FR2152534A1 - - Google Patents
Info
- Publication number
- FR2152534A1 FR2152534A1 FR7224192A FR7224192A FR2152534A1 FR 2152534 A1 FR2152534 A1 FR 2152534A1 FR 7224192 A FR7224192 A FR 7224192A FR 7224192 A FR7224192 A FR 7224192A FR 2152534 A1 FR2152534 A1 FR 2152534A1
- Authority
- FR
- France
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Withdrawn
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/82—Rotorcraft; Rotors peculiar thereto characterised by the provision of an auxiliary rotor or fluid-jet device for counter-balancing lifting rotor torque or changing direction of rotorcraft
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/82—Rotorcraft; Rotors peculiar thereto characterised by the provision of an auxiliary rotor or fluid-jet device for counter-balancing lifting rotor torque or changing direction of rotorcraft
- B64C2027/8263—Rotorcraft; Rotors peculiar thereto characterised by the provision of an auxiliary rotor or fluid-jet device for counter-balancing lifting rotor torque or changing direction of rotorcraft comprising in addition rudders, tails, fins, or the like
- B64C2027/8281—Rotorcraft; Rotors peculiar thereto characterised by the provision of an auxiliary rotor or fluid-jet device for counter-balancing lifting rotor torque or changing direction of rotorcraft comprising in addition rudders, tails, fins, or the like comprising horizontal tail planes
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mutual Connection Of Rods And Tubes (AREA)
- Earth Drilling (AREA)
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US18029571A | 1971-09-14 | 1971-09-14 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| FR2152534A1 true FR2152534A1 (enExample) | 1973-04-27 |
Family
ID=22659927
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| FR7224192A Withdrawn FR2152534A1 (enExample) | 1971-09-14 | 1972-06-28 |
Country Status (6)
| Country | Link |
|---|---|
| US (1) | US3706432A (enExample) |
| JP (1) | JPS4862199A (enExample) |
| DE (1) | DE2231010A1 (enExample) |
| FR (1) | FR2152534A1 (enExample) |
| GB (1) | GB1332620A (enExample) |
| IT (1) | IT967164B (enExample) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP0007317A3 (en) * | 1978-07-12 | 1980-02-06 | United Technologies Corporation | Helicopter with stabilator detuned in antisymmetric vibration modes from main rotor wake excitation frequency |
Families Citing this family (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE3500454A1 (de) * | 1985-01-09 | 1986-07-10 | Valerij Vladimirovič Moskau/Moskva Archipov | Ladetreppe |
| ES2279716B1 (es) * | 2005-12-26 | 2008-08-16 | Airbus España, S.L. | Herraje de giro para un empenaje de una aeronave. |
| ES2345584B1 (es) * | 2007-12-21 | 2011-07-18 | Airbus Operations, S.L. | Superficie de control de aeronave. |
| EP2878536B1 (en) | 2013-11-29 | 2017-05-24 | AIRBUS HELICOPTERS DEUTSCHLAND GmbH | Advanced pitch stabilizer |
| US20170106970A1 (en) * | 2015-10-15 | 2017-04-20 | The Boeing Company | Composite failsafe torque tube |
| CN107745809B (zh) * | 2017-10-14 | 2020-04-21 | 上海歌尔泰克机器人有限公司 | 飞行器 |
| US12151811B2 (en) * | 2019-08-13 | 2024-11-26 | Textron Innovations Inc. | Tilting wing rotorcrafts and wing rotation systems |
| US11685515B2 (en) * | 2019-10-11 | 2023-06-27 | Textron Innovations Inc. | Active horizontal stabilizer for high speed rotorcraft |
| CN110697024B (zh) * | 2019-10-14 | 2022-07-15 | 中国航空工业集团公司西安飞机设计研究所 | 一种飞机尾翼结构 |
Family Cites Families (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2437330A (en) * | 1944-01-24 | 1948-03-09 | Alexander S Mullgardt | Variable incidence wing control for aircraft of the rotaly wing or airplane sustained type |
| US2959373A (en) * | 1954-12-10 | 1960-11-08 | Daniel R Zuck | Convertiplane |
-
1971
- 1971-09-14 US US180295A patent/US3706432A/en not_active Expired - Lifetime
-
1972
- 1972-06-24 DE DE2231010A patent/DE2231010A1/de active Pending
- 1972-06-28 FR FR7224192A patent/FR2152534A1/fr not_active Withdrawn
- 1972-06-28 GB GB3015872A patent/GB1332620A/en not_active Expired
- 1972-09-06 IT IT28838/72A patent/IT967164B/it active
- 1972-09-07 JP JP47089967A patent/JPS4862199A/ja active Pending
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP0007317A3 (en) * | 1978-07-12 | 1980-02-06 | United Technologies Corporation | Helicopter with stabilator detuned in antisymmetric vibration modes from main rotor wake excitation frequency |
Also Published As
| Publication number | Publication date |
|---|---|
| JPS4862199A (enExample) | 1973-08-30 |
| GB1332620A (en) | 1973-10-03 |
| DE2231010A1 (de) | 1973-03-22 |
| IT967164B (it) | 1974-02-28 |
| US3706432A (en) | 1972-12-19 |
Similar Documents
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| ST | Notification of lapse |