Accès libre

Design Method for Pressurised and Non-Pressurised Tail Cargo Door’s Fairings Compartment in Transport Category Aircraft

Oleksandr Grebenikov
Oleksandr Grebenikov
, 
Andrii Humennyi
Andrii Humennyi
, 
Vasyl Loginov
Vasyl Loginov
, 
Olexandr Dveirin
Olexandr Dveirin
 et 
Dmytro Konyshev
Dmytro Konyshev
   | 13 sept. 2023
Transactions on Aerospace Research's Cover Image
À propos de cet article
Article précédent
Article suivant
Citez
Article Category: Research Article
Publié en ligne: 13 sept. 2023
Pages: 55 - 71
Reçu: 22 déc. 2021
Accepté: 06 juil. 2023
DOI: https://doi.org/10.2478/tar-2023-0017
Mots clés
© 2023 Oleksandr Grebenikov et al., published by Sciendo
This work is licensed under the Creative Commons Attribution-NonCommercial-NoDerivatives 4.0 International License.

Figure 1.

Options for the loads arrangement in the cargo compartment for transportation in containers and on standard aircraft pallets.
Options for the loads arrangement in the cargo compartment for transportation in containers and on standard aircraft pallets.

Figure 2.

Schemes for loading cargo in containers and on standard aircraft pallets.
Schemes for loading cargo in containers and on standard aircraft pallets.

Figure 3.

Sections of the cargo compartment in the zone of the fuselage single curvature (a – regular fuselage cross-section; b – fuselage cross section in the wing area).
Sections of the cargo compartment in the zone of the fuselage single curvature (a – regular fuselage cross-section; b – fuselage cross section in the wing area).

Figure 4.

Scheme for determining the length of the sloped floor and the nodes of the ramp hinge. FRP, fuselage reference plane.
Scheme for determining the length of the sloped floor and the nodes of the ramp hinge. FRP, fuselage reference plane.

Figure 5.

General view of a pressurisated fairing compartment. FRP, fuselage reference plane; FSP, fuselage symmetry plane.
General view of a pressurisated fairing compartment. FRP, fuselage reference plane; FSP, fuselage symmetry plane.

Figure 6.

Sectional view of a pressurisated fairing compartment.
Sectional view of a pressurisated fairing compartment.

Figure 7.

Fairing closed position lock. FTC, fuselage theoretical contour.
Fairing closed position lock. FTC, fuselage theoretical contour.

Figure 8.

Main view of fuselage tail part with non-pressurisated fairing compartment. FRP, fuselage reference plane; SRP, stabiliser reference plane.
Main view of fuselage tail part with non-pressurisated fairing compartment. FRP, fuselage reference plane; SRP, stabiliser reference plane.

Figure 9.

Main and bottom view of non-pressurisated fairing compartment. FRP, fuselage reference plane; FTC, fuselage theoretical contour; FSP, fuselage symmetry plane.
Main and bottom view of non-pressurisated fairing compartment. FRP, fuselage reference plane; FTC, fuselage theoretical contour; FSP, fuselage symmetry plane.

Figure 10.

Sectional view of non-pressurisated fairing compartment. FRP, fuselage reference plane.
Sectional view of non-pressurisated fairing compartment. FRP, fuselage reference plane.

Figure 11.

Profiling of the cutouts for the side flaps hinge nodes and determination of the cut of the fairing compartment tail section. FRP, fuselage reference plane; FTC, fuselage theoretical contour.
Profiling of the cutouts for the side flaps hinge nodes and determination of the cut of the fairing compartment tail section. FRP, fuselage reference plane; FTC, fuselage theoretical contour.

Figure 12.

Side flaps catchers location. FRP, fuselage reference plane.
Side flaps catchers location. FRP, fuselage reference plane.

Figure 13.

Sectional view of the side flaps. FRP, fuselage reference plane; FTC, fuselage theoretical contour.
Sectional view of the side flaps. FRP, fuselage reference plane; FTC, fuselage theoretical contour.

Figure 14.

Central fairing controlling. (10 – carrier; 20 – carrier bracket; 30 – rear hitch assembly; 40 – rail.) FRP, fuselage reference plane; SRP, stabiliser reference plane.
Central fairing controlling. (10 – carrier; 20 – carrier bracket; 30 – rear hitch assembly; 40 – rail.) FRP, fuselage reference plane; SRP, stabiliser reference plane.

Figure 15.

Central fairing in the open position. FTC, fuselage theoretical contour.
Central fairing in the open position. FTC, fuselage theoretical contour.

Figure 16.

Fairing compartment of a double-deck fuselage. FRP, fuselage reference plane; FTC, fuselage theoretical contour.
Fairing compartment of a double-deck fuselage. FRP, fuselage reference plane; FTC, fuselage theoretical contour.

Figure 17.

Sectional view of the double-deck fuselage fairing compartment. FRP, fuselage reference plane; FTC, fuselage theoretical contour.
Sectional view of the double-deck fuselage fairing compartment. FRP, fuselage reference plane; FTC, fuselage theoretical contour.

Figure 18.

Cargo door pressurised and non-pressurised fairing compartment.
Cargo door pressurised and non-pressurised fairing compartment.

Transported loads nomenclature.

Transported loads Quantity Weight, tones.
Soldiers, people 90 10.8
Paratroopers, people 70 8.3
Injured on stretchers + on chairs, people 48 + 15 6.0
Containers, inch (m):
M1 96″ × 96″ × 125″ (2,438 × 2,438 × 3,175) 4 18.0
M2 96″ × 96″ × 238.5″ (2,438 × 2,438 × 6,058) 2 18.0
M3 88″ × 96″ × 125″ (2,235 × 2,438 × 3,175) 4 18.0
ID 96″ × 96″ × 117.8″ (2,438 × 2,438 × 2,991) 2 18.0
1C 96″ × 96″ × 238.5″ (2,438 × 2,438 × 6,058) 2 18.0
Pallets, inch (m):
88″ × 108″ (2,235 × 2,743) 5 18.0
88″ × 108″ (2,235 × 3,175) 4 18.0
88″ × 108″ (2,438 × 3,175) 4 18.0
88″ × 108″ (2,438 × 6,058) 2 18.0
eISSN:
2545-2835
Langue:
Anglais
Périodicité:
4 fois par an
Sujets de la revue:
Engineering, Introductions and Overviews, other, Geosciences, Materials Sciences, Physics
RSS Feed de la revue