GB1202211A - Improvements relating to aircraft crash recorder units - Google Patents
Improvements relating to aircraft crash recorder unitsInfo
- Publication number
- GB1202211A GB1202211A GB5048466A GB5048466A GB1202211A GB 1202211 A GB1202211 A GB 1202211A GB 5048466 A GB5048466 A GB 5048466A GB 5048466 A GB5048466 A GB 5048466A GB 1202211 A GB1202211 A GB 1202211A
- Authority
- GB
- United Kingdom
- Prior art keywords
- aircraft
- cover
- location
- spring
- withdraws
- 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
- 230000001960 triggered effect Effects 0.000 abstract 1
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 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
- B64D25/00—Emergency apparatus or devices, not otherwise provided for
- B64D25/08—Ejecting or escaping means
- B64D25/20—Releasing of crash position indicators
Landscapes
- Business, Economics & Management (AREA)
- Emergency Management (AREA)
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
Abstract
1,202,211. Aircraft emergency apparatus. M. L. AVIATION CO. Ltd. 31 Jan., 1968 [10 Nov., 1966], No. 50484/60. Heading B7G. An aircraft flight recorder 5, which is buoyant (e.g. by having a floatable tank 6 attached thereto) is ejected from an aircraft when the aircraft sinks after ditching by apparatus comprising a releasable cover 15 covering an opening to the location of the flight recorder, a normally shut valve (e.g. a flap 17) sealing the location from the exterior of the cover, an ejection device (e.g. a spring 10) for ejecting the flight recorder outwardly through the opening, and a mechanism (e.g. a barometric switch 19 activated by water entering the inlet 20) which on actuation opens the valve 17 to flood the location thereby relieving the pressure differential across the cover, releases the cover and also causes the ejection device to operate. The barometric switch 19 when triggered withdraws a pin 21 allowing the spring 50 to collapse a toggle linkage 22, 23 which in turn withdraws a hook 24 releasing the spring 10, and via a linkage 28 to 32 withdraws a hook 36 releasing the cover 15 and the flap 17. There may be three hooks 36 and three flaps 17 moved together by three links 30 moved together by an interconnection 70. The flight recorder 5 may be connected to aircraft instruments by a cable 7 having two push in connectors 8, 9 of which at least one disconnects when the recorder is ejected.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB5048466A GB1202211A (en) | 1966-11-10 | 1966-11-10 | Improvements relating to aircraft crash recorder units |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB5048466A GB1202211A (en) | 1966-11-10 | 1966-11-10 | Improvements relating to aircraft crash recorder units |
Publications (1)
Publication Number | Publication Date |
---|---|
GB1202211A true GB1202211A (en) | 1970-08-12 |
Family
ID=10456059
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB5048466A Expired GB1202211A (en) | 1966-11-10 | 1966-11-10 | Improvements relating to aircraft crash recorder units |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB1202211A (en) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN103646442A (en) * | 2013-11-28 | 2014-03-19 | 陕西千山航空电子有限责任公司 | Aviation recorder with smell positioning function |
DE102015014602B3 (en) * | 2015-11-13 | 2017-05-11 | Münir Alatas | Flight recorder device |
CN114537668A (en) * | 2022-04-26 | 2022-05-27 | 成都凯天电子股份有限公司 | Locking and ejecting mechanism of throwing type flight parameter recorder and control method thereof |
-
1966
- 1966-11-10 GB GB5048466A patent/GB1202211A/en not_active Expired
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN103646442A (en) * | 2013-11-28 | 2014-03-19 | 陕西千山航空电子有限责任公司 | Aviation recorder with smell positioning function |
CN103646442B (en) * | 2013-11-28 | 2015-12-02 | 陕西千山航空电子有限责任公司 | A kind of aviation recorder with sense of smell positioning function |
DE102015014602B3 (en) * | 2015-11-13 | 2017-05-11 | Münir Alatas | Flight recorder device |
CN114537668A (en) * | 2022-04-26 | 2022-05-27 | 成都凯天电子股份有限公司 | Locking and ejecting mechanism of throwing type flight parameter recorder and control method thereof |
CN114537668B (en) * | 2022-04-26 | 2022-09-09 | 成都凯天电子股份有限公司 | Locking and ejecting mechanism of throwing type flight parameter recorder and control method thereof |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
PS | Patent sealed | ||
PLNP | Patent lapsed through nonpayment of renewal fees |