Examples of 'fuselage section' in a sentence

Meaning of "fuselage section"

Fuselage section: A specific part of an aircraft's main body where passengers, cargo, or fuel are stored. It is used in aviation and engineering when discussing the structure and components of an airplane

How to use "fuselage section" in a sentence

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fuselage section
The fuselage section can be one composite fuselage section.
The mandrel provides the basic shape of a fuselage section.
The aircraft fuselage section comprises an outside and an inside.
The two engines are located next to the rear fuselage section.
Evolutional fuselage section.
The aft fuselage section was raised the following day and the forward section shortly after.
The test barrel is representative of the main fuselage section of the upcoming CSeries aircraft.
The centre fuselage section was badly burned in a post crash fire.
The pressure bulkhead may be directly attached to the fuselage section at the intersection line.
An aircraft fuselage section typically is in the form of a substantially cylindrical shell.
The inspector observed leaked fuel below the fuselage section where the fuel tank was mounted.
The fuselage section is a slightly rounded rectangle, higher than it is wide.
Aircraft fuselage section.
The fuselage section integrates the cockpit, radar sections and avionics bay.
In some methods, the tabs may be integral with the first fuselage section.

See also

Slide the joined front fuselage section onto the integral chassis rails.
Therein, the virtual intersection line extends on the inner surface of the fuselage section.
Replica of the fuselage section on display at IWM London.
Moreover, the intersection line may extend on the inner surface of the fuselage section.
FIG . 3 shows a fuselage section for an aircraft according to a particular embodiment of the disclosed embodiments.
Of course, the junction element may comprise a ferrule instead of the adjacent fuselage section part.
BAE Systems manufactures the type 's aft fuselage section at its Samlesbury site in northwest England.
The line is a three-dimensional curve extending parallel to the inner surface of the fuselage section.
At least one fuselage section according to one of claims 5 to 7.
Furthermore the invention relates to a method for manufacturing a one-piece composite aircraft fuselage section.
An aircraft, comprising at least one fuselage section according to claim 9.
However, the pressure bulkhead is adapted to effectively transmit pressure loads into the fuselage section.
First fuselage section 1 a is connected to a second fuselage section 1 b by junction means 6.
The light attack aircraft comes with multiple hard-points under the fuselage section and wings.
Fuselage section comprising,.
An example of a process for attaching composite stringers to a fuselage section is illustrated in FIG . 2.
The side wall 21 of the fuselage section includes an opening on which a window 11 is mounted.
Titanium matrix composites were used by McDonnell Douglas to create a representative fuselage section called " Task D.
The stiffening elements of the fuselage section further include frames 10 and stringers 19.
Consequently, a portion of this stiffener element 5 a thus is situated at second fuselage section 2 b.
After the war, only the fuselage section remained, without the wings or tail.
A cargo hold 2, situated on the inside of a fuselage 3, transports a fuselage section 4 of a secondary aircraft.
By way of example, the fuselage section 10 comprises one hundred and sixty structural elements.
In other embodiments the mid-fuselage barrel 100 is a cured single barrel fuselage section.
FIG . 1 shows a fuselage section in perspective according to the prior state of the art ;.
These windows 11 are aligned and regularly spaced along the longitudinal axis 12 of the fuselage section.
FIG . 1 schematically shows the partial view of a fuselage section of the prior art aircraft ;.
FIGS . 3 and 4 show a set of fuselage elements assembled with each other to form a fuselage section.
The fuselage section includes frames 10 and windows 11 mounted on openings.
FIG . 2 is an illustration of a perspective view of a barrel-shaped fuselage section for an aircraft.
The fuselage section 32 also comprises two beams 39 separated from said inner reticular structure 53.
Stiffener element 5 a extends beyond free edge 7 of skin 3 a of first fuselage section 2 a by a predetermined length L.
The IL-78M variant is fitted with an additional freight hold tank on the fuselage section.
FIG . 5 schematically shows the fuselage section of FIG . 3 as a front view ;.
FIG . 11 shows a seventh embodiment in which the junction element comprises an adjacent fuselage section part.

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