GB711434A - Improvements in or relating to puncture sealing devices for aircraft pressurised cabins and the like - Google Patents
Improvements in or relating to puncture sealing devices for aircraft pressurised cabins and the likeInfo
- Publication number
- GB711434A GB711434A GB2260251A GB2260251A GB711434A GB 711434 A GB711434 A GB 711434A GB 2260251 A GB2260251 A GB 2260251A GB 2260251 A GB2260251 A GB 2260251A GB 711434 A GB711434 A GB 711434A
- Authority
- GB
- United Kingdom
- Prior art keywords
- tube
- relating
- sealing devices
- sept
- puncture sealing
- 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
- B64C1/14—Windows; Doors; Hatch covers or access panels; Surrounding frame structures; Canopies; Windscreens accessories therefor, e.g. pressure sensors, water deflectors, hinges, seals, handles, latches, windscreen wipers
- B64C1/1476—Canopies; Windscreens or similar transparent elements
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Measuring Fluid Pressure (AREA)
Abstract
711,434. Fluid flow indicator. NORMALIER, Ltd. Sept. 12, 1952 [Sept. 27, 1951], No. 22602/51. Class 97(2) [Also in Group XXXIII] A fluid flow indicator adapted to detect leaks in the wall of a pressurized space (see Group XXXIII) comprises a tube h in which is a vane j mounted on a spindle m supported by ball bearings k. The spindle carries two light leaf springs n, whose motion is limited by the stop o, and whose inner faces are luminous. The vane rotates at a speed depending on the pressure difference between ends of the tube, and by centrifugal force, a corresponding apparent luminous area is seen from the left hand end of the tube as shown. Such an indicator may be provided at each end of the tube.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB2260251A GB711434A (en) | 1952-09-12 | 1952-09-12 | Improvements in or relating to puncture sealing devices for aircraft pressurised cabins and the like |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB2260251A GB711434A (en) | 1952-09-12 | 1952-09-12 | Improvements in or relating to puncture sealing devices for aircraft pressurised cabins and the like |
Publications (1)
Publication Number | Publication Date |
---|---|
GB711434A true GB711434A (en) | 1954-06-30 |
Family
ID=10182098
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB2260251A Expired GB711434A (en) | 1952-09-12 | 1952-09-12 | Improvements in or relating to puncture sealing devices for aircraft pressurised cabins and the like |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB711434A (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2821298A (en) * | 1954-04-07 | 1958-01-28 | Normalair Ltd | Method and means for temporarily stopping leakage |
-
1952
- 1952-09-12 GB GB2260251A patent/GB711434A/en not_active Expired
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2821298A (en) * | 1954-04-07 | 1958-01-28 | Normalair Ltd | Method and means for temporarily stopping leakage |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
CH294464A (en) | Working medium line on gas turbine systems. | |
GB986831A (en) | Improvements in and relating to flowmeters | |
GB470088A (en) | Improvements in fluid-operated piston apparatus | |
GB711434A (en) | Improvements in or relating to puncture sealing devices for aircraft pressurised cabins and the like | |
GB776486A (en) | Improvements in or relating to air stream direction indicator | |
GB579775A (en) | Improvements relating to labyrinth packings for elastic fluid turbines | |
GB1166012A (en) | Apparatus for Preventing Gas Flow Through Bearings | |
FR888695A (en) | A method of measuring the speed of gas flow, in particular for measuring the speed of a vehicle or an airplane relative to the surrounding air | |
GB549957A (en) | Improvements in or relating to fluid density measuring devices | |
GB700877A (en) | Improvements relating to aerodynamic instruments | |
GB636301A (en) | Fluid seal | |
GB544756A (en) | Improvements in control systems | |
GB578560A (en) | Improvements in remote indicating systems responsive to speed of rotation | |
CA466602A (en) | Fluid pressure compressor governor | |
IIDAKA et al. | Flow in a shock tube with an orifice(Shock tube orifice effect on gas flow velocity and pressure drop, using pressure probes and Jenny friction formula) | |
Youtz | A Device to Protect Large Vacuum Systems Against Accidental Interruptions of the Mechanical Pump | |
GB747857A (en) | Improvements in warning devices | |
GB551439A (en) | Device for indicating or controlling the turning of a craft | |
GB662301A (en) | Improvements in means for balancing the axial thrust of elastic fluid compressors and turbines of the axial flow type | |
ES286170A1 (en) | Mineral starting apparatus (Machine-translation by Google Translate, not legally binding) | |
GB124827A (en) | A Combined Pressure and Static Head for Air Speed Indicators. | |
AU150605B2 (en) | Gaseous fluid turbine pump units | |
GB738212A (en) | Improvements in or relating to beer pump systems | |
CA463898A (en) | Indicator or condition-responsive device for use in high velocity fluid streams | |
GB518479A (en) | Improvements in means for relieving axial and lateral loads |