Secondary Antenna Switching Device SASD Patent 547107 Presented

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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 © 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 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, ZK-HTF late 2005 in New Zealand, highlighted the

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 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

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

Here is ZK-HTF ! 10/7/2020 www. aviationsafety. co. nz 6

Here is ZK-HTF ! 10/7/2020 www. aviationsafety. co. nz 6

Actual site of crash 10/7/2020 www. aviationsafety. co. nz 7

Actual site of crash 10/7/2020 www. aviationsafety. co. nz 7

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

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

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. nz 10

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. co. nz 11

Antenna remains 10/7/2020 www. aviationsafety. co. nz 12

Antenna remains 10/7/2020 www. aviationsafety. co. nz 12

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 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 • 10/7/2020 www. aviationsafety. co. nz 14

ELT • 10/7/2020 www. aviationsafety. co. nz 14

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 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 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 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 ZK-HTF was US$1, 400, 000 •

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 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 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 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 10/7/2020 © www. aviationsafety. co. nz 22

SASD 10/7/2020 © www. aviationsafety. co. nz 22

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. 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 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 • 10/7/2020 © www. aviationsafety. co. nz 25

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 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 • 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 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, 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 10/7/2020 www. aviationsafety. co. nz 30

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 antenna is visible behind battery box 10/7/2020 www. aviationsafety. co. nz 31

ELT Growth 10/7/2020 www. aviationsafety. co. nz 32

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 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 • • 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. 4209279 Email sales@aviationsafety. co. nz www. aviationsafety. co. nz 34