GB107050A - - Google Patents
Info
- Publication number
- GB107050A GB107050A GB107050DA GB107050A GB 107050 A GB107050 A GB 107050A GB 107050D A GB107050D A GB 107050DA GB 107050 A GB107050 A GB 107050A
- Authority
- GB
- United Kingdom
- Prior art keywords
- cushion
- wheel
- aircraft
- secured
- rim
- 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.)
- Active
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64B—LIGHTER-THAN AIR AIRCRAFT
- B64B1/00—Lighter-than-air aircraft
- B64B1/005—Arrangements for landing or taking-off, e.g. alighting gear
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Fluid-Damping Devices (AREA)
Abstract
107,050. Sloper, T. June 12, 1916. Pneumatic springs.-Relates to means for mounting air-cushions for aircraft of the kind described in Specification 105,977. According to the invention, the air cushion is rotatably mounted on a support, the axis of rotation being perpendicular to the side of the cushion whereby it is secured to the support. As shown in Fig. 1, the plate A<2> of the cushion A is provided with a hollow spindle B rotatably mounted in the hub C of a wire wheel provided with spokes C<2> and a rim C<1>. The rim C<1> is preferably L-shaped to provide a flange C<3> to which radial struts D and tangential ties, secured at the other ends to the aircraft, are attached. Ties D<2> may be provided to prevent the hub C from tilting. The cushion A may be provided with an external annular plate to prevent abrasion by the flange C<3>. The axis of rotation may be arranged at an angle to the aircraft, and more than one cushioning-device D may be provided on one frame E, as shown in Fig. 3. In a modification, the wheel is arranged to rotate with the air cushion, the rim serving as a support for the cushion when under load. According to the Provisional Specification, the rotatable mounting may be dispensed with, the wheel and the cushion being fixed with regard to the aircraft, the cushion may be secured to the periphery of the wheel, and the struts D may be hinged to the wheel.
Publications (1)
Publication Number | Publication Date |
---|---|
GB107050A true GB107050A (en) |
Family
ID=1701792
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB107050D Active GB107050A (en) |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB107050A (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2887055A (en) * | 1956-08-07 | 1959-05-19 | Harvey Machine Co Inc | Training and test missile |
WO2006013392A3 (en) * | 2004-08-03 | 2006-04-27 | Michael Zabrana | Self sealing airship |
-
0
- GB GB107050D patent/GB107050A/en active Active
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2887055A (en) * | 1956-08-07 | 1959-05-19 | Harvey Machine Co Inc | Training and test missile |
WO2006013392A3 (en) * | 2004-08-03 | 2006-04-27 | Michael Zabrana | Self sealing airship |
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