MX2016000192A - A step platform. - Google Patents
A step platform.Info
- Publication number
- MX2016000192A MX2016000192A MX2016000192A MX2016000192A MX2016000192A MX 2016000192 A MX2016000192 A MX 2016000192A MX 2016000192 A MX2016000192 A MX 2016000192A MX 2016000192 A MX2016000192 A MX 2016000192A MX 2016000192 A MX2016000192 A MX 2016000192A
- Authority
- MX
- Mexico
- Prior art keywords
- step platform
- relates
- helicopters
- fairing
- payloads
- Prior art date
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D9/00—Equipment for handling freight; Equipment for facilitating passenger embarkation or the like
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/40—Weight reduction
Abstract
The present invention essentially relates to a step platform (1) which is designed to be used in the helicopters (H), enables the pilot and passenger to enter and exit the cockpit of the helicopter easily and allows the payloads (F) to be carried safely. Besides, it relates to a fairing (8) which covers the payload (F) and reduces possible aerodynamic performance losses caused by protruding structure.
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
TR201308035 | 2013-07-03 | ||
PCT/TR2014/000192 WO2015002623A1 (en) | 2013-07-03 | 2014-05-27 | A step platform |
Publications (1)
Publication Number | Publication Date |
---|---|
MX2016000192A true MX2016000192A (en) | 2016-06-07 |
Family
ID=51179130
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
MX2016000192A MX2016000192A (en) | 2013-07-03 | 2014-05-27 | A step platform. |
Country Status (5)
Country | Link |
---|---|
BR (1) | BR112016000069B1 (en) |
CL (1) | CL2015003791A1 (en) |
MX (1) | MX2016000192A (en) |
SA (1) | SA114350628B1 (en) |
WO (1) | WO2015002623A1 (en) |
Family Cites Families (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CA913591A (en) * | 1971-11-09 | 1972-10-31 | T. Cannon Corbitt | Helicopter cargo pod |
US4609167A (en) * | 1984-11-05 | 1986-09-02 | The United States Of America As Represented By The Secretary Of The Army | Helicopter cargo rack |
US4860972A (en) * | 1988-02-09 | 1989-08-29 | Era Aviation, Inc. | Auxiliary fuel tanks for aircraft |
US5072895A (en) * | 1990-07-05 | 1991-12-17 | Mark Camus | Cargo platform assembly mounted to a helicopter |
-
2014
- 2014-05-27 MX MX2016000192A patent/MX2016000192A/en active IP Right Grant
- 2014-05-27 BR BR112016000069-2A patent/BR112016000069B1/en active IP Right Grant
- 2014-05-27 WO PCT/TR2014/000192 patent/WO2015002623A1/en active Application Filing
- 2014-06-26 SA SA114350628A patent/SA114350628B1/en unknown
-
2015
- 2015-12-30 CL CL2015003791A patent/CL2015003791A1/en unknown
Also Published As
Publication number | Publication date |
---|---|
WO2015002623A1 (en) | 2015-01-08 |
CL2015003791A1 (en) | 2017-03-31 |
BR112016000069B1 (en) | 2022-05-10 |
SA114350628B1 (en) | 2017-05-30 |
BR112016000069A2 (en) | 2017-08-22 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
FG | Grant or registration |