CN1405062A - Independent safety passenger driver cabin - Google Patents
Independent safety passenger driver cabin Download PDFInfo
- Publication number
- CN1405062A CN1405062A CN01141729A CN01141729A CN1405062A CN 1405062 A CN1405062 A CN 1405062A CN 01141729 A CN01141729 A CN 01141729A CN 01141729 A CN01141729 A CN 01141729A CN 1405062 A CN1405062 A CN 1405062A
- Authority
- CN
- China
- Prior art keywords
- driving compartment
- lock
- main cabin
- independent
- make
- 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.)
- Pending
Links
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 claims description 11
- 239000010865 sewage Substances 0.000 claims description 10
- IWEDIXLBFLAXBO-UHFFFAOYSA-N dicamba Chemical compound COC1=C(Cl)C=CC(Cl)=C1C(O)=O IWEDIXLBFLAXBO-UHFFFAOYSA-N 0.000 claims description 7
- 235000013361 beverage Nutrition 0.000 claims description 2
- 150000001875 compounds Chemical class 0.000 claims 1
- 238000000034 method Methods 0.000 claims 1
- 238000012806 monitoring device Methods 0.000 claims 1
- 238000000926 separation method Methods 0.000 abstract 1
- 238000004140 cleaning Methods 0.000 description 2
- 238000011010 flushing procedure Methods 0.000 description 2
- 238000012423 maintenance Methods 0.000 description 2
- 238000002955 isolation Methods 0.000 description 1
- 239000007921 spray Substances 0.000 description 1
- 238000009423 ventilation Methods 0.000 description 1
Images
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
- B64C1/1407—Doors; surrounding frames
- B64C1/1469—Doors between cockpit and cabin
-
- 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
- B64D45/00—Aircraft indicators or protectors not otherwise provided for
- B64D45/0015—Devices specially adapted for the protection against criminal attack, e.g. anti-hijacking systems
- B64D45/0051—Devices specially adapted for the protection against criminal attack, e.g. anti-hijacking systems by monitoring passengers or crew on aircraft
- B64D45/0053—Devices specially adapted for the protection against criminal attack, e.g. anti-hijacking systems by monitoring passengers or crew on aircraft using visual equipment, e.g. cameras
-
- 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
- B64D45/00—Aircraft indicators or protectors not otherwise provided for
- B64D45/0015—Devices specially adapted for the protection against criminal attack, e.g. anti-hijacking systems
- B64D45/0021—Devices specially adapted for the protection against criminal attack, e.g. anti-hijacking systems means for restricting access to flight deck
- B64D45/0028—Devices specially adapted for the protection against criminal attack, e.g. anti-hijacking systems means for restricting access to flight deck doors or door arrangements specially adapted to restrict unauthorized access
- B64D45/0029—Devices specially adapted for the protection against criminal attack, e.g. anti-hijacking systems means for restricting access to flight deck doors or door arrangements specially adapted to restrict unauthorized access electrically actuated
-
- H—ELECTRICITY
- H04—ELECTRIC COMMUNICATION TECHNIQUE
- H04L—TRANSMISSION OF DIGITAL INFORMATION, e.g. TELEGRAPHIC COMMUNICATION
- H04L63/00—Network architectures or network communication protocols for network security
- H04L63/08—Network architectures or network communication protocols for network security for authentication of entities
- H04L63/0861—Network architectures or network communication protocols for network security for authentication of entities using biometrical features, e.g. fingerprint, retina-scan
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Health & Medical Sciences (AREA)
- Biomedical Technology (AREA)
- General Health & Medical Sciences (AREA)
- Computer Hardware Design (AREA)
- Computer Security & Cryptography (AREA)
- Computing Systems (AREA)
- General Engineering & Computer Science (AREA)
- Computer Networks & Wireless Communication (AREA)
- Signal Processing (AREA)
- Lock And Its Accessories (AREA)
- Vehicle Waterproofing, Decoration, And Sanitation Devices (AREA)
Abstract
The invention utilizes effective separation of driver and passenger contact to prevent air piracy. Said design can utilize safety identification system to raise strength of control cabin and its anti-breaking capacity, and utilizes its single life-protecting system to make control cabin independently guarantee life of driver to make driver have no need of leaving control cabin and can fly.
Description
Along with the continuous increase of seating plane passenger capacity, the case that passenger plane is held as a hostage happens occasionally, and has seriously endangered national security and social stability.
Airplane hijacking mainly contains two kinds of situations: first kind when flight when leaving driving compartment (generation), and second kind is that the offender is when rushing in driving compartment by force (generation).
The present invention designs in order to prevent to hijack a plane, and a kind of free-standing aircraft cockpit provides complete life-support systems for the aviator, and by the security identification system main cabin and driving compartment is really isolated.The design has completely cut off aviator and passenger's touch opportunity by life-support systems (three) and the common free-standing driving compartment of forming of intelligent and safe recognition system (two).Though passenger plane is in the past compared passenger plane such as B747, nearly 14 lavatories (and health) and the diligent personnel's special use of a special visitor, the aviator must leave driving compartment and could use, also this fatal scarce limit just, just to the offender with opportunity.Thereby fundamentally prevent the generation of hijacking a plane, independent just aircraft cockpit () makes the aviator needn't be more as before.Rely on the common facilities in main cabin, independent aircraft cockpit (one) is eliminated major safety risks with the mode that increases a little space (cost), makes driving compartment become the firmest fort in cabin, no matter which kind of accident takes place in the main cabin, guarantee that yoke grasp forever is in hand of driver.
In conjunction with Figure of description, be described in detail as follows down:
Fig. 1, driving cofferdam lateral plan
Fig. 2, driving cofferdam birds-eye view
Fig. 3, intelligent and safe means of identification planar view (chaufeur direction)
Fig. 4, slight sewage treatment system.
Fig. 5, severe sewage treatment system.
Fig. 6, free-standing driving compartment panoramic view.
As shown in Figure 1
(1) the independent cofferdam of driving
(2) intelligent and safe recognition system
(3) life-support systems
Isolate bulkhead 1. ' with independent driving compartment and fuselage other parts (main cabin), pilot's (chaufeur) can by security identification system (two) enter independent driving compartment and within it (independent driving compartment in) finish driving task (independent driving compartment ()) for chaufeur provides basic demand guarantee (life-support systems (three)), guarantee chaufeur be not subjected to after engine room the influence of contingent incident.S is the water source.As shown in Figure 2
Wherein (two) are the intelligent and safe recognition system
(3) the basic supply kept system, comprises 1. lavatory.2. between food and beverage store (cabinet).F is a ventilation equipment, and S is a water source supply.(2) enter unique passage Fig. 3 of (independent driving compartment ()) for the main cabin as shown in the figure
Intelligent identification device (two) is by isolating bulkhead 1. as shown in Figure 3 ': with isolate hatch door 2. ' and hatch door on the main cabin display device 3. ' form jointly and wherein isolate hatch door 2. ' and door lock thereof are described in detail as follows and isolate hatch door and comprise the A external lock, the B internal lock, C intelligent emergent lock.
The A external lock 
A external lock B internal lock (intelligent)
Slight sewage treatment system (the S of C automatic emergency lock Fig. 4
1)
Wash water for the lavatory can adopt direct exhaust system, and its structure is as follows.
The 1-cleaning vat; 2-airborne release bar assembly, the 3-overflow weir; 4-balancing orifice pipe; The 5-silencer; The anti-icing element of 6-electricity; 7-cleaning vat discharge side stops up; The 8-floor; The 9-lavatory; The 10-front door; 11-heavier-duty driving compartment boundary bulkhead 1. '; The 12-water source; The 13-fuselage skin; The H-water heater; The M-silencer.Fig. 5 vacuum type sewage treatment system (S
2)
The severe sewage that the lavatory produced is handled, can be adopted the processing mode of vacuum type, its structure is as follows:
1-toilet seat basin; The 2-ring sparger; 3-washes the water source; The 4-blowoff valve; The 5-check valve; The 6-fuselage skin; The 7-deflation hole; 8-vacuum pump assembly; 9-foul water tank assembly; 10-ground maintenance blowoff valve; 11-blowoff valve joystick; 12-ground maintenance flap; 13-blowoff valve bar handle; 14-Sewage outlet joint; 15-foul water tank assembly ground flushing pipe joint; 16-sprays ozzle; The 17-flushing pipe; The 18-catch water; 19-sewage discharge house steward; 20-isolates the driving compartment floor.Fig. 6 aircraft safety is isolated driving compartment complete set view.
(1) independent driving compartment
(2) security identification system
(3) 1. lavatory
(5) main cabin
2. ' the isolation safe hatch door is 3. ' be that the main cabin monitors display device
Claims (5)
1, the present invention relates to the driving compartment of seating plane and safety system thereof by improving the independence of driving compartment, increase safety factor, it is characterized in that: by intelligent and safe recognition system (two) aircraft cockpit and main cabin (comprising front door) are isolated, form (relatively) independent driving compartment ().In independent driving compartment (), make the aviator needn't leave driving compartment (can ensure existence demand), life-support systems (three)
2, according to claim, in/described independent the driving compartment (), security identification system (two) feature is as follows, and by the isolated full wall of heavier-duty 1. it be '; Intelligent Recognition safety hatch door is 2. ' (comprising A intelligence external lock, B, intelligent internal lock, C automatic emergency lock); And be positioned at hatch door 2. common composition of ' main cabin on top monitor that display device 3. ' (can connect one or more monitoring devices, and changeable picture).
3, as described in the claim 1, its life-support systems (three), feature is as follows, comprise that the lavatory 1., 2. small-sized compound addendum cabinet (be used for store food and beverage), existence support system (three) (ventilating and the water source) by the isolated bulkhead of heavier-duty 1. ' in show that pipeline links to each other with the corresponding establishment in main cabin, wherein, 1. the lavatory comprises two cover sewage disposal states.
S
1The direct exhaust system of wash water.
S
2Severe sewage sewage treatment system.
4, according to this claim 2, the Intelligent Recognition hatch door is 2. ' feature be: the A external lock
The B internal lock
(annotate: the B lock has the voice suggestion state, and the driving engine that only exists the B lock to be in the lock state just can start, and the B internal lock can be set in state of flight can't opening, internal lock can only be finished by control in the cofferdam and operation and open and locking.) C automatic emergency lock
5, as described in claim 1, independent driving compartment (one) is characterized in that, security identification system two improves the safety of driving compartment, improve the independence of driving compartment by life-support systems (three), make the aviator not go out driving compartment and can finish flight whole process, by security identification system (two) its form one fully independently aircraft cockpit () make the aviator can not rely on the common plant in main cabin, from under situation, finishing technical operation, from start to finish, be not subjected to the main cabin the influence of emergency may take place, outside driving compartment, make dangerous pass driving compartment become the firmest fort in the passenger plane, in this seating plane structure in the past, do not have.
Priority Applications (3)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN01141729A CN1405062A (en) | 2001-09-17 | 2001-09-17 | Independent safety passenger driver cabin |
| AU2002332217A AU2002332217A1 (en) | 2001-09-17 | 2002-09-13 | Isolating security cockpit for the airplane |
| PCT/CN2002/000644 WO2003047973A1 (en) | 2001-09-17 | 2002-09-13 | Isolating security cockpit for the airplane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN01141729A CN1405062A (en) | 2001-09-17 | 2001-09-17 | Independent safety passenger driver cabin |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN1405062A true CN1405062A (en) | 2003-03-26 |
Family
ID=4676366
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN01141729A Pending CN1405062A (en) | 2001-09-17 | 2001-09-17 | Independent safety passenger driver cabin |
Country Status (3)
| Country | Link |
|---|---|
| CN (1) | CN1405062A (en) |
| AU (1) | AU2002332217A1 (en) |
| WO (1) | WO2003047973A1 (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102574571A (en) * | 2009-10-09 | 2012-07-11 | 空中客车德国运营有限责任公司 | Pressure fuselage of an aircraft comprising a tail-face pressure calotte |
| US8544795B2 (en) | 2007-06-15 | 2013-10-01 | Airbus Operations Sas | Item of aircraft galley furniture and aircraft comprising such an item of furniture |
Families Citing this family (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE102007041391A1 (en) * | 2007-08-31 | 2009-03-05 | Airbus Deutschland Gmbh | Secured cockpit with integrated lounge area and sanitary facilities |
| ES2615153B1 (en) * | 2015-12-04 | 2018-03-16 | Luís Víctor SALUEÑA SALUEÑA | Window to supply the flight crew with food |
| ES2615163B1 (en) * | 2015-12-04 | 2018-03-16 | Luís Víctor SALUEÑA SALUEÑA | Wheeled toilet installed inside the designated flight crew cabin ensuring flight with the cabin door closed inside |
| US12397913B2 (en) * | 2023-01-30 | 2025-08-26 | Airbus Operations Gmbh | Aircraft section and aircraft having a monument with two lavatories |
Family Cites Families (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3704845A (en) * | 1971-01-14 | 1972-12-05 | Michael Ord | Airplane hijacking prevention system |
| DE2210312C3 (en) * | 1972-03-03 | 1980-06-26 | Hauni-Werke Koerber & Co Kg, 2050 Hamburg | Arrangement in a commercial aircraft to reduce the risk of kidnapping |
| US4275470A (en) * | 1979-07-18 | 1981-06-30 | Rogerson Aircraft Controls | Vacuum-flush toilet arrangement for aircraft |
| CN85100918A (en) * | 1985-04-01 | 1985-12-20 | 易明 | Passenger plane with " Convention for the Suppression of Unlawful Seizure of Aircraft " function |
| JPH0723358Y2 (en) * | 1988-04-04 | 1995-05-31 | 株式会社ジャムコ | Lavatory unit for airliner |
| CN1038434A (en) * | 1988-06-07 | 1990-01-03 | 张华� | Anti-hijacking device aboard is installed |
| FR2641397A1 (en) * | 1989-01-05 | 1990-07-06 | Coret Francis | Devices for disabling attackers on board aircraft |
| FR2662419A1 (en) * | 1990-05-28 | 1991-11-29 | Darniche Patrick | Safety system |
| DE19732806A1 (en) * | 1997-07-30 | 1999-02-04 | Vidair Avionics Ag | Monitoring device for the interior of aircraft, in particular passenger aircraft |
-
2001
- 2001-09-17 CN CN01141729A patent/CN1405062A/en active Pending
-
2002
- 2002-09-13 AU AU2002332217A patent/AU2002332217A1/en not_active Abandoned
- 2002-09-13 WO PCT/CN2002/000644 patent/WO2003047973A1/en not_active Ceased
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US8544795B2 (en) | 2007-06-15 | 2013-10-01 | Airbus Operations Sas | Item of aircraft galley furniture and aircraft comprising such an item of furniture |
| CN101765541B (en) * | 2007-06-15 | 2013-11-20 | 空中客车运营公司 | Item of aircraft galley furniture and aircraft comprising such an item of furniture |
| CN102574571A (en) * | 2009-10-09 | 2012-07-11 | 空中客车德国运营有限责任公司 | Pressure fuselage of an aircraft comprising a tail-face pressure calotte |
| US8939404B2 (en) | 2009-10-09 | 2015-01-27 | Airbus Operations Gmbh | Pressure fuselage of an aircraft with dome-shaped pressure bulkhead |
| CN102574571B (en) * | 2009-10-09 | 2015-09-09 | 空中客车德国运营有限责任公司 | There is the pressure fuselage of the aircraft of the holding bulkhead of tail side |
Also Published As
| Publication number | Publication date |
|---|---|
| WO2003047973A1 (en) | 2003-06-12 |
| AU2002332217A1 (en) | 2003-06-17 |
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Legal Events
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|---|---|---|---|
| C10 | Entry into substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| C06 | Publication | ||
| PB01 | Publication | ||
| C10 | Entry into substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| C10 | Entry into substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| C57 | Notification of unclear or unknown address | ||
| DD01 | Delivery of document by public notice |
Addressee: Lu Dawei Document name: Notice of application for publication of patent for invention and entry into the substantive examination procedure |
|
| C02 | Deemed withdrawal of patent application after publication (patent law 2001) | ||
| WD01 | Invention patent application deemed withdrawn after publication |