GB560578A - Improvements in or relating to aircraft bodies - Google Patents
Improvements in or relating to aircraft bodiesInfo
- Publication number
- GB560578A GB560578A GB1558242A GB1558242A GB560578A GB 560578 A GB560578 A GB 560578A GB 1558242 A GB1558242 A GB 1558242A GB 1558242 A GB1558242 A GB 1558242A GB 560578 A GB560578 A GB 560578A
- Authority
- GB
- United Kingdom
- Prior art keywords
- panel
- flanges
- edge
- locking bolt
- body 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
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
- B64C1/32—Severable or jettisonable parts of fuselage facilitating emergency escape
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Component Parts Of Construction Machinery (AREA)
Abstract
560,578. Escape hatches. BOOTH, J. H., and PERFECTA MOTOR EQUIPMENTS, Ltd. Nov. 5, 1942, No. 15582. [Class 4] An escape hatch construction for an aircraft body comprises a panel 37 with a releasable fastening 45, 46, and 29, Fig. 6, at one edge and a hook engagement 50, 53 at the opposite edge, which will be self-releasing when the fastened edge is moved outwardly after release. The fastening means, further shown in section, Fig. 7, comprises angle brackets, carried by the panel 37, with flanges 45 inserted between spaced flanges 29 of brackets mounted on the body wall 16, a locking bolt 46 passing through holes in the flanges 45, 29 and being connected to a flexible cable 47, which passes through a sleeve 35 rotatable so as to exert tension on the cable by pulling down an operating handle 39. In a modification a rigid tension rod operated by a rotatable sleeve is connected to the locking bolt. Resilient packing 24 is mounted in channels of metal lining members 19 of the body wall and is bent down by angle members 42 lining the panel 37.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB1558242A GB560578A (en) | 1942-11-05 | 1942-11-05 | Improvements in or relating to aircraft bodies |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB1558242A GB560578A (en) | 1942-11-05 | 1942-11-05 | Improvements in or relating to aircraft bodies |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB560578A true GB560578A (en) | 1944-04-11 |
Family
ID=10061697
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB1558242A Expired GB560578A (en) | 1942-11-05 | 1942-11-05 | Improvements in or relating to aircraft bodies |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB560578A (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB2236515A (en) * | 1989-08-24 | 1991-04-10 | Raam Shankar Pershadsingh | Civil passenger aircraft escape system |
| WO1998019908A1 (en) * | 1996-11-08 | 1998-05-14 | Sikorsky Aircraft Corporation | Emergency egress system for aircraft |
| US6047701A (en) * | 1996-12-16 | 2000-04-11 | Feldman; Marvin Karpa | Tray with grooves and slots for recirculation of moist air for a humidor in operation |
-
1942
- 1942-11-05 GB GB1558242A patent/GB560578A/en not_active Expired
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB2236515A (en) * | 1989-08-24 | 1991-04-10 | Raam Shankar Pershadsingh | Civil passenger aircraft escape system |
| WO1998019908A1 (en) * | 1996-11-08 | 1998-05-14 | Sikorsky Aircraft Corporation | Emergency egress system for aircraft |
| US5826824A (en) * | 1996-11-08 | 1998-10-27 | Sikorsky Aircraft Corporation | Emergency egress system for aircraft |
| CN1087252C (en) * | 1996-11-08 | 2002-07-10 | 西科尔斯基飞机公司 | Emergency egress system for aircraft |
| US6047701A (en) * | 1996-12-16 | 2000-04-11 | Feldman; Marvin Karpa | Tray with grooves and slots for recirculation of moist air for a humidor in operation |
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