AIRPLANES STRUCTURAL PARTS

Brand Owner (click to sort) Address Description
BBJ THE BOEING COMPANY 7755 E. Marginal Way S. Seattle WA 98108 Airplanes [ and structural parts and manuals therefor ];
BOEING BUSINESS JETS THE BOEING COMPANY 7755 E. Marginal Way S. Seattle WA 98108 Airplanes [ and structural parts and manuals therefor ];BUSINESS JETS;
F/A-18E THE BOEING COMPANY 7755 E. Marginal Way S. Seattle WA 98108 airplanes [ and structural parts therefor ];
MALIBU MATRIX PIPER AIRCRAFT, INC. 2926 Piper Drive Vero Beach FL 32960 airplanes [ and structural parts therefor ];
MIRAGE PIPER AIRCRAFT, INC. 2926 Piper Drive Vero Beach FL 32960 airplanes [ and structural parts therefor ];
 

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.