GB1325083A - Parachute deployment system - Google Patents
Parachute deployment systemInfo
- Publication number
- GB1325083A GB1325083A GB456671A GB1325083DA GB1325083A GB 1325083 A GB1325083 A GB 1325083A GB 456671 A GB456671 A GB 456671A GB 1325083D A GB1325083D A GB 1325083DA GB 1325083 A GB1325083 A GB 1325083A
- Authority
- GB
- United Kingdom
- Prior art keywords
- parachute
- signal
- height
- passed
- relay
- 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
- 230000003111 delayed effect Effects 0.000 abstract 1
- 230000000694 effects 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; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D17/00—Parachutes
- B64D17/40—Packs
- B64D17/52—Opening, e.g. manual
- B64D17/54—Opening, e.g. manual automatic
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Radar Systems Or Details Thereof (AREA)
Abstract
1325083 Radar M L AVIATION CO Ltd 8 May 1972 [12 Feb 1971] 4566/71 Heading H4D [Also in Division B7] Apparatus for association with a parachute, particularly for supply dropping, to effect deployment of the parachute at a predetermined altitude comprises a transmitter 1 for transmitting a frequency-modulated carrier wave, a receiver 2 which receives signals reflected from the ground always at a different frequency from those transmitted, a filter 3 to which the signal from receiver 2 is fed to remove the modulating wave. The signal is then passed to a high pass filter 4 to remove the carrier wave thus leaving the beat or difference frequency between the transmitted and received signals, which is passed to an amplifier 5. The output from the amplifier is fed to a Schmitt trigger 6 which produces a pulse at a preset input level, such pulses being counted by an integrator stage 7 and the resulting D.C. voltage, which is proportional to the altitude, is used to set a further Schmitt trigger 8, which is arranged toreset toits normal state after the pro-selected deployment height. The device is energized by a battery 14 via a switch 15 closed by a lanyard when the parachute is dropped. A relay 9 is provided to be energized in the absence of a signal or in the presence of a signal equivalent to an altitude below the preset level, and a further relay 10 is arranged as a delayed arming system to ensure that the circuit will not be armed until a height of between 1À2 and 2À2 times the preset height is passed within a period of 3 seconds. When the beat or difference frequency falls to that corresponding to the preset height relay 9 will pull in to complete the circuit to a connector 12 which will operate a cable cutter or other device to initiate deployment of the parachute.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB456671 | 1971-02-12 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB1325083A true GB1325083A (en) | 1973-08-01 |
Family
ID=9779569
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB456671A Expired GB1325083A (en) | 1971-02-12 | 1971-02-12 | Parachute deployment system |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB1325083A (en) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN105775142A (en) * | 2016-03-25 | 2016-07-20 | 深圳市轻准科技有限公司 | Autonomous parachute opening safety protection method and system for small aircraft |
RU2737458C1 (en) * | 2019-12-17 | 2020-11-30 | ФЕДЕРАЛЬНОЕ ГОСУДАРСТВЕННОЕ КАЗЕННОЕ ВОЕННОЕ ОБРАЗОВАТЕЛЬНОЕ УЧРЕЖДЕНИЕ ВЫСШЕГО ОБРАЗОВАНИЯ "Военная академия Ракетных войск стратегического назначения имени Петра Великого" МИНИСТЕРСТВА ОБОРОНЫ РОССИЙСКОЙ ФЕДЕРАЦИИ | Device for polythermal cutting of reserve parachute closing loop |
RU2737456C1 (en) * | 2019-11-27 | 2020-11-30 | ФЕДЕРАЛЬНОЕ ГОСУДАРСТВЕННОЕ КАЗЕННОЕ ВОЕННОЕ ОБРАЗОВАТЕЛЬНОЕ УЧРЕЖДЕНИЕ ВЫСШЕГО ОБРАЗОВАНИЯ "Военная академия Ракетных войск стратегического назначения имени Петра Великого" МИНИСТЕРСТВА ОБОРОНЫ РОССИЙСКОЙ ФЕДЕРАЦИИ | Device for thermal cutting of reserve parachute closing loop |
-
1971
- 1971-02-12 GB GB456671A patent/GB1325083A/en not_active Expired
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN105775142A (en) * | 2016-03-25 | 2016-07-20 | 深圳市轻准科技有限公司 | Autonomous parachute opening safety protection method and system for small aircraft |
RU2737456C1 (en) * | 2019-11-27 | 2020-11-30 | ФЕДЕРАЛЬНОЕ ГОСУДАРСТВЕННОЕ КАЗЕННОЕ ВОЕННОЕ ОБРАЗОВАТЕЛЬНОЕ УЧРЕЖДЕНИЕ ВЫСШЕГО ОБРАЗОВАНИЯ "Военная академия Ракетных войск стратегического назначения имени Петра Великого" МИНИСТЕРСТВА ОБОРОНЫ РОССИЙСКОЙ ФЕДЕРАЦИИ | Device for thermal cutting of reserve parachute closing loop |
RU2737458C1 (en) * | 2019-12-17 | 2020-11-30 | ФЕДЕРАЛЬНОЕ ГОСУДАРСТВЕННОЕ КАЗЕННОЕ ВОЕННОЕ ОБРАЗОВАТЕЛЬНОЕ УЧРЕЖДЕНИЕ ВЫСШЕГО ОБРАЗОВАНИЯ "Военная академия Ракетных войск стратегического назначения имени Петра Великого" МИНИСТЕРСТВА ОБОРОНЫ РОССИЙСКОЙ ФЕДЕРАЦИИ | Device for polythermal cutting of reserve parachute closing loop |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
PS | Patent sealed | ||
PLNP | Patent lapsed through nonpayment of renewal fees |