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Integrated Main Gear Box And Upper Control System For Advanced Helicopters

Abstract: In conventional Helicopters, upper control system is separately positioned over the . main gear box assembly to transfer the control input to the main _rotor blade. In this arrangement, upper control systems are not protected from environmental effects and small arm fire. To protect the upper control system from such threats, main gearbox is made to accommodate upper control system inside the gearbox and this assembly become one. unit for assembly and also this assembly supports all · accessories like Alternator drive, Hydraulic drive, lube oil pump for its own lubrication ·purpose. It is called Integrated Dynamic System (IDS) where in main gearbox, upper control system, rotor hub and actuator are assembled as a single unit.

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Notices, Deadlines & Correspondence

Patent Information

Application #
Filing Date
29 December 2016
Publication Number
27/2018
Publication Type
INA
Invention Field
MECHANICAL ENGINEERING
Status
Email
Parent Application
Patent Number
Legal Status
Grant Date
2024-01-03
Renewal Date

Applicants

Hindustan Aeronautics Limited
Rotary Wing Research and Design Centre Design Complex, Vimanapura post, Bengaluru, Karnataka, India 560017.

Inventors

1. K.SELVAKUMAR
Transmission & Rotor, design group Hindustan Aeronautics, Limited Rotary Wing Research, and Design Centre Design Complex Vimanapura post, Bengaluru, Karnataka, India 560017
2. C. PRADHAN
Transmission & Rotor, design group Hindustan Aeronautics, Limited Rotary Wing Research, and Design Centre Design Complex Vimanapura post, Bengaluru, Karnataka, India 560017
3. LAKKAPPA HUNALLI
Transmission & Rotor, design group Hindustan Aeronautics, Limited Rotary Wing Research, and Design Centre Design Complex Vimanapura post, Bengaluru, Karnataka, India 560017
4. R. NAGARAJAN
Transmission & Rotor, design group Hindustan Aeronautics, Limited Rotary Wing Research, and Design Centre Design Complex Vimanapura post, Bengaluru, Karnataka, India 560017
5. M.S.NARAYANAN
Transmission & Rotor, design group Hindustan Aeronautics, Limited Rotary Wing Research, and Design Centre Design Complex Vimanapura post, Bengaluru, Karnataka, India 560017
6. S. BHATTACHARYA
Transmission & Rotor, design group Hindustan Aeronautics, Limited Rotary Wing Research, and Design Centre Design Complex Vimanapura post, Bengaluru, Karnataka, India 560017

Specification

Documents

Application Documents

# Name Date
1 Form3_As Filed_29-11-2016.pdf 2016-11-29
2 Form2 Title Page_Provisional_29-11-2016.pdf 2016-11-29
3 Form1_As Filed_29-11-2016.pdf 2016-11-29
4 Description Provisional_As Filed_29-11-2016.pdf 2016-11-29
5 Correspondence by Applicant_As Filed_29-12-2016.pdf 2016-12-29
6 Form3_After Provisional_21-11-2017.pdf 2017-11-21
7 Form2 Title Page_Complete_21-11-2017.pdf 2017-11-21
8 Form1_After Provisional_21-11-2017.pdf 2017-11-21
9 Form18_Normal Request_21-11-2017.pdf 2017-11-21
10 Drawing_After Provisional_21-11-2017.pdf 2017-11-21
11 Description Complete_As Filed_21-11-2017.pdf 2017-11-21
12 Correspondence by Applicant_Complete_21-11-2017.pdf 2017-11-21
13 Claims_After Provisional_21-11-2017.pdf 2017-11-21
14 Abstract_After Provisional_21-11-2017.pdf 2017-11-21
15 201641044829-Drawing_FER Reply_24-02-2021.pdf 2021-02-24
16 201641044829-Claims_FER Reply_24-02-2021.pdf 2021-02-24
17 201641044829-Amended Pages Of Specification_FER Reply_24-02-2021.pdf 2021-02-24
18 201641044829-Abstract_FER Reply_24-02-2021.pdf 2021-02-24
19 201641044829-FER.pdf 2021-10-17
20 201641044829-Correspondence_FER Reply_24-02-201.pdf 2021-10-17
21 201641044829-US(14)-HearingNotice-(HearingDate-05-12-2023).pdf 2023-11-14
22 201641044829-Proof of Right [07-12-2023(online)].pdf 2023-12-07
23 201641044829-Written submissions and relevant documents [18-12-2023(online)].pdf 2023-12-18
24 201641044829-Retyped Pages under Rule 14(1) [18-12-2023(online)].pdf 2023-12-18
25 201641044829-Annexure [18-12-2023(online)].pdf 2023-12-18
26 201641044829-2. Marked Copy under Rule 14(2) [18-12-2023(online)].pdf 2023-12-18
27 201641044829-PatentCertificate03-01-2024.pdf 2024-01-03
28 201641044829-IntimationOfGrant03-01-2024.pdf 2024-01-03

Search Strategy

1 SEARCH_STRATEGY_201641044829E_19-08-2020.pdf

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