GB948105A - Improvements relating to hose inlet connections for aircraft ventilating systems - Google Patents
Improvements relating to hose inlet connections for aircraft ventilating systemsInfo
- Publication number
- GB948105A GB948105A GB4146561A GB4146561A GB948105A GB 948105 A GB948105 A GB 948105A GB 4146561 A GB4146561 A GB 4146561A GB 4146561 A GB4146561 A GB 4146561A GB 948105 A GB948105 A GB 948105A
- Authority
- GB
- United Kingdom
- Prior art keywords
- aircraft
- improvements relating
- inlet connections
- hose
- hose inlet
- 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
- 238000007789 sealing Methods 0.000 abstract 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D13/00—Arrangements or adaptations of air-treatment apparatus for aircraft crew or passengers, or freight space, or structural parts of the aircraft
Landscapes
- Health & Medical Sciences (AREA)
- General Health & Medical Sciences (AREA)
- Pulmonology (AREA)
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Specific Sealing Or Ventilating Devices For Doors And Windows (AREA)
Abstract
948,105. Aircraft ground service connections. M. L. AVIATION CO. Ltd. Nov. 20, 1962 [Nov. 20, 1961], No. 41465/61. Heading B7W. [Also in Division E2] An opening is provided in the fuselage of an aircraft so that a hose 5 can be connected, by means of a bayonet fastening 3, 4, which is automatically released as the aircraft moves off (see Division E2) to the aircraft ventilating system when the aircraft is on the ground. The opening has an inner, sealing door 6 and an outer access panel 15 held together in the closed position (Fig. 2, not shown) by a latch fastening (see Division E2). The door and the panel are closed on removal of the hose by a cord 28.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB4146561A GB948105A (en) | 1961-11-20 | 1961-11-20 | Improvements relating to hose inlet connections for aircraft ventilating systems |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB4146561A GB948105A (en) | 1961-11-20 | 1961-11-20 | Improvements relating to hose inlet connections for aircraft ventilating systems |
Publications (1)
Publication Number | Publication Date |
---|---|
GB948105A true GB948105A (en) | 1964-01-29 |
Family
ID=10419810
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB4146561A Expired GB948105A (en) | 1961-11-20 | 1961-11-20 | Improvements relating to hose inlet connections for aircraft ventilating systems |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB948105A (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2183582A (en) * | 1985-12-02 | 1987-06-10 | Neville Hamilton Birch | Aircraft security method and apparatus |
-
1961
- 1961-11-20 GB GB4146561A patent/GB948105A/en not_active Expired
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2183582A (en) * | 1985-12-02 | 1987-06-10 | Neville Hamilton Birch | Aircraft security method and apparatus |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
GB1024952A (en) | Diverter valve assembly | |
GB1201568A (en) | Improvements in or relating to ventilated apparatus cabinets | |
GB948105A (en) | Improvements relating to hose inlet connections for aircraft ventilating systems | |
CA603540A (en) | Aircraft cabin air conditioning system | |
AEPLI | Some technical aspects of modern military vtol aircraft, particularly propulsion system installation and development | |
CA628014A (en) | Cabin air supply means for aircraft | |
AU224591B2 (en) | Jet lift flap systems for aircraft | |
CA636858A (en) | Aircraft air conditioning system | |
CA621493A (en) | Aircraft with jet flap | |
CA680362A (en) | Air intakes for supersonic aircraft | |
CA628453A (en) | Aircraft air conditioning system including a temperature simulator | |
GB583334A (en) | Improvements in or relating to ventilating systems | |
AU4185158A (en) | Jet lift flap systems for aircraft | |
CA636415A (en) | Flow divider for fuel system for jet engine | |
CA694794A (en) | Inlet for vertical take-off aircraft | |
CA633590A (en) | Control system for air inlet bypass | |
AU258967B2 (en) | Crankcase valve ventilating system | |
CA651423A (en) | Turbo jet fuel control with emergency system | |
CA626751A (en) | Aircraft engine fuel systems | |
CA636464A (en) | Air intakes for air aspirating aircraft engines | |
CA614014A (en) | Control systems for gas turbine power units for aircraft | |
CA529722A (en) | Aircraft jet engine cooling system | |
CA690680A (en) | Wing fan doors for aircraft | |
CA622755A (en) | Aircraft control system for cruising flight | |
AU2562362A (en) | Crankcase valve ventilating system |