GB2236515A - Civil passenger aircraft escape system - Google Patents

Civil passenger aircraft escape system Download PDF

Info

Publication number
GB2236515A
GB2236515A GB8919294A GB8919294A GB2236515A GB 2236515 A GB2236515 A GB 2236515A GB 8919294 A GB8919294 A GB 8919294A GB 8919294 A GB8919294 A GB 8919294A GB 2236515 A GB2236515 A GB 2236515A
Authority
GB
United Kingdom
Prior art keywords
escape system
passenger aircraft
aloft
civil passenger
aircraft escape
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.)
Withdrawn
Application number
GB8919294A
Other versions
GB8919294D0 (en
Inventor
Raam Shankar Pershadsingh
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Individual
Original Assignee
Individual
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 Individual filed Critical Individual
Priority to GB8919294A priority Critical patent/GB2236515A/en
Publication of GB8919294D0 publication Critical patent/GB8919294D0/en
Publication of GB2236515A publication Critical patent/GB2236515A/en
Withdrawn legal-status Critical Current

Links

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
    • B64D25/00—Emergency apparatus or devices, not otherwise provided for
    • 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
    • B64C1/32—Severable or jettisonable parts of fuselage facilitating emergency escape

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Business, Economics & Management (AREA)
  • Emergency Management (AREA)
  • Mechanical Engineering (AREA)
  • Emergency Lowering Means (AREA)

Abstract

An escape system by which passengers may disembark from an aloft aircraft. Comprising parachutes stored in front of all seats a spring driven latch secured to the distant end of the parachutes release cord ; a 'bar', uninterrupted, the distance between exits over and onto which the spring driven 'rip cord' latch is placed. Additionally, the incorporation of as many new exits as structurally feasible located in either the port or the starboard walls of the lavatory with a release bar on the side of the exit facing the nose of the aircraft, will provide an alternative exit with a greater positive safety margin.

Description

DESCRIPTIOM ALOFT CIVIL PASSENGER AIRCRAFT ESCAPE II THE CONSTRUCTION OF NEW EXIT(S) , AS STRUCTURALLY FEAS ABLE , LOCATED IN EITHER THE PORT OR STARBOARD WALL(S) OF THE LAVATORY(S) , WITH A 'RELEASE BAR' - FICED TO THE SIDE OF THE EXIT FACING THE NOSE OF THE AIRCRAFT .
THE NEW EXIT IS RETAINED I. POSITION BY FOUR OR MORE RELEASE LATCHES AS IN FIGS.3 , 4 & 5 .
THE NEW EXIT IS ALSO RETALIED BY AN INSET OVERNANG AS IN FIGS. I , 2 , 3 & 5 .

Claims (1)

  1. Claima an aloft civil passenger aircraft escape system .
    Claims an aloft civil passenger aircraft escape system such that parachutes are introduced aboaad civil passenger aircraft .
    Claims an aloft civil passenger aircraft escape system in which a spring driven latch is secured to the distant end of the parachute release cord .
    Claims an aloft civil passenger aircraft escape system with an uninterrupted 'bar' running between exits over and onto which the spring driven latch is placed .
    Claims an aloft civil passenger aircraft escape system substantially as described in figs.I-5 Claims 'new' exit(s) as stucturally feasable located in either the port or starboard wall(s) of the lavatory(s) with a 'release bar' on the side of the exit facing the nose of the aircraft .
GB8919294A 1989-08-24 1989-08-24 Civil passenger aircraft escape system Withdrawn GB2236515A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB8919294A GB2236515A (en) 1989-08-24 1989-08-24 Civil passenger aircraft escape system

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB8919294A GB2236515A (en) 1989-08-24 1989-08-24 Civil passenger aircraft escape system

Publications (2)

Publication Number Publication Date
GB8919294D0 GB8919294D0 (en) 1989-10-04
GB2236515A true GB2236515A (en) 1991-04-10

Family

ID=10662074

Family Applications (1)

Application Number Title Priority Date Filing Date
GB8919294A Withdrawn GB2236515A (en) 1989-08-24 1989-08-24 Civil passenger aircraft escape system

Country Status (1)

Country Link
GB (1) GB2236515A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US10377463B2 (en) * 2014-09-29 2019-08-13 Airbus Operations (S.A.S.) Aircraft comprising a hatch and a fall-protection device

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB410361A (en) * 1933-08-04 1934-05-17 Stanley Switlik Improvements in and relating to parachute pack and chair
GB560578A (en) * 1942-11-05 1944-04-11 John Holt Booth Improvements in or relating to aircraft bodies
GB560803A (en) * 1942-11-13 1944-04-20 Arthur Sam Cheston Improvements relating to escape hatches and other detachable panels of aircraft
GB1093241A (en) * 1964-04-22 1967-11-29 British Aircraft Corp Ltd Improvements in emergency exit arrangements in aircraft
US3488021A (en) * 1968-02-19 1970-01-06 Mc Donnell Douglas Corp Escape system module feed and release mechanism

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB410361A (en) * 1933-08-04 1934-05-17 Stanley Switlik Improvements in and relating to parachute pack and chair
GB560578A (en) * 1942-11-05 1944-04-11 John Holt Booth Improvements in or relating to aircraft bodies
GB560803A (en) * 1942-11-13 1944-04-20 Arthur Sam Cheston Improvements relating to escape hatches and other detachable panels of aircraft
GB1093241A (en) * 1964-04-22 1967-11-29 British Aircraft Corp Ltd Improvements in emergency exit arrangements in aircraft
US3488021A (en) * 1968-02-19 1970-01-06 Mc Donnell Douglas Corp Escape system module feed and release mechanism

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US10377463B2 (en) * 2014-09-29 2019-08-13 Airbus Operations (S.A.S.) Aircraft comprising a hatch and a fall-protection device

Also Published As

Publication number Publication date
GB8919294D0 (en) 1989-10-04

Similar Documents

Publication Publication Date Title
DE59208399D1 (en) Aircraft
CA2296252A1 (en) Emergency exit system
MX9206903A (en) EQUIPMENT TO VENTILATE THE PASSENGER AREA IN CABINS IN FAST RUN ELEVATORS.
ATE266563T1 (en) LUGGAGE STORAGE ARRANGEMENT IN AN AIRCRAFT PASSENGER CABIN
FR2714021B1 (en) Aircraft seat, particularly rotorcraft seat, with energy absorption device automatically adjustable according to the size of the occupant.
CA2349076A1 (en) Safety system for a helicopter
GB2236515A (en) Civil passenger aircraft escape system
US3348513A (en) Life-saving safety devices for twin passenger aircraft or ships
DE3760575D1 (en) Aerial propellers, in particular for aircraft propulsion
GB9012432D0 (en) Connection system for aircraft propeller blades
GB1186631A (en) A Parachute
GB1287755A (en) Improvements in or relating to gliding-type parachutes
RU1795947C (en) Mounting helicopter
GB1141669A (en) Aircraft emergency ejection arrangement
Fox Realistic civil helicopter crash safety
RU2075861C1 (en) METHOD FOR EMERGENCY LEAVING THE AIRCRAFT CREW
MICCICHE et al. HASEP- Survival from crashed Navy helicopters
Jeziorski Realistic research
LORCH Preliminary development of the XV(Ex-Vee) aircrew restraint
HE et al. Onset mechanism of blade stall flutter
Ropelewski NASA plans high-speed design for follow-on QSRA research.
RODRIGUEZ et al. Aircrew restraint improvement program
Frisbee The track to survival
TURNBOW et al. Crash survival design guide(Design criteria for safety factors in aircraft crash survival)
RU96108215A (en) AIRCRAFT RESCUE SYSTEM

Legal Events

Date Code Title Description
WAP Application withdrawn, taken to be withdrawn or refused ** after publication under section 16(1)