BE407576A - - Google Patents
Info
- Publication number
- BE407576A BE407576A BE407576DA BE407576A BE 407576 A BE407576 A BE 407576A BE 407576D A BE407576D A BE 407576DA BE 407576 A BE407576 A BE 407576A
- Authority
- BE
- Belgium
- Prior art keywords
- tilting
- airplanes
- piston
- pilot
- controlled
- Prior art date
Links
- 239000012530 fluid Substances 0.000 claims description 9
- 238000005192 partition Methods 0.000 claims description 3
- 230000000750 progressive effect Effects 0.000 claims description 3
- 230000000694 effects Effects 0.000 claims 1
- 230000004048 modification Effects 0.000 claims 1
- 238000012986 modification Methods 0.000 claims 1
- 238000006073 displacement reaction Methods 0.000 description 4
- 241000209140 Triticum Species 0.000 description 1
- 235000021307 Triticum Nutrition 0.000 description 1
- 230000036461 convulsion Effects 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 239000011259 mixed solution Substances 0.000 description 1
- 210000000056 organ Anatomy 0.000 description 1
- 230000002035 prolonged effect Effects 0.000 description 1
- 239000000243 solution Substances 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C29/00—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft
- B64C29/0008—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded
- B64C29/0016—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded the lift during taking-off being created by free or ducted propellers or by blowers
- B64C29/0033—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded the lift during taking-off being created by free or ducted propellers or by blowers the propellers being tiltable relative to the fuselage
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/22—Compound rotorcraft, i.e. aircraft using in flight the features of both aeroplane and rotorcraft
- B64C27/28—Compound rotorcraft, i.e. aircraft using in flight the features of both aeroplane and rotorcraft with forward-propulsion propellers pivotable to act as lifting rotors
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- Toys (AREA)
Publications (1)
| Publication Number | Publication Date |
|---|---|
| BE407576A true BE407576A (de) |
Family
ID=72328
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| BE407576D BE407576A (de) |
Country Status (1)
| Country | Link |
|---|---|
| BE (1) | BE407576A (de) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP3140190A4 (de) * | 2014-05-07 | 2018-01-17 | Xti Aircraft Company | Senkrechtstart- und -landeflugzeug |
-
0
- BE BE407576D patent/BE407576A/fr unknown
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP3140190A4 (de) * | 2014-05-07 | 2018-01-17 | Xti Aircraft Company | Senkrechtstart- und -landeflugzeug |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CA2705655C (fr) | Procede de controle en lacet d'un helicoptere hybride, et helicoptere hybride muni d'un dispositif de commande en lacet apte a mettre en oeuvre ledit procede | |
| EP0234157B1 (de) | Umlaufender Dämpfer | |
| EP0304599B1 (de) | Mit Mitteln zur Änderung der Dämpfungscharakteristik ausgerüsteter hydraulischer Stossdämpfer | |
| WO2015055434A1 (fr) | Dispositif de commande de vol d'un aéronef | |
| FR3050385A1 (fr) | Drone comportant au moins trois rotors de sustentation et de propulsion | |
| FR2686857A1 (fr) | Amortisseur de jambe de train d'atterrissage d'aeronef. | |
| EP1348623A1 (de) | Drehflüglerrotor mit homokinetischem Gelenk mit leistungsverzweigender Differentialwirkung | |
| CA2914331C (fr) | Rotor arriere de giravion, giravion equipe d'un tel rotor arriere et procede d'equilibrage statique et/ou dynamique d'un rotor arriere de giravion | |
| FR2685902A1 (fr) | Amortisseur de train d'atterrissage d'aeronef. | |
| EP0289374A1 (de) | Kombinierte Lagervorrichtung eines Drehflügelflugzeugrotors und damit ausgerüsteter Rotor | |
| EP0086490A1 (de) | Rotor mit doppeltem Zug-/Torsions-Verbindungselement | |
| EP3297911A1 (de) | Drohne mit verstellbarem rotor | |
| EP0359624B1 (de) | Blattverstelleinzelsteuervorrichtung mit drehbaren Linearzylindern | |
| FR2769284A1 (fr) | Dispositif de commande d'une surface aerodynamique de direction d'un helicoptere | |
| EP0200244B1 (de) | Kupplungsvorrichtung für eine Umhüllung und einen Bestandteil ausserhalb dieser Umhüllung | |
| FR2764008A1 (fr) | Servoactionneur electrohydrostatique de plateforme mobile suspendue | |
| EP0191674A1 (de) | Druckflüssigkeitsmechanismus mit Rotor | |
| FR3022217A1 (fr) | Aeronef convertible a aile basculante | |
| FR2636594A1 (fr) | Dispositif de commande de pas monocyclique en repere fixe et multicyclique en repere tournant, pour pales de rotors de giravions | |
| RU2303559C2 (ru) | Летательный аппарат тяжелее воздуха с вертикальным взлетом и посадкой с винтонесущими гондолами, имеющими возможность свободного поворота на 90° под управлением демпфирующих устройств | |
| US1972486A (en) | Variable pitch propeller mechanism | |
| FR2775654A1 (fr) | Perfectionnements aux pales de rotor a volet orientable | |
| FR3037922A1 (fr) | Dispositif de regulation d'une helice a pales a calage variable d'un turbopropulseur | |
| FR2831933A1 (fr) | Boite de transmission basculante a liaison pivotante a paliers lisses | |
| US2761521A (en) | Helicopter rotor control mechanism |