braced strut造句

• Long braced struts also connected the transmission units to the rear fuselage forward of the fin.
• The V-form bracing struts linked the extremes of these panels to the lower fuselage.
• Single bracing struts run forward from the wheel mountings to the lower longerons forward of the wings.
• On each side a forward leaning bracing strut runs from the lower rear cabin to the front wing spar.
• The single thick struts were replaced with more conventional parallel wire braced struts and the landing gear was lengthened.
• A diameter propeller rotated over the wing behind the rear bracing strut within the inner section of the wing.
• So until the 1930s most wings were too lightweight to have enough strength and external bracing struts and wires were added.
• They were temporarily grounded in July of that year because of severe vibration, being modified with additional interplane bracing struts.
• Each had a fixed tailwheel undercarriage with the two outboard engined slung from the supporting bracing struts to the high wing.
• So until the 1930s most wings were too light weight to have enough strength and external bracing struts and wires were added.
• The two engines, Lorraine 8Bd V-8s on production aircraft, were mounted between the wings using vee bracing struts.
• The wings had steel spars and were mounted on the top of the fuselage, with pairs of bracing struts to the chines.
• Following the storm two diagonal bracing struts were added to give the telescope greater rigidity when parked in the zenith to ride out storms.
• Two of the three Renard Type 120, five-cylinder radial engines were mounted on frames below the wing within the bracing struts.
• The wide track undercarriage had a single vertical long travel leg on each side to the main spar, with a small bracing strut forward.
• The AL 3's elderly track undercarriage seen from ahead formed a splayed M-form set of rigid, longitudinally wire braced struts.
• Its slightly swept-back wing was attached to the fuselage by bracing struts, its two floats were braced to both the wing and fuselage.
• The most visible difference between the HH-53B and HH-53C was that the HH-53C dispensed with the fuel-tank bracing struts.
• The legs were mounted at the end of the centre section, each with a rearward strut and a long bracing strut outwards to the main spar.
• A second AL 5, built to order, had its first flight on 11 September 1935 Its revised undercarriage had extra diagonal cross-bracing struts.