GB1204615A - Canopy for airplane loading and unloading gangway or ramp - Google Patents
Canopy for airplane loading and unloading gangway or rampInfo
- Publication number
- GB1204615A GB1204615A GB611568A GB611568A GB1204615A GB 1204615 A GB1204615 A GB 1204615A GB 611568 A GB611568 A GB 611568A GB 611568 A GB611568 A GB 611568A GB 1204615 A GB1204615 A GB 1204615A
- Authority
- GB
- United Kingdom
- Prior art keywords
- canopy
- airplane
- ramp
- links
- motor
- 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
- B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
- B64F1/00—Ground or aircraft-carrier-deck installations
- B64F1/30—Ground or aircraft-carrier-deck installations for embarking or disembarking passengers
- B64F1/305—Bridges extending between terminal building and aircraft, e.g. telescopic, vertically adjustable
Landscapes
- Engineering & Computer Science (AREA)
- Architecture (AREA)
- Civil Engineering (AREA)
- Structural Engineering (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Body Structure For Vehicles (AREA)
Abstract
1,204,615. Airplane loading and unloading ramps or gangways. STANRAY CORP. 7 Feb., 1968, No. 6115/68. Heading B7J. The canopy 40 of an airplane passenger ramp or gangway 10 (extending from a terminal building and being of swing and/or extensible type) comprises a flexible resilient bumper 42 engageable with the airplane fuselage 18 above a doorway therein and carried by independent pivoted arm means 46, 46 so as to be extendable to engage portions of the fuselage 18 located at different distances from the ramp 10. Each arm means 46 comprises arms 50, 52 pivoted at 54, 56 to the frame 20 of a cab 14 of the ramp 10, and at 62, 60 to a link 58 connected to the bumper 42. The links 58 are interconnected by spreaders 64, 66 bearing slotted plates engaging with free plug pins on the links 58, so that the arm means are independent (within limits). The canopy 40 has a flexible covering 80 secured to bumper 42 and spreader 66, and flexible sides 94 connected to the links 58 and to the floor 22. The canopy 40 is extended under gravity, or retracted, by rotation of a reversible electric motor 102 acting on a cable 106 secured at its free end to a member 122 connected by an elastic shock cord 124 and an adjustable chain 126 to the frame 20. The member 122 constantly engages or closes a motor switch 130 (when the canopy is not engaged with the airplane) so that operation of a master switch operates the motor until the canopy engages the airplane and the tension in the cable 106 is reduced and the switch 130 opens. Two retraction limit switches 132 in parallel stop the motor 102 only when both are opened by the arms 52.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB611568A GB1204615A (en) | 1968-02-07 | 1968-02-07 | Canopy for airplane loading and unloading gangway or ramp |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB611568A GB1204615A (en) | 1968-02-07 | 1968-02-07 | Canopy for airplane loading and unloading gangway or ramp |
Publications (1)
Publication Number | Publication Date |
---|---|
GB1204615A true GB1204615A (en) | 1970-09-09 |
Family
ID=9808663
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB611568A Expired GB1204615A (en) | 1968-02-07 | 1968-02-07 | Canopy for airplane loading and unloading gangway or ramp |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB1204615A (en) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO1990005665A1 (en) * | 1988-11-22 | 1990-05-31 | Rheem Australia Limited | Aircraft loading bridge |
CN111824444A (en) * | 2019-04-23 | 2020-10-27 | 许布奈有限两合公司 | Joint module |
CN115703545A (en) * | 2021-08-04 | 2023-02-17 | 许布奈有限两合公司 | Coupling module as interface between a boarding bridge or stairway and an aircraft fuselage |
-
1968
- 1968-02-07 GB GB611568A patent/GB1204615A/en not_active Expired
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO1990005665A1 (en) * | 1988-11-22 | 1990-05-31 | Rheem Australia Limited | Aircraft loading bridge |
CN111824444A (en) * | 2019-04-23 | 2020-10-27 | 许布奈有限两合公司 | Joint module |
CN115703545A (en) * | 2021-08-04 | 2023-02-17 | 许布奈有限两合公司 | Coupling module as interface between a boarding bridge or stairway and an aircraft fuselage |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
PS | Patent sealed | ||
PLNP | Patent lapsed through nonpayment of renewal fees |