GB2145381B - Powerplant for a helicopter - Google Patents
Powerplant for a helicopterInfo
- Publication number
- GB2145381B GB2145381B GB08426403A GB8426403A GB2145381B GB 2145381 B GB2145381 B GB 2145381B GB 08426403 A GB08426403 A GB 08426403A GB 8426403 A GB8426403 A GB 8426403A GB 2145381 B GB2145381 B GB 2145381B
- Authority
- GB
- United Kingdom
- Prior art keywords
- powerplant
- helicopter
- Prior art date
- 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.)
- Expired
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/22—Compound rotorcraft, i.e. aircraft using in flight the features of both aeroplane and rotorcraft
- B64C27/26—Compound rotorcraft, i.e. aircraft using in flight the features of both aeroplane and rotorcraft characterised by provision of fixed wings
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C15/00—Attitude, flight direction, or altitude control by jet reaction
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Toys (AREA)
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB08426403A GB2145381B (en) | 1982-12-01 | 1984-10-18 | Powerplant for a helicopter |
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB08234318A GB2130984B (en) | 1982-12-01 | 1982-12-01 | Compound helicopter and power plant therefor |
| GB08426403A GB2145381B (en) | 1982-12-01 | 1984-10-18 | Powerplant for a helicopter |
Publications (3)
| Publication Number | Publication Date |
|---|---|
| GB8426403D0 GB8426403D0 (en) | 1984-11-21 |
| GB2145381A GB2145381A (en) | 1985-03-27 |
| GB2145381B true GB2145381B (en) | 1986-07-02 |
Family
ID=26284554
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB08426403A Expired GB2145381B (en) | 1982-12-01 | 1984-10-18 | Powerplant for a helicopter |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB2145381B (en) |
Families Citing this family (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4655685A (en) * | 1985-12-16 | 1987-04-07 | United Technologies Corporation | Helicopter main rotor blade having a short span slot near the tip end |
| GB2242236B (en) * | 1990-03-09 | 1994-10-26 | Sidney Patrick Taylor | Improvements in and relating to apparatus for use with aircraft jet engines |
-
1984
- 1984-10-18 GB GB08426403A patent/GB2145381B/en not_active Expired
Also Published As
| Publication number | Publication date |
|---|---|
| GB8426403D0 (en) | 1984-11-21 |
| GB2145381A (en) | 1985-03-27 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PCNP | Patent ceased through non-payment of renewal fee |
Effective date: 19941201 |