GB1158641A - Improvements relating to Ground-Effect Craft - Google Patents
Improvements relating to Ground-Effect CraftInfo
- Publication number
- GB1158641A GB1158641A GB1610065A GB1610065A GB1158641A GB 1158641 A GB1158641 A GB 1158641A GB 1610065 A GB1610065 A GB 1610065A GB 1610065 A GB1610065 A GB 1610065A GB 1158641 A GB1158641 A GB 1158641A
- Authority
- GB
- United Kingdom
- Prior art keywords
- cushion
- skirts
- air
- side walls
- wall
- 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
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B60—VEHICLES IN GENERAL
- B60V—AIR-CUSHION VEHICLES
- B60V1/00—Air-cushion
- B60V1/16—Flexible skirts
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B60—VEHICLES IN GENERAL
- B60V—AIR-CUSHION VEHICLES
- B60V1/00—Air-cushion
- B60V1/04—Air-cushion wherein the cushion is contained at least in part by walls
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Transportation (AREA)
- Mechanical Engineering (AREA)
- Mattresses And Other Support Structures For Chairs And Beds (AREA)
Abstract
1,158,641. Air cushion vehicles. R. D. PARKHOUSE. 14 July, 1966 [14 April, 1965], No. 16100/65. Heading B7K. An air cushion vehicle comprises a base structure 1 formed with side walls 2 to form therewith a plenum chamber 5 supplied with cushion-forming air by a fan 7, the side walls being formed with rests or pads 13 to support the vehicle when not cushion-borne. A flexible, inflatable skirt member 12 is secured to each wall 2 in such manner that when inflated it extends below the wall to assist in containing the cushion and when deflated it collapses so as not to become trapped beneath a side rest. Ports 18 in the members 12 provide for inflation of the skirts by cushion air, though this may be done by providing ducts through side walls 2. The skirts may be double walled on their lower sides to resist abrasion and the skirts may be formed in individual contiguous sealed sections.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB1610065A GB1158641A (en) | 1965-04-14 | 1965-04-14 | Improvements relating to Ground-Effect Craft |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB1610065A GB1158641A (en) | 1965-04-14 | 1965-04-14 | Improvements relating to Ground-Effect Craft |
Publications (1)
Publication Number | Publication Date |
---|---|
GB1158641A true GB1158641A (en) | 1969-07-16 |
Family
ID=10071194
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB1610065A Expired GB1158641A (en) | 1965-04-14 | 1965-04-14 | Improvements relating to Ground-Effect Craft |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB1158641A (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN114524083A (en) * | 2022-04-21 | 2022-05-24 | 中国空气动力研究与发展中心空天技术研究所 | Buoyancy-adjustable wing control surface structure |
-
1965
- 1965-04-14 GB GB1610065A patent/GB1158641A/en not_active Expired
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN114524083A (en) * | 2022-04-21 | 2022-05-24 | 中国空气动力研究与发展中心空天技术研究所 | Buoyancy-adjustable wing control surface structure |
CN114524083B (en) * | 2022-04-21 | 2022-07-12 | 中国空气动力研究与发展中心空天技术研究所 | Buoyancy-adjustable wing control surface structure |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
414F | Notice of opposition given (sect. 14/1949) | ||
414B | Case decided by the comptroller ** grants allowed (sect. 14/1949) | ||
PS | Patent sealed |