GB699290A - Improvements relating to emergency escape apparatus for aircraft - Google Patents
Improvements relating to emergency escape apparatus for aircraftInfo
- Publication number
- GB699290A GB699290A GB3026350A GB3026350A GB699290A GB 699290 A GB699290 A GB 699290A GB 3026350 A GB3026350 A GB 3026350A GB 3026350 A GB3026350 A GB 3026350A GB 699290 A GB699290 A GB 699290A
- Authority
- GB
- United Kingdom
- Prior art keywords
- fuselage
- cabin
- aircraft
- separation
- detached
- 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
- 238000000926 separation method Methods 0.000 abstract 3
- 230000008878 coupling Effects 0.000 abstract 2
- 238000010168 coupling process Methods 0.000 abstract 2
- 238000005859 coupling reaction Methods 0.000 abstract 2
- 108010066057 cabin-1 Proteins 0.000 abstract 1
- 239000002360 explosive Substances 0.000 abstract 1
- 230000000087 stabilizing effect Effects 0.000 abstract 1
- 230000003068 static effect Effects 0.000 abstract 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D25/00—Emergency apparatus or devices, not otherwise provided for
- B64D25/08—Ejecting or escaping means
- B64D25/12—Ejectable capsules
Abstract
699,290. Dropping cabins from aircraft. M. L. AVIATION CO., Ltd. Feb. 12, 1952 [Dec. 11, 1950], No. 30263/50. Class 9(ii) [Also in Groups XXV and XXXIII] In an aircraft emergency escape apparatus the cabin forming the nose of the aircraft can be detached from the fuselage and brought to earth by parachute: Separation of the cabin and fuselage is effected by a cartridge-operated mechanism which first disengages the couplings securing the cabin to the fuselage, breaks the electric control circuits, erects the cabin stabilizing fins and finally causes forceful separation of the cabin and fuselage. As shown, Fig. 1, the cabin 1, is separable from the fuselage 2 at 4. The cartridge operated gun, 5, Fig. 2, operates the fins 17, electrical separation 18, and mechanical couplings 15 through the linkwork 6, 9, 10, 13, 14, 15, 16. During the final period of its stroke the gun operates a telescopic cylinder (not shown) which thrusts the cabin and fuselage apart. The parachutes (not shown) are released by a static line attached to the fuselage and three sets of progressively larger parachutes are opened and then detached at predetermined intervals by explosive devices before the final group is opened. Specification 645,605, [Group XXVIII], is referred to.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB3026350A GB699290A (en) | 1950-12-11 | 1950-12-11 | Improvements relating to emergency escape apparatus for aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB3026350A GB699290A (en) | 1950-12-11 | 1950-12-11 | Improvements relating to emergency escape apparatus for aircraft |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB699290A true GB699290A (en) | 1953-11-04 |
Family
ID=10304872
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB3026350A Expired GB699290A (en) | 1950-12-11 | 1950-12-11 | Improvements relating to emergency escape apparatus for aircraft |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB699290A (en) |
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2762588A (en) * | 1954-01-21 | 1956-09-11 | Martin James | Ejection seat and parachute assembly for a single person |
| DE1038409B (en) * | 1955-05-04 | 1958-09-04 | Philipp Georg Alexander Helmut | Drop-off cabins, especially for aircraft taking off and landing vertically |
| US2941764A (en) * | 1957-08-08 | 1960-06-21 | Electronics Corp America | Flaps for supersonic aircraft escape systems |
| US2977080A (en) * | 1955-05-04 | 1961-03-28 | Zborowski Helmut Ph G A R Von | Aircraft having a detachable cabin |
| GB2118522A (en) * | 1982-04-16 | 1983-11-02 | Messerschmitt Boelkow Blohm | A two part connection having a taper sleeve and a taper shank |
| GB2200877A (en) * | 1987-02-10 | 1988-08-17 | Zinovi Levin | Crew safety device for spacecraft and aeroplanes. joints for booster rocket segments |
-
1950
- 1950-12-11 GB GB3026350A patent/GB699290A/en not_active Expired
Cited By (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2762588A (en) * | 1954-01-21 | 1956-09-11 | Martin James | Ejection seat and parachute assembly for a single person |
| DE1038409B (en) * | 1955-05-04 | 1958-09-04 | Philipp Georg Alexander Helmut | Drop-off cabins, especially for aircraft taking off and landing vertically |
| US2977080A (en) * | 1955-05-04 | 1961-03-28 | Zborowski Helmut Ph G A R Von | Aircraft having a detachable cabin |
| US2941764A (en) * | 1957-08-08 | 1960-06-21 | Electronics Corp America | Flaps for supersonic aircraft escape systems |
| GB2118522A (en) * | 1982-04-16 | 1983-11-02 | Messerschmitt Boelkow Blohm | A two part connection having a taper sleeve and a taper shank |
| GB2200877A (en) * | 1987-02-10 | 1988-08-17 | Zinovi Levin | Crew safety device for spacecraft and aeroplanes. joints for booster rocket segments |
| GB2200877B (en) * | 1987-02-10 | 1990-10-10 | Zinovi Levin | Device for overcoming the problem of crew safety during a spacecraft launch and improve the joints connecting the segments of the solid rocket booster |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| GB699290A (en) | Improvements relating to emergency escape apparatus for aircraft | |
| GB1214875A (en) | Emergency landing apparatus for aircraft | |
| GB731660A (en) | Improvements relating to aircraft | |
| GB793927A (en) | Improvements relating to rocket containers for aircraft | |
| GB724092A (en) | Aircraft interconnecting mechanism | |
| US1715742A (en) | Safety device for aeroplanes | |
| GB609229A (en) | Improvements in or relating to aircraft | |
| GB1237189A (en) | Emergency landing system, particularly for aircraft with high aspect ratio wings | |
| CN211874182U (en) | Central control door lock system of luggage compartment of civil aircraft | |
| GB899043A (en) | Aircraft with a detachable emergency unit | |
| GB748956A (en) | Improvements relating to escape equipment for aircraft | |
| GB494399A (en) | Aerial bombing devices | |
| GB672915A (en) | Improvements in aircraft | |
| GB580592A (en) | Improvements in and relating to automatic parachute release apparatus for use in aircraft | |
| Martin | Ejection from high speed aircraft | |
| JPS59209999A (en) | Device for relaxing shock on emergency drop of aircraft | |
| GB723922A (en) | Improvements in and relating to control means for use with ejection seats of aircraft | |
| GB652131A (en) | Control means for use with ejection seat of aircraft | |
| JANIK | Possibilities of in-flight simulation of rotary wing and VTOL aircraft systems by means of a BO 105 helicopter(Rotary wing and VTOL aircraft controllability requirements definition through in-flight simulation of visual and kinetic impressions and environmental conditions by BO-105 helicopter) | |
| ES243170A1 (en) | Improvements introduced in the parachute (Machine-translation by Google Translate, not legally binding) | |
| GB191108220A (en) | Improvements in or relating to Bombs for use with Aeroplanes and other Flying Machines. | |
| AU152259B2 (en) | Improvements in parachute apparatus for retarding aircraft, particularly before landing | |
| GB564415A (en) | An improved air-drag landing anchor device for aircraft | |
| GB623891A (en) | Improvements in or relating to aircraft cockpit hoods | |
| CA465616A (en) | Landing and launching apparatus for aircraft |