10

Family

ID=60526194

Family Applications (1)

Application Number Title Priority Date Filing Date
SU3389822/23A SU1034303A1 (en) 1982-01-25 1982-01-25 POWER LOCK FOR FASTENING OF AIRCRAFT HATS

Country Status (1)

Country Link
SU (1) SU1034303A1 (en)

Similar Documents

Publication Publication Date Title
ATE45486T1 (en) BONE PLATE ASSEMBLY.
PT81339B (en) PROCESS FOR THE PREPARATION OF PAPALS OF PARA-ARAMIDE WITH HIGH DENSITY
ES296515Y (en) BARREL WITH PLUG
MX154661A (en) IMPROVEMENTS TO A SECURITY MECHANISM FOR WINDOWS, DOORS AND THE LIKE
DE3673967D1 (en) ARRANGEMENT FOR SAILS WITH WING PROFILE.
ES2012804B3 (en) PIGMENTS OF MODIFIED SURFACE AND METHODS TO OBTAIN THEM, AND THE ELASTOMERS THAT CONTAIN THEM.
SU1034303A1 (en) POWER LOCK FOR FASTENING OF AIRCRAFT HATS
DK447088D0 (en) PROCEDURE FOR THE IMPROVEMENT OF WELLNESS OILS, THE PRODUCTS OBTAINED AND THE USE OF THE PRODUCTS TO REPLACE LIGHT FUEL OILS AND DIESEL FUEL
ES556991A0 (en) PROVISION FOR THE PERFORMANCE OF FUNCTIONS RELATED TO PASSENGERS AND NOT A FLIGHT COMPANION ON AN AIRPLANE
BR8600488A (en) PROCESS TO RECTIFY AN INTERNAL CYLINDRICAL HOLE
IT8348699A0 (en) BLIND RIVET WITH SELF-ADJUSTING LOCKING PIN
SE8503683D0 (en) locking mechanism
SU917450A1 (en) POWER LOCK FOR FIXING THE HATCHES OF AIRCRAFT
ATE29688T1 (en) SHAVER HEAD FRAME WITH UP AND DOWN RAMPS.
SU1047073A1 (en) POWER LOCK FOR FASTENING OF AIRCRAFT HATS
SU948066A1 (en) POWER LOCK FOR FIXING THE HATCHES OF AIRCRAFT
SU978505A1 (en) POWER LOCK FOR FIXING THE HATCHES OF AIRCRAFT
ES548736A0 (en) PROCEDURE WITH ITS CORRESPONDING DEVICE FOR DRY COKE COOLING
BR8101767A (en) STRUCTURE AND PROCESS TO IMPROVE THE PERFORMANCE OF A HELICOPTER ROTOR
SU1320997A1 (en) CASTLE OF THE AIRCRAFT
BR7702649A (en) SCREWED CONNECTION AND PROCESS TO PRODUCE AN EXTERNAL THREAD MEMBER
SU844131A1 (en) Built up cutting tool
SU672789A1 (en) CUTTER PILON OF THE AIRCRAFT
SU1103953A1 (en) Composite cutting tool
SU999417A1 (en) ROCK UNIT OF AIRCRAFT UNIT