Secondary Antenna Switching Device SASD Patent 547107 Presented
![Secondary Antenna Switching Device ( SASD )- Patent 547107 Presented by Lloyd Klee 10/7/2020 Secondary Antenna Switching Device ( SASD )- Patent 547107 Presented by Lloyd Klee 10/7/2020](https://slidetodoc.com/presentation_image/ff0427a6271f29bd7582151387a03934/image-1.jpg)
![Project Goals • The project goal is to improve the ability of locating a Project Goals • The project goal is to improve the ability of locating a](https://slidetodoc.com/presentation_image/ff0427a6271f29bd7582151387a03934/image-2.jpg)
![Background • A recent helicopter crash, ZK-HTF late 2005 in New Zealand, highlighted the Background • A recent helicopter crash, ZK-HTF late 2005 in New Zealand, highlighted the](https://slidetodoc.com/presentation_image/ff0427a6271f29bd7582151387a03934/image-3.jpg)
![Background • The helicopter was found some 15 days after going missing. • It Background • The helicopter was found some 15 days after going missing. • It](https://slidetodoc.com/presentation_image/ff0427a6271f29bd7582151387a03934/image-4.jpg)
![ZK-HTF • ZK-HTF Eurocopter 120 B 10/7/2020 www. aviationsafety. co. nz 5 ZK-HTF • ZK-HTF Eurocopter 120 B 10/7/2020 www. aviationsafety. co. nz 5](https://slidetodoc.com/presentation_image/ff0427a6271f29bd7582151387a03934/image-5.jpg)
![Here is ZK-HTF ! 10/7/2020 www. aviationsafety. co. nz 6 Here is ZK-HTF ! 10/7/2020 www. aviationsafety. co. nz 6](https://slidetodoc.com/presentation_image/ff0427a6271f29bd7582151387a03934/image-6.jpg)
![Actual site of crash 10/7/2020 www. aviationsafety. co. nz 7 Actual site of crash 10/7/2020 www. aviationsafety. co. nz 7](https://slidetodoc.com/presentation_image/ff0427a6271f29bd7582151387a03934/image-7.jpg)
![Close up of crash site 10/7/2020 www. aviationsafety. co. nz 8 Close up of crash site 10/7/2020 www. aviationsafety. co. nz 8](https://slidetodoc.com/presentation_image/ff0427a6271f29bd7582151387a03934/image-8.jpg)
![After bush had been cleared 10/7/2020 www. aviationsafety. co. nz 9 After bush had been cleared 10/7/2020 www. aviationsafety. co. nz 9](https://slidetodoc.com/presentation_image/ff0427a6271f29bd7582151387a03934/image-9.jpg)
![ZK-HTF • Internal position of Kannad 406 AF, post crash 10/7/2020 www. aviationsafety. co. ZK-HTF • Internal position of Kannad 406 AF, post crash 10/7/2020 www. aviationsafety. co.](https://slidetodoc.com/presentation_image/ff0427a6271f29bd7582151387a03934/image-10.jpg)
![ZK-HTF • Remains of the external antenna, the branch is above 10/7/2020 www. aviationsafety. ZK-HTF • Remains of the external antenna, the branch is above 10/7/2020 www. aviationsafety.](https://slidetodoc.com/presentation_image/ff0427a6271f29bd7582151387a03934/image-11.jpg)
![Antenna remains 10/7/2020 www. aviationsafety. co. nz 12 Antenna remains 10/7/2020 www. aviationsafety. co. nz 12](https://slidetodoc.com/presentation_image/ff0427a6271f29bd7582151387a03934/image-12.jpg)
![Antenna Test Results d. Bu. V/m • Antenna Vertical Horizontal • Damaged 121. 5 Antenna Test Results d. Bu. V/m • Antenna Vertical Horizontal • Damaged 121. 5](https://slidetodoc.com/presentation_image/ff0427a6271f29bd7582151387a03934/image-13.jpg)
![ELT • 10/7/2020 www. aviationsafety. co. nz 14 ELT • 10/7/2020 www. aviationsafety. co. nz 14](https://slidetodoc.com/presentation_image/ff0427a6271f29bd7582151387a03934/image-14.jpg)
![Summary • The tragedy was that the 406 AF-H ELT activated upon impact but Summary • The tragedy was that the 406 AF-H ELT activated upon impact but](https://slidetodoc.com/presentation_image/ff0427a6271f29bd7582151387a03934/image-15.jpg)
![Other reasons for failures to detect an ELT An ELT could “fail” for other Other reasons for failures to detect an ELT An ELT could “fail” for other](https://slidetodoc.com/presentation_image/ff0427a6271f29bd7582151387a03934/image-16.jpg)
![Solution ? • Directly as a result of this incident, a development of a Solution ? • Directly as a result of this incident, a development of a](https://slidetodoc.com/presentation_image/ff0427a6271f29bd7582151387a03934/image-17.jpg)
![Solution • The direct cost of searching for ZK-HTF was US$1, 400, 000 • Solution • The direct cost of searching for ZK-HTF was US$1, 400, 000 •](https://slidetodoc.com/presentation_image/ff0427a6271f29bd7582151387a03934/image-18.jpg)
![Solution ? • The SASD is located between the fixed ELT and the primary Solution ? • The SASD is located between the fixed ELT and the primary](https://slidetodoc.com/presentation_image/ff0427a6271f29bd7582151387a03934/image-19.jpg)
![Solution • The SASD will use the first 406 MHz signal from the ELT Solution • The SASD will use the first 406 MHz signal from the ELT](https://slidetodoc.com/presentation_image/ff0427a6271f29bd7582151387a03934/image-20.jpg)
![Solution l. If damaged, all further 406 MHz and 121. 5 MHz transmissions will Solution l. If damaged, all further 406 MHz and 121. 5 MHz transmissions will](https://slidetodoc.com/presentation_image/ff0427a6271f29bd7582151387a03934/image-21.jpg)
![SASD 10/7/2020 © www. aviationsafety. co. nz 22 SASD 10/7/2020 © www. aviationsafety. co. nz 22](https://slidetodoc.com/presentation_image/ff0427a6271f29bd7582151387a03934/image-22.jpg)
![SASD setup option • ELT to SASD with auxiliary antenna 10/7/2020 © www. aviationsafety. SASD setup option • ELT to SASD with auxiliary antenna 10/7/2020 © www. aviationsafety.](https://slidetodoc.com/presentation_image/ff0427a6271f29bd7582151387a03934/image-23.jpg)
![Summary • In the passive (non operational ) state, SASD always remains connected to Summary • In the passive (non operational ) state, SASD always remains connected to](https://slidetodoc.com/presentation_image/ff0427a6271f29bd7582151387a03934/image-24.jpg)
![SASD Block Diagram • 10/7/2020 © www. aviationsafety. co. nz 25 SASD Block Diagram • 10/7/2020 © www. aviationsafety. co. nz 25](https://slidetodoc.com/presentation_image/ff0427a6271f29bd7582151387a03934/image-25.jpg)
![Solution • When activated the SASD will result in a power loss of only Solution • When activated the SASD will result in a power loss of only](https://slidetodoc.com/presentation_image/ff0427a6271f29bd7582151387a03934/image-26.jpg)
![Patent 547107 approved • A worldwide patent has been applied for NZ # 547107 Patent 547107 approved • A worldwide patent has been applied for NZ # 547107](https://slidetodoc.com/presentation_image/ff0427a6271f29bd7582151387a03934/image-27.jpg)
![Sales l It is anticipated that the SASD will be sold as a standard Sales l It is anticipated that the SASD will be sold as a standard](https://slidetodoc.com/presentation_image/ff0427a6271f29bd7582151387a03934/image-28.jpg)
![Current Status • Overview of progress against schedule – On track initial concept, patent, Current Status • Overview of progress against schedule – On track initial concept, patent,](https://slidetodoc.com/presentation_image/ff0427a6271f29bd7582151387a03934/image-29.jpg)
![Auxiliary Antenna Trials 10/7/2020 www. aviationsafety. co. nz 30 Auxiliary Antenna Trials 10/7/2020 www. aviationsafety. co. nz 30](https://slidetodoc.com/presentation_image/ff0427a6271f29bd7582151387a03934/image-30.jpg)
![Tail Boom • Inside Tail Rotor boom, structure is Aluminium and Nomex • The Tail Boom • Inside Tail Rotor boom, structure is Aluminium and Nomex • The](https://slidetodoc.com/presentation_image/ff0427a6271f29bd7582151387a03934/image-31.jpg)
![ELT Growth 10/7/2020 www. aviationsafety. co. nz 32 ELT Growth 10/7/2020 www. aviationsafety. co. nz 32](https://slidetodoc.com/presentation_image/ff0427a6271f29bd7582151387a03934/image-32.jpg)
![Logo • Our logo includes a view of the Earth as seen by Apollo Logo • Our logo includes a view of the Earth as seen by Apollo](https://slidetodoc.com/presentation_image/ff0427a6271f29bd7582151387a03934/image-33.jpg)
![Contact Details • • 10/7/2020 Aviation Safety Supplies Ltd Phone +649. 4206079 Fax. +649. Contact Details • • 10/7/2020 Aviation Safety Supplies Ltd Phone +649. 4206079 Fax. +649.](https://slidetodoc.com/presentation_image/ff0427a6271f29bd7582151387a03934/image-34.jpg)
- Slides: 34
![Secondary Antenna Switching Device SASD Patent 547107 Presented by Lloyd Klee 1072020 Secondary Antenna Switching Device ( SASD )- Patent 547107 Presented by Lloyd Klee 10/7/2020](https://slidetodoc.com/presentation_image/ff0427a6271f29bd7582151387a03934/image-1.jpg)
Secondary Antenna Switching Device ( SASD )- Patent 547107 Presented by Lloyd Klee 10/7/2020 © www. aviationsafety. co. nz 1
![Project Goals The project goal is to improve the ability of locating a Project Goals • The project goal is to improve the ability of locating a](https://slidetodoc.com/presentation_image/ff0427a6271f29bd7582151387a03934/image-2.jpg)
Project Goals • The project goal is to improve the ability of locating a crashed aircraft in the event that the 406 MHz ELT primary external antenna is compromised. 10/7/2020 www. aviationsafety. co. nz 2
![Background A recent helicopter crash ZKHTF late 2005 in New Zealand highlighted the Background • A recent helicopter crash, ZK-HTF late 2005 in New Zealand, highlighted the](https://slidetodoc.com/presentation_image/ff0427a6271f29bd7582151387a03934/image-3.jpg)
Background • A recent helicopter crash, ZK-HTF late 2005 in New Zealand, highlighted the fragility of ELT antennas. • The 406 MHz ELT in this high speed incident functioned as designed • With the external antenna ripped off by a tree upon impact, the 406 and 121. 5 MHz transmissions were too weak to be picked up by the Cospas-sarsat system or searching aircraft. 10/7/2020 www. aviationsafety. co. nz 3
![Background The helicopter was found some 15 days after going missing It Background • The helicopter was found some 15 days after going missing. • It](https://slidetodoc.com/presentation_image/ff0427a6271f29bd7582151387a03934/image-4.jpg)
Background • The helicopter was found some 15 days after going missing. • It was located in a small bush covered creek bed 15 metres (50 feet) wide. • The area had been flown over a number of times by searching aircraft and the land owner had walked by the crash scene without realising that the helicopter was within a few metres of his path. 10/7/2020 www. aviationsafety. co. nz 4
![ZKHTF ZKHTF Eurocopter 120 B 1072020 www aviationsafety co nz 5 ZK-HTF • ZK-HTF Eurocopter 120 B 10/7/2020 www. aviationsafety. co. nz 5](https://slidetodoc.com/presentation_image/ff0427a6271f29bd7582151387a03934/image-5.jpg)
ZK-HTF • ZK-HTF Eurocopter 120 B 10/7/2020 www. aviationsafety. co. nz 5
![Here is ZKHTF 1072020 www aviationsafety co nz 6 Here is ZK-HTF ! 10/7/2020 www. aviationsafety. co. nz 6](https://slidetodoc.com/presentation_image/ff0427a6271f29bd7582151387a03934/image-6.jpg)
Here is ZK-HTF ! 10/7/2020 www. aviationsafety. co. nz 6
![Actual site of crash 1072020 www aviationsafety co nz 7 Actual site of crash 10/7/2020 www. aviationsafety. co. nz 7](https://slidetodoc.com/presentation_image/ff0427a6271f29bd7582151387a03934/image-7.jpg)
Actual site of crash 10/7/2020 www. aviationsafety. co. nz 7
![Close up of crash site 1072020 www aviationsafety co nz 8 Close up of crash site 10/7/2020 www. aviationsafety. co. nz 8](https://slidetodoc.com/presentation_image/ff0427a6271f29bd7582151387a03934/image-8.jpg)
Close up of crash site 10/7/2020 www. aviationsafety. co. nz 8
![After bush had been cleared 1072020 www aviationsafety co nz 9 After bush had been cleared 10/7/2020 www. aviationsafety. co. nz 9](https://slidetodoc.com/presentation_image/ff0427a6271f29bd7582151387a03934/image-9.jpg)
After bush had been cleared 10/7/2020 www. aviationsafety. co. nz 9
![ZKHTF Internal position of Kannad 406 AF post crash 1072020 www aviationsafety co ZK-HTF • Internal position of Kannad 406 AF, post crash 10/7/2020 www. aviationsafety. co.](https://slidetodoc.com/presentation_image/ff0427a6271f29bd7582151387a03934/image-10.jpg)
ZK-HTF • Internal position of Kannad 406 AF, post crash 10/7/2020 www. aviationsafety. co. nz 10
![ZKHTF Remains of the external antenna the branch is above 1072020 www aviationsafety ZK-HTF • Remains of the external antenna, the branch is above 10/7/2020 www. aviationsafety.](https://slidetodoc.com/presentation_image/ff0427a6271f29bd7582151387a03934/image-11.jpg)
ZK-HTF • Remains of the external antenna, the branch is above 10/7/2020 www. aviationsafety. co. nz 11
![Antenna remains 1072020 www aviationsafety co nz 12 Antenna remains 10/7/2020 www. aviationsafety. co. nz 12](https://slidetodoc.com/presentation_image/ff0427a6271f29bd7582151387a03934/image-12.jpg)
Antenna remains 10/7/2020 www. aviationsafety. co. nz 12
![Antenna Test Results d Bu Vm Antenna Vertical Horizontal Damaged 121 5 Antenna Test Results d. Bu. V/m • Antenna Vertical Horizontal • Damaged 121. 5](https://slidetodoc.com/presentation_image/ff0427a6271f29bd7582151387a03934/image-13.jpg)
Antenna Test Results d. Bu. V/m • Antenna Vertical Horizontal • Damaged 121. 5 MHz • Auxiliary Antenna 24. 5 111. 4 22. 7 92. 3 • Damaged 406 MHz • Auxiliary Antenna 82. 5 131. 7 72. 6 105. 1 10/7/2020 www. aviationsafety. co. nz 13
![ELT 1072020 www aviationsafety co nz 14 ELT • 10/7/2020 www. aviationsafety. co. nz 14](https://slidetodoc.com/presentation_image/ff0427a6271f29bd7582151387a03934/image-14.jpg)
ELT • 10/7/2020 www. aviationsafety. co. nz 14
![Summary The tragedy was that the 406 AFH ELT activated upon impact but Summary • The tragedy was that the 406 AF-H ELT activated upon impact but](https://slidetodoc.com/presentation_image/ff0427a6271f29bd7582151387a03934/image-15.jpg)
Summary • The tragedy was that the 406 AF-H ELT activated upon impact but the transmissions were not detected as the external antenna was destroyed. • In this case, had the antenna been on the other side of the aircraft, it is possible that the antenna would have survived the impact. For a report on the actions of the rescue coordination centre go to http: //www. nzsar. org. nz/reports. html 10/7/2020 www. aviationsafety. co. nz 15
![Other reasons for failures to detect an ELT An ELT could fail for other Other reasons for failures to detect an ELT An ELT could “fail” for other](https://slidetodoc.com/presentation_image/ff0427a6271f29bd7582151387a03934/image-16.jpg)
Other reasons for failures to detect an ELT An ELT could “fail” for other reasons such as: • An electronic malfunction of the ELT or remote control • Antenna cables breaking on impact • The ELT being inadvertently turned off on the remote control • Lack of or poor service to the ELT 10/7/2020 www. aviationsafety. co. nz 16
![Solution Directly as a result of this incident a development of a Solution ? • Directly as a result of this incident, a development of a](https://slidetodoc.com/presentation_image/ff0427a6271f29bd7582151387a03934/image-17.jpg)
Solution ? • Directly as a result of this incident, a development of a Secondary Antenna Switching Device (SASD) has been achieved • This will allow for an auxiliary antenna to be fitted to the SASD or at a nearby location within the fuselage which will be activated if the external antenna is damaged. 10/7/2020 www. aviationsafety. co. nz 17
![Solution The direct cost of searching for ZKHTF was US1 400 000 Solution • The direct cost of searching for ZK-HTF was US$1, 400, 000 •](https://slidetodoc.com/presentation_image/ff0427a6271f29bd7582151387a03934/image-18.jpg)
Solution • The direct cost of searching for ZK-HTF was US$1, 400, 000 • Had the SASD device been fitted and worked as designed, the search cost would have been less than US$3000 10/7/2020 © www. aviationsafety. co. nz 18
![Solution The SASD is located between the fixed ELT and the primary Solution ? • The SASD is located between the fixed ELT and the primary](https://slidetodoc.com/presentation_image/ff0427a6271f29bd7582151387a03934/image-19.jpg)
Solution ? • The SASD is located between the fixed ELT and the primary external antenna. • In the normal state, the SASD has no effect on the circuit. It is “transparent” or INERT. • However, should the external antenna be damaged in a crash, the SASD will detect this fact via the activation of the 406 MHz ELT 10/7/2020 www. aviationsafety. co. nz 19
![Solution The SASD will use the first 406 MHz signal from the ELT Solution • The SASD will use the first 406 MHz signal from the ELT](https://slidetodoc.com/presentation_image/ff0427a6271f29bd7582151387a03934/image-20.jpg)
Solution • The SASD will use the first 406 MHz signal from the ELT to detect the fact that the primary external antenna has been damaged. • The 160 msec carrier lead signal is utilized and the SASD will switch rapidly to the auxiliary antenna within 5 msec. 10/7/2020 www. aviationsafety. co. nz 20
![Solution l If damaged all further 406 MHz and 121 5 MHz transmissions will Solution l. If damaged, all further 406 MHz and 121. 5 MHz transmissions will](https://slidetodoc.com/presentation_image/ff0427a6271f29bd7582151387a03934/image-21.jpg)
Solution l. If damaged, all further 406 MHz and 121. 5 MHz transmissions will be passed to the auxiliary antenna. The switched relay will stay in the alternate auxillary antenna position as the SASD has its’ own inherent battery power l 10/7/2020 www. aviationsafety. co. nz 21
![SASD 1072020 www aviationsafety co nz 22 SASD 10/7/2020 © www. aviationsafety. co. nz 22](https://slidetodoc.com/presentation_image/ff0427a6271f29bd7582151387a03934/image-22.jpg)
SASD 10/7/2020 © www. aviationsafety. co. nz 22
![SASD setup option ELT to SASD with auxiliary antenna 1072020 www aviationsafety SASD setup option • ELT to SASD with auxiliary antenna 10/7/2020 © www. aviationsafety.](https://slidetodoc.com/presentation_image/ff0427a6271f29bd7582151387a03934/image-23.jpg)
SASD setup option • ELT to SASD with auxiliary antenna 10/7/2020 © www. aviationsafety. co. nz 23
![Summary In the passive non operational state SASD always remains connected to Summary • In the passive (non operational ) state, SASD always remains connected to](https://slidetodoc.com/presentation_image/ff0427a6271f29bd7582151387a03934/image-24.jpg)
Summary • In the passive (non operational ) state, SASD always remains connected to the primary antenna • If the secondary antenna is activated, the primary antenna can be restored by pressing the reset switch on the SASD 10/7/2020 www. aviationsafety. co. nz 24
![SASD Block Diagram 1072020 www aviationsafety co nz 25 SASD Block Diagram • 10/7/2020 © www. aviationsafety. co. nz 25](https://slidetodoc.com/presentation_image/ff0427a6271f29bd7582151387a03934/image-25.jpg)
SASD Block Diagram • 10/7/2020 © www. aviationsafety. co. nz 25
![Solution When activated the SASD will result in a power loss of only Solution • When activated the SASD will result in a power loss of only](https://slidetodoc.com/presentation_image/ff0427a6271f29bd7582151387a03934/image-26.jpg)
Solution • When activated the SASD will result in a power loss of only 0. 5 d. B • This is well within the specifications as laid down by Cospas-sarsat of 5 watts plus or minus 2 d. B as per C/S S. 007 page 6 - 49 clause 5. 3. 1. 3 10/7/2020 www. aviationsafety. co. nz 26
![Patent 547107 approved A worldwide patent has been applied for NZ 547107 Patent 547107 approved • A worldwide patent has been applied for NZ # 547107](https://slidetodoc.com/presentation_image/ff0427a6271f29bd7582151387a03934/image-27.jpg)
Patent 547107 approved • A worldwide patent has been applied for NZ # 547107 • A new TSO currently being written 10/7/2020 www. aviationsafety. co. nz 27
![Sales l It is anticipated that the SASD will be sold as a standard Sales l It is anticipated that the SASD will be sold as a standard](https://slidetodoc.com/presentation_image/ff0427a6271f29bd7582151387a03934/image-28.jpg)
Sales l It is anticipated that the SASD will be sold as a standard accessory for a 406 MHz antenna or ELT l 10/7/2020 Sales of the SASD, once all necessary approvals are in place, will be sold via ELT & antenna manufacturers www. aviationsafety. co. nz 28
![Current Status Overview of progress against schedule On track initial concept patent Current Status • Overview of progress against schedule – On track initial concept, patent,](https://slidetodoc.com/presentation_image/ff0427a6271f29bd7582151387a03934/image-29.jpg)
Current Status • Overview of progress against schedule – On track initial concept, patent, testing & samples produced – On schedule with testing and approval process – Testing has been accomplished with auxiliary antennas transmitting from within various fuselage types 10/7/2020 www. aviationsafety. co. nz 29
![Auxiliary Antenna Trials 1072020 www aviationsafety co nz 30 Auxiliary Antenna Trials 10/7/2020 www. aviationsafety. co. nz 30](https://slidetodoc.com/presentation_image/ff0427a6271f29bd7582151387a03934/image-30.jpg)
Auxiliary Antenna Trials 10/7/2020 www. aviationsafety. co. nz 30
![Tail Boom Inside Tail Rotor boom structure is Aluminium and Nomex The Tail Boom • Inside Tail Rotor boom, structure is Aluminium and Nomex • The](https://slidetodoc.com/presentation_image/ff0427a6271f29bd7582151387a03934/image-31.jpg)
Tail Boom • Inside Tail Rotor boom, structure is Aluminium and Nomex • The antenna is visible behind battery box 10/7/2020 www. aviationsafety. co. nz 31
![ELT Growth 1072020 www aviationsafety co nz 32 ELT Growth 10/7/2020 www. aviationsafety. co. nz 32](https://slidetodoc.com/presentation_image/ff0427a6271f29bd7582151387a03934/image-32.jpg)
ELT Growth 10/7/2020 www. aviationsafety. co. nz 32
![Logo Our logo includes a view of the Earth as seen by Apollo Logo • Our logo includes a view of the Earth as seen by Apollo](https://slidetodoc.com/presentation_image/ff0427a6271f29bd7582151387a03934/image-33.jpg)
Logo • Our logo includes a view of the Earth as seen by Apollo 17 in December 1972. Upon leaving the lunar surface, Commander Gene Cernan said • "we leave as we came, and, God willing, we shall return, with peace and hope for all mankind. " • 10/7/2020 © courtesy of NASA www. aviationsafety. co. nz 33
![Contact Details 1072020 Aviation Safety Supplies Ltd Phone 649 4206079 Fax 649 Contact Details • • 10/7/2020 Aviation Safety Supplies Ltd Phone +649. 4206079 Fax. +649.](https://slidetodoc.com/presentation_image/ff0427a6271f29bd7582151387a03934/image-34.jpg)
Contact Details • • 10/7/2020 Aviation Safety Supplies Ltd Phone +649. 4206079 Fax. +649. 4209279 Email sales@aviationsafety. co. nz www. aviationsafety. co. nz 34
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