STRUCTURAL PARTS AIRPLANES

Brand Owner (click to sort) Address Description
ACCORDIA MSA AIRCRAFT PRODUCTS, INC. 4330 LA JOLLA VILLAGE DR. STE. 270 SAN DIEGO CA 92122 structural parts for airplanes, namely aircraft windows;
ACCORDIA MSA AIRCRAFT PRODUCTS, LTD. 10000 IOTA DRIVE SAN ANTONIO TX 782172628 structural parts for airplanes, namely aircraft windows;
AEROKIT TYEE AIRCRAFT, INC. SNOHOMISH COUNTY AIRPORT EVERETT WA 98201 structural parts for airplanes;
FINLETS Vortex Control Technologies 3300 100th St. SW Everett WA 98204 structural parts for airplanes, namely, devices for improving drag, reducing fuel consumption, and increasing range of the airplane;
LUSCOMBE Collins, Dennis M. 950 W. Sierra Madre Azusa CA 91702 structural parts for airplanes;
MESHAGON ABEMIS 2683 Hampshire Rd, #1 Cleveland OH 44106 Structural parts for airplanes; Structural parts for ambulances; Structural parts for boats; Structural parts for buses; Structural parts for gliders; Structural parts for helicopters; Structural parts for motorcycles; Structural parts for trucks; Structural parts for vans;
NEXFLITE Kelley, Gary A. 3348 Coquina Key Drive SE St Petersburg FL 33705 Structural parts for airplanes;
SILVAIRE Collins, Dennis M. 950 W. Sierra Madre Azusa CA 91702 structural parts for airplanes;
SPRAGGINS MSA AIRCRAFT INTERIOR PRODUCTS, INC. 329 BREESPORT SAN ANTONIO TX 78216 structural parts for airplanes, namely, aircraft windows;
VORTEX CONTROL FINLETS Consulting Aviation Services, Inc. 1275 Shiloh Road, Suite 2820 Kennesaw GA 30144 structural parts for airplanes, namely, devices for improving drag, reducing fuel consumption, and increasing range of the airplane;VORTEX CONTROL;
 

Where the owner name is not linked, that owner no longer owns the brand

    
Technical Examples
  1. A device (1) for detachably connecting two abutting structural parts (2, 3) comprises a tie member (4), adapted to be at least partially inserted in a recess (5) formed in a first (2) of the structural parts (2, 3), and a locking element (6) operable to be disposed in a second (3) of the structural parts (2, 3) and to cooperate with an engagement surface (14, 45) of a rod member (10), slidably housed in a body (8) of the tie member (4), to pull the same towards the second structural part (3). The body (8) is provided with a first, expandable, portion (9) adapted to frictionally engage the recess (5) and with an engaging zone (13) cooperating with an expander region (12) of the rod member (10) operable to expand the first, expandable, portion (9) of the body (8) upon displacement of the rod member (10) relative to the same. The rod member (10) is provided with a traction portion (15) radially outwardly extending therefrom and adapted to cooperate with abutment means (16) radially formed in the body (8) of the tie member (4) at a predetermined axial distance from the engaging zone (13) to effect a substantially simultaneous displacement towards the second structural part (3) of the first, expandable, portion (9) of the body (8) of the tie member (4) and of the first structural part (2) in frictional engagement therewith.