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Guillaume Gallant
Guillaume Gallant, Plaisance Du Touch FR
| Patent application number | Description | Published |
|---|---|---|
| 20100032523 | AIRCRAFT FUSELAGE MADE FROM LONGITUDINAL PANELS AND METHOD OF PRODUCING SUCH A FUSELAGE - The invention relates to an aircraft fuselage comprising a nose cone, a tail section and a central section, the central section comprising longitudinal panels assembled directly with one another, at least one of these longitudinal panels having a length corresponding to the distance between the nose cone and the tail section in order to connect said nose cone with said tail section. | 02-11-2010 |
| 20100044513 | AIRCRAFT CABIN WINDOW ASSEMBLY METHOD - A method for assembling a cabin window to a bay in a side wall of an aircraft fuselage, the cabin window including an outer transparent element and at least one inner transparent element. A non-through hole is made in a portion of the side wall along the edge of the bay. Subsequently, the outer transparent element is positioned in the bay from the exterior of the fuselage. The element includes a first part which has a diameter greater than that of the bay and which is shaped to co-operate with the above mentioned portion such as to block the outer transparent element in the bay both laterally and longitudinally. A second part of the outer transparent element has a groover that projects into the fuselage. The outer transparent element and the at least one inner transparent element are welded to the fuselage using a strap which presses a seal against at least the fuselage and the inner wall of the groove. | 02-25-2010 |
| 20110017870 | SECTION OF AIRCRAFT FUSELAGE AND AIRCRAFT INCLUDING ONE SUCH SECTION - The invention relates to a section of fuselage for an aircraft, including frames and bays for receiving cabin windows. According the the disclosed embodiments, at least some of the frames include at least one frame segment that surrounds at least one bay, the frame segment having two branches that are disposed to the side of the bay. The ends of the branches are attached to each of the ends of the frame segment such as to form a Y. | 01-27-2011 |
Guillaume Gallant, Lareole FR
| Patent application number | Description | Published |
|---|---|---|
| 20100206986 | CURRENT RETURN NETWORK ELEMENT FOR AN AIRCRAFT - The invention relates to a current return network element ( | 08-19-2010 |
| 20110001006 | Process for making an aircraft having a floor - The method of fabricating an aircraft comprises the following steps: | 01-06-2011 |
| 20110001008 | Aircraft floor of optimized compactness - An aircraft floor portion includes crossmembers. Each crossmember comprises a top partial crossmember and a bottom crossmember, with at least one gap being left between the top partial crossmember and the bottom partial crossmember of each crossmember. | 01-06-2011 |
| 20110147521 | METHOD OF CONSTRUCTING A FIXED-WING AIRCRAFT - The following steps are performed in the method of constructing an aircraft: taking a subassembly comprising two wings that are rigidly fastened together, and fitting it to a fuselage wall; and fastening the subassembly to the wall by means of fastener elements that are distinct from the subassembly and that present main axes that are vertical. | 06-23-2011 |
Guillaume Gallant, Finhan FR
| Patent application number | Description | Published |
|---|---|---|
| 20100264273 | FUSELAGE STRUCTURE FOR AN AIRCRAFT FUSELAGE IN COMPOSITE MATERIAL AND AIRCRAFT EQUIPPED WITH SUCH A FUSELAGE STRUCTURE - A fuselage structure for an aircraft fuselage in composite material and an aircraft including such a fuselage structure. The fuselage structure provides savings in mass while allowing grounding of electric systems, and with which substantial mechanical stiffness characteristics may be guaranteed. In the fuselage structure attachment modules provide an assembling function as well as an electric function. | 10-21-2010 |
Guillaume Gallant, Plaisance Due Touch FR
| Patent application number | Description | Published |
|---|---|---|
| 20100200691 | DEVICE FOR ATTACHING A LIFT MEMBER TO THE FUSELAGE OF AN AIRCRAFT - The disclosed embodiments relate to an aircraft equipped with at least one device for attaching a lift member to the fuselage which includes elastic articulations whose rigidity in translation and in rotation can be adjusted axially, vertically, and transversely. An airfoil may be connected to the body of the fuselage by these elastic articulations. | 08-12-2010 |