GB734491A - Improvements in or relating to launching and landing devices for aircraft and rocket or autopropelled bodies - Google Patents
Improvements in or relating to launching and landing devices for aircraft and rocket or autopropelled bodiesInfo
- Publication number
- GB734491A GB734491A GB9062/51A GB906251A GB734491A GB 734491 A GB734491 A GB 734491A GB 9062/51 A GB9062/51 A GB 9062/51A GB 906251 A GB906251 A GB 906251A GB 734491 A GB734491 A GB 734491A
- Authority
- GB
- United Kingdom
- Prior art keywords
- aircraft
- launching
- pivots
- landing
- modification
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired
Links
- 230000004048 modification Effects 0.000 abstract 3
- 238000012986 modification Methods 0.000 abstract 3
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
- B64C29/0025—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 fixed relative to the fuselage
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F41—WEAPONS
- F41F—APPARATUS FOR LAUNCHING PROJECTILES OR MISSILES FROM BARRELS, e.g. CANNONS; LAUNCHERS FOR ROCKETS OR TORPEDOES; HARPOON GUNS
- F41F3/00—Rocket or torpedo launchers
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Transmission Devices (AREA)
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
Abstract
734,491. Launching and landing aircraft. ANDERSON, J. R. April 7, 1952 [April 18, 1951], No. 9062/51. Class 4. [Also in Group XXI] A launching or landing device for aircraft which take off and/or land vertically or substantially vertically, is provided with a member or cradle which permits freedom of angular movement of the axis of the aircraft when launching or landing. In Fig. 1, member 1 is inside the fuselage to which it is pivoted by internally projecting pivots 3. Pivots 4 attached to the member engage yokes 5 on pillars 6. Part of the latter may be. swung aside to give clearance when manoeuvring to land. In a modification the pillars consist of two pairs of telescopic legs which may be retracted into the aircraft when in flight. In Fig. 2, member 1 is outside the fuselage. In a modification, the member is a split ring, enabling the aircraft to enter laterally. In a further modification, member 1 depends from its pivots by vertical lugs and has upstanding yokes bearing pivots 4. Specifications 568,548, 612,880, 612,881 and 629,460 are referred to.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB9062/51A GB734491A (en) | 1951-04-18 | 1951-04-18 | Improvements in or relating to launching and landing devices for aircraft and rocket or autopropelled bodies |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB9062/51A GB734491A (en) | 1951-04-18 | 1951-04-18 | Improvements in or relating to launching and landing devices for aircraft and rocket or autopropelled bodies |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB734491A true GB734491A (en) | 1955-08-03 |
Family
ID=9864665
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB9062/51A Expired GB734491A (en) | 1951-04-18 | 1951-04-18 | Improvements in or relating to launching and landing devices for aircraft and rocket or autopropelled bodies |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB734491A (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE1144120B (en) * | 1959-02-24 | 1963-02-21 | Messerschmitt Boelkow Blohm | Take-off car for aircraft taking off vertically |
| CN105822425A (en) * | 2016-04-01 | 2016-08-03 | 北京航天发射技术研究所 | Load transmitting device for installation of small solid engine |
-
1951
- 1951-04-18 GB GB9062/51A patent/GB734491A/en not_active Expired
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE1144120B (en) * | 1959-02-24 | 1963-02-21 | Messerschmitt Boelkow Blohm | Take-off car for aircraft taking off vertically |
| CN105822425A (en) * | 2016-04-01 | 2016-08-03 | 北京航天发射技术研究所 | Load transmitting device for installation of small solid engine |
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