GB1486202A - Ladders - Google Patents
LaddersInfo
- Publication number
- GB1486202A GB1486202A GB4025074A GB4025074A GB1486202A GB 1486202 A GB1486202 A GB 1486202A GB 4025074 A GB4025074 A GB 4025074A GB 4025074 A GB4025074 A GB 4025074A GB 1486202 A GB1486202 A GB 1486202A
- Authority
- GB
- United Kingdom
- Prior art keywords
- link
- links
- cam
- sub
- pivot point
- 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
- 239000000725 suspension Substances 0.000 abstract 1
Classifications
-
- E—FIXED CONSTRUCTIONS
- E06—DOORS, WINDOWS, SHUTTERS, OR ROLLER BLINDS IN GENERAL; LADDERS
- E06C—LADDERS
- E06C1/00—Ladders in general
- E06C1/52—Ladders in general with non-rigid longitudinal members
Landscapes
- Ladders (AREA)
Abstract
1486202 Extending ladder M L AVIATION CO Ltd 19 Nov 1975 [16 Sept 1974] 40250/74 Heading E1S An extending ladder of the suspension type comprises rungs 5 connected to articulated rigid links comprising sub-links 8, 15 provided with cooperating pressure pads 13, 14. by means of a member 4 to which the sub-links are pivoted, the links being foldable to a stacked configuration in which they lie substantially horizontally on top of one another in the plane of the rungs (see Fig. 2), the hinged joints between adjacent links including interlocks each comprising a cam 2 on the end of one link 15 in the form of a sectorshaped portion centred about the pivot point 3 of that end of the link and a co-operating cam follower 10 on the end of the adjacent link 8 which bears against the cam surface (10B, Fig. 2) to prevent rotation until the upper link 15 rotates to take the cam to a position (2A in Fig. 2) in which the cam follower is beyond the end of the sectorshaped portion and is allowed to move towards the pivot point 3 thus permitting turning movement of link 18 (Fig. 2) to the vertical position (as 8 in Fig. 1) in which position the link next above it is locked in the vertical position and cannot start to turn to a horizontal position until link 8 (Fig. 1) is substantially horizontal, the links being prevented from turning past the fully extended position by pressure pads 16, 12 which cooperate with pressure pad 11 on the intermediate member 4.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB4025074A GB1486202A (en) | 1975-11-19 | 1975-11-19 | Ladders |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB4025074A GB1486202A (en) | 1975-11-19 | 1975-11-19 | Ladders |
Publications (1)
Publication Number | Publication Date |
---|---|
GB1486202A true GB1486202A (en) | 1977-09-21 |
Family
ID=10413965
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB4025074A Expired GB1486202A (en) | 1975-11-19 | 1975-11-19 | Ladders |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB1486202A (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2979898A1 (en) * | 2011-09-13 | 2013-03-15 | Airbus Operations Sas | Retractable ladder for emergency exit of aircraft to evacuate pilots, has segments swiveling between posts along rotational axes perpendicular to plane of ladder, where rotational axes are distributed on posts in same manner |
-
1975
- 1975-11-19 GB GB4025074A patent/GB1486202A/en not_active Expired
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2979898A1 (en) * | 2011-09-13 | 2013-03-15 | Airbus Operations Sas | Retractable ladder for emergency exit of aircraft to evacuate pilots, has segments swiveling between posts along rotational axes perpendicular to plane of ladder, where rotational axes are distributed on posts in same manner |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
PS | Patent sealed | ||
PCNP | Patent ceased through non-payment of renewal fee |