NO138830B - ROLLER BELT DEVICE FOR TWO AIRCRAFT SEATS ARRANGED SIDE BY SIDE IN AN AIRCRAFT CABIN - Google Patents

ROLLER BELT DEVICE FOR TWO AIRCRAFT SEATS ARRANGED SIDE BY SIDE IN AN AIRCRAFT CABIN Download PDF

Info

Publication number
NO138830B
NO138830B NO760458A NO760458A NO138830B NO 138830 B NO138830 B NO 138830B NO 760458 A NO760458 A NO 760458A NO 760458 A NO760458 A NO 760458A NO 138830 B NO138830 B NO 138830B
Authority
NO
Norway
Prior art keywords
pilot
seat
aircraft
roller
block
Prior art date
Application number
NO760458A
Other languages
Norwegian (no)
Other versions
NO760458L (en
NO138830C (en
Inventor
Sverre Danielsen
Original Assignee
Sverre Danielsen
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Sverre Danielsen filed Critical Sverre Danielsen
Priority to NO76760458A priority Critical patent/NO138830C/en
Priority to DE19772703799 priority patent/DE2703799A1/en
Priority to GB3816/77A priority patent/GB1570326A/en
Priority to AU21889/77A priority patent/AU502712B2/en
Priority to NL7701224A priority patent/NL7701224A/en
Priority to CA271,122A priority patent/CA1059485A/en
Priority to FR7703581A priority patent/FR2340744A1/en
Priority to SE7701461A priority patent/SE411877B/en
Publication of NO760458L publication Critical patent/NO760458L/en
Priority to US05/873,480 priority patent/US4121792A/en
Publication of NO138830B publication Critical patent/NO138830B/en
Publication of NO138830C publication Critical patent/NO138830C/en

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D25/00Emergency apparatus or devices, not otherwise provided for
    • B64D25/02Supports or holding means for living bodies

Description

Oppfinnelsen angår en anordning ved rullebelter for to flyførerseter som er anordnet side om side i en flyfører-kabin, omfattende en eventuelt to faststående rullemekanismer på hvert flyførersete. The invention relates to a device for roller belts for two pilot's seats which are arranged side by side in a pilot's cabin, comprising an optional two fixed roller mechanisms on each pilot's seat.

Pra U.S.-patentskrift nr. 2.883.123 er det tidligere kjent en sikkerhetsanordning for bruk i motordrevet kjøretøy, der den som sitter-i et sete på kjøretøyet ved registrering av en fare, kan trykke på en bryter, slik at eget setebelte blir strammet til, eller kjøretøyets fører kan ved ekstra trykk på bremsepedalen bevirke at alle setebeltene i kjøretøyet strammes til. Denne anordning er særlig beregnet på passasjer-er i kjøretøyet. According to U.S. Patent No. 2,883,123, a safety device for use in a motor-driven vehicle is previously known, where the person sitting in a seat on the vehicle, when a danger is detected, can press a switch, so that their own seat belt is tightened , or the driver of the vehicle can, by extra pressure on the brake pedal, cause all the seat belts in the vehicle to be tightened. This device is particularly intended for passengers in the vehicle.

To flyførerseter er vanligvis anordnet side om side Two pilot seats are usually arranged side by side

i førerkabinen og det anvendes rullebelter for at flyførerne skal kunne nå frem til instrumentpanelene. Mellom hvert av flyførersetene og instrumentpanelene er det anordnet en be-tjeningsspake som ved tumlebevegelse betjener høyderor og balanseror og disse spaker er parallelkoplet. Hvis en av fly-førerne skulle få et illebefinnende og siger frem over sin spake, og derved setter flyet i en stupebevegelse, kan det være vanskelig for den annen flyfører å holde igjen med sin spake, og det kan skje en katastrofe. in the driver's cabin and roller belts are used so that the pilots can reach the instrument panels. Between each of the pilot's seats and the instrument panels, there is an operating lever which, with a tumbling movement, operates the elevator and balance rudder, and these levers are connected in parallel. If one of the pilots should feel unwell and pull forward on his lever, thereby setting the plane into a dive, it may be difficult for the other pilot to keep up with his lever, and a disaster may occur.

Hensikten med oppfinnelsen er å muliggjøre for The purpose of the invention is to make it possible for

den annen flyfører uten utøvelse av den kraft som er nødvendig for å fjerne den første flyfører fra sin spake og uten å fjerne seg fra sitt eget sete, å frigjøre spaken og dermed hindre katastrofen. the second pilot without exerting the force necessary to remove the first pilot from his lever and without removing himself from his own seat, to release the lever and thereby prevent the disaster.

Dette oppnås ifølge oppfinnelsen ved at rullemekanismen eller rullemekanismene på det ene flyførersete via en utveksling er tilkoplet en drivkilde, og at det innen rekkevidde av flyføreren i det andre flyførersete er anordnet et betjeningsorgan for drivkilden. This is achieved according to the invention by the fact that the roller mechanism or roller mechanisms on one pilot's seat are connected to a drive source via a transmission, and that an operating device for the drive source is arranged within reach of the pilot in the other pilot's seat.

Ytterligere trekk ved oppfinnelsen vil fremgå av kravene 2 og 3. Further features of the invention will appear from claims 2 and 3.

Et utførelseseksempel på en anordning ifølge oppfinnelsen skal nedenfor forklares nærmere under henvisning til tegningen som skjematisk viser to flyførerseter sett bakfra og utrustet med en anordning ifølge oppfinnelsen. An embodiment of a device according to the invention will be explained in more detail below with reference to the drawing which schematically shows two pilot's seats seen from behind and equipped with a device according to the invention.

Rullemekanismene 1 for hvert belte via en trommel er forbundet med den ene ende av en wire 2 som vikles av og på trommelen og over lederuller 3 er ført over en blokkskive i en første blokk 8 i en talje 4,8, over en første blokkskive i en andre blokk 4 i taljen, over en andre blokkskive i den første blokk 8, og er sluttelig festet til den andre blokk 4. Den andre blokk 4 er fast forbundet med flyførersetet, og den første blokk 8 er forbundet med den midtre del av en arm 7 hvis ender er forbundet med den ene ende av hver sin trykkluft-sylinder 5 hvis andre ende er fast forbundet med flyførersetet. Gjennom ledninger 6 er de to trykkluftsylindre forbundet med en ikke vist trykkluftbeholder via en betjeningsventil 11 resp. 10. På denne måte kan flyføreren til høyre på tegningen ved betjening av ventilen 11 rulle inn beltene for flyføreren til venstre på tegningen og omvendt. The roller mechanisms 1 for each belt via a drum are connected to one end of a wire 2 which is wound on and off the drum and over guide rollers 3 are led over a block sheave in a first block 8 in a pulley 4,8, over a first block sheave in a second block 4 in the hoist, over a second block disc in the first block 8, and is finally attached to the second block 4. The second block 4 is firmly connected to the pilot's seat, and the first block 8 is connected to the middle part of a arm 7 whose ends are connected to one end of each compressed air cylinder 5 whose other end is firmly connected to the pilot's seat. Through lines 6, the two compressed air cylinders are connected to a not shown compressed air container via an operating valve 11 or 10. In this way, the pilot on the right in the drawing can by operating the valve 11 roll in the belts for the pilot on the left in the drawing and vice versa.

Det er klart at det kan anvendes en annen trykk-mediumkilde enn en trykkluftflaske, nemlig flyets eget trykk-luf tanlegg, eller flyets eget hydrauliske trykkanlegg. Videre kan det istedet for arbeidssylindre og talje, anvendes elektrisk motor med stor utveksling. It is clear that a different source of pressure medium than a compressed air cylinder can be used, namely the aircraft's own compressed air system, or the aircraft's own hydraulic pressure system. Furthermore, instead of working cylinders and pulleys, an electric motor with a large ratio can be used.

Claims (3)

1. Anordning ved rullebelte for to flyførerseter som er anordnet side om side i en flyførerkabin, omfattende en eventuelt to faststående rullemekanismer (1) på hvert flyfører-sete, karakterisert ved at rullemekanismen eller rullemekanismene (1) på det ene flyførersete (9 resp. 12) via en utveksling (2-8) er tilkoplet en drivkilde, og at det innen rekkevidde av flyføreren i det andre flyførersete (12 resp. 9) er anordnet et betjeningsorgan (11 resp. 10) for drivkilden.1. Device by roller belt for two pilot's seats which are arranged side by side in a pilot's cabin, comprising an optional two fixed roller mechanisms (1) on each pilot's seat, characterized in that the roller mechanism or roller mechanisms (1) on one pilot's seat (9 resp. 12) via a transmission (2-8) a drive source is connected, and that an operating device (11 or 10) for the drive source is arranged within reach of the pilot in the second pilot's seat (12 or 9). 2. Anordning ifølge krav 1, karakterisert ved at utvekslingen omfatter en talje (2,4,8) med en wire (2) hvis ene ende er forbundet med rullemekanismen resp. rullemekanismene (1) og hvis andre ende er forbundet med minst én arbeidssylinder (5) hvis trykkmedium via et betjeningsorgan i form av en ventil (10 resp. 11) tilføres fra et trykk-reservoar for mediet.2. Device according to claim 1, characterized in that the exchange comprises a pulley (2,4,8) with a wire (2), one end of which is connected to the roller mechanism or the roller mechanisms (1) and whose other end is connected to at least one working cylinder (5) whose pressure medium is supplied via an operating device in the form of a valve (10 or 11) from a pressure reservoir for the medium. 3. Anordning ifølge krav 2, karakterisert ved at den ene blokk (4) i taljen er fast lagret i flyfører-setet (9 resp. 12) og at den andre blokk (8) er forbundet med den ene ende av arbeidssylinderen resp. -sylinderne (5) hvis andre ende er festet i flyførersetet.3. Device according to claim 2, characterized in that one block (4) in the hoist is fixedly stored in the pilot's seat (9 or 12) and that the other block (8) is connected to one end of the working cylinder or -the cylinders (5) whose other end is fixed in the pilot's seat.
NO76760458A 1976-02-12 1976-02-12 ROLLER BELT DEVICE FOR TWO AIRCRAFT SEATS Arranged SIDE BY SIDE IN AN AIRCRAFT CABIN NO138830C (en)

Priority Applications (9)

Application Number Priority Date Filing Date Title
NO76760458A NO138830C (en) 1976-02-12 1976-02-12 ROLLER BELT DEVICE FOR TWO AIRCRAFT SEATS Arranged SIDE BY SIDE IN AN AIRCRAFT CABIN
DE19772703799 DE2703799A1 (en) 1976-02-12 1977-01-29 DEVICE FOR ROLL BELT FOR AIRCRAFT DRIVER'S SEATS
GB3816/77A GB1570326A (en) 1976-02-12 1977-01-31 Combined aircraft seating and safety harness system
AU21889/77A AU502712B2 (en) 1976-02-12 1977-02-03 Airplane pilot harness
CA271,122A CA1059485A (en) 1976-02-12 1977-02-04 Roller harness arrangement for airplane pilot seats
NL7701224A NL7701224A (en) 1976-02-12 1977-02-04 ROLLER SEAT BELT FOR AIRCRAFT OPERATORS.
FR7703581A FR2340744A1 (en) 1976-02-12 1977-02-09 ROLLER HARNESS KIT FOR AIRCRAFT PILOTS SEATS
SE7701461A SE411877B (en) 1976-02-12 1977-02-09 DEVICE IN INVENTABLE SECURITY BELT FOR AIRCRAFT
US05/873,480 US4121792A (en) 1976-02-12 1978-01-30 Roller harness arrangement for airplane pilot seats

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
NO76760458A NO138830C (en) 1976-02-12 1976-02-12 ROLLER BELT DEVICE FOR TWO AIRCRAFT SEATS Arranged SIDE BY SIDE IN AN AIRCRAFT CABIN

Publications (3)

Publication Number Publication Date
NO760458L NO760458L (en) 1977-08-15
NO138830B true NO138830B (en) 1978-08-14
NO138830C NO138830C (en) 1978-11-22

Family

ID=19882712

Family Applications (1)

Application Number Title Priority Date Filing Date
NO76760458A NO138830C (en) 1976-02-12 1976-02-12 ROLLER BELT DEVICE FOR TWO AIRCRAFT SEATS Arranged SIDE BY SIDE IN AN AIRCRAFT CABIN

Country Status (8)

Country Link
AU (1) AU502712B2 (en)
CA (1) CA1059485A (en)
DE (1) DE2703799A1 (en)
FR (1) FR2340744A1 (en)
GB (1) GB1570326A (en)
NL (1) NL7701224A (en)
NO (1) NO138830C (en)
SE (1) SE411877B (en)

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3903924A1 (en) * 1989-02-10 1990-08-23 Autoflug Gmbh Safety belt arrangement for pilots
FR2658478A1 (en) * 1990-02-19 1991-08-23 Jdc Electronic Sa Device for semi-automatic setting of the flight position of a parapentist
DE19505448A1 (en) * 1995-02-17 1996-08-22 Bayerische Motoren Werke Ag Safety device, especially for a two-wheeler

Also Published As

Publication number Publication date
NL7701224A (en) 1977-08-16
NO760458L (en) 1977-08-15
FR2340744A1 (en) 1977-09-09
NO138830C (en) 1978-11-22
CA1059485A (en) 1979-07-31
FR2340744B1 (en) 1983-09-09
SE7701461L (en) 1977-08-13
GB1570326A (en) 1980-06-25
SE411877B (en) 1980-02-11
AU2188977A (en) 1978-08-10
AU502712B2 (en) 1979-08-02
DE2703799A1 (en) 1977-08-18

Similar Documents

Publication Publication Date Title
ITMO20120320A1 (en) METHOD AND APPARATUS FOR CHECKING THE BRAKING OF A TRAILER TRAILER COMBINATION.
NO138830B (en) ROLLER BELT DEVICE FOR TWO AIRCRAFT SEATS ARRANGED SIDE BY SIDE IN AN AIRCRAFT CABIN
US2033433A (en) Pedal mechanism
US2192021A (en) Automatic braking system
US3240291A (en) Vehicle braking system
US2252013A (en) Pedal control and spacer for power and brake systems or the like
US1998677A (en) Operating mechanism
US2322499A (en) Auxiliary brake operator for vehicles
US2065354A (en) Foot pedal organization for motor vehicles
US2792083A (en) Hydraulic brake system
US1985346A (en) Vehicle brake arrangement
US2750010A (en) Automatic parking brake for motor vehicles
US1883414A (en) Air vehicle
US1576717A (en) Brake for motor vehicles
US2499154A (en) Spring applied vacuum released brake
US3344895A (en) Hand brake arrangement
US4121792A (en) Roller harness arrangement for airplane pilot seats
GB2051986A (en) Automatically applied brakes
DE2165261A1 (en) LEG REST FOR DRIVERS
US1620744A (en) Motor vehicle
US1828641A (en) Braking apparatus for aircraft
US1563588A (en) Brake mechanism for automobiles
USRE18997E (en) Brake control
US1605558A (en) Brake mechanism
US714035A (en) Steering apparatus for boats.