A SYSTEM FOR REAL TIME DETERMINATION OF PARAMETERS OF AN AIRCRAFT
LaoBiz.com profiles the Laos Patent “A SYSTEM FOR REAL TIME DETERMINATION OF PARAMETERS OF AN AIRCRAFT” from open registry fields, filed by RUNWEIGHT PTY LTD on 2017-08-07; current status: Awaiting formal examination. Identifiers include application No. P/642; DIP id LAP642; protection kind Patent - PCT National Phase. Key dates: publication 2025-12-19. Classification: B64D 45/00、G01G 19/07、G01M 1/12、G07B 15/00. Inventor(s)/designer(s): Bill HARTMANN. Abstract hint: There is provided a system for determining real-time parameters of an aircraft, the system comprising: at least two sensing apparatus, each…. This prose is informational only and does not constitute legal advice, ownership proof or an infringement opinion.
P/642
Mark
Key facts
- Type
- Patent
- App. no.
P/642- Status
- Awaiting formal examination
- Applicant
- RUNWEIGHT PTY LTD
- Agent
- Tilleke & Gibbins Lao Co., Ltd
- Filing date
- 2017-08-07
- Publication
- 2025-12-19
- Protection kind
- Patent - PCT National Phase
- Priority
- AU · 2016903644 · 2016-09-09
- Applicant address
- RUNWEIGHT PTY LTD · 5 Mareno Road, Tullamarine, Victoria 3043, Australia · AU
- Agent address
- Tilleke & Gibbins Lao Co., Ltd · No. 302/1B, 3rd Floor, Vieng Vang Tower, Unit 15, Boulichan Road, Dongpalan Thong Village, Sisattanak District, Vientiane Capital, Lao PDR · LA
- Nice / IPC classes
- B64D 45/00 · G01G 19/07 · G01M 1/12 · G07B 15/00
- Goods / services
- —
Process
Steps follow the current public status-
Filed
-
Formal examination In progress
-
Substantive examination
-
Published
-
Granted
Related records
Linked from the LaoBiz.com company databaseSimilar Patent
Abstract
There is provided a system for determining real-time parameters of an aircraft, the system comprising: at least two sensing apparatus, each of the at least two sensing apparatus including a plurality of in-ground sensors; and at least one processing apparatus to process data received from the at least two sensing apparatus. It is preferable that a positioning of the at least two sensing apparatus is determined by a type of the aircraft being measured
There is provided a system for determining real-time parameters of an aircraft, the system comprising: at least two sensing apparatus, each of the at least two sensing apparatus including a plurality of in-ground sensors; and at least one processing apparatus to process data received from the at least two sensing apparatus. It is preferable that a positioning of the at least two sensing apparatus is determined by a type of the aircraft being measured
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